Merge branch 'chrislgarry:master' into master

.github/workflows/markdownlint.yml

@@ -5,6 +5,6 @@ jobs:
     runs-on: ubuntu-latest
     steps:
     - name: Check out code
-      uses: actions/checkout@master
+      uses: actions/checkout@v2
     - name: Run mdl
-      uses: actionshub/markdownlint@master
+      uses: actionshub/markdownlint@2.0.2

CONTRIBUTING.ar.md

@@ -8,10 +8,15 @@
 [English][EN]،
 [Español][ES]،
 [Français][FR]،
-[Kurdi][KU],
+[Italiano][IT]،
+[Kurdi][KU]،
+[Lietuvių][LT]،
 [Nederlands][NL]،
+[Norsk][NO]،
+[Polski][PL]،
 [Português][PT_BR]،
 [Türkçe][TR]،
+[Ελληνικά][GR]،
 **العربية**،
 [日本語][JA]،
 [正體中文][ZH_TW]،
@@ -24,10 +29,15 @@
 [EN]:CONTRIBUTING.md
 [ES]:CONTRIBUTING.es.md
 [FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
 [JA]:CONTRIBUTING.ja.md
 [KO_KR]:CONTRIBUTING.ko_kr.md
 [KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
 [NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
 [PT_BR]:CONTRIBUTING.pt_br.md
 [TR]:CONTRIBUTING.tr.md
 [ZH_CN]:CONTRIBUTING.zh_cn.md
@@ -117,7 +127,7 @@ R0820
 </div>
 
 ```plain
-	1)  FOO BAR BAZ QUX QUUX QUUZ. CORGE, GRAULT,
+	1)  FOO BAR BAZ QUX QUUX QUUZ. CORGE, GRAULT،
 	GARPLY, WALDO.
 ```
 
@@ -126,7 +136,7 @@ R0820
 </div>
 
 ```plain
-	1) FOO BAR BAZ QUX QUUX QUUZ.  CORGE, GRAULT,
+	1) FOO BAR BAZ QUX QUUX QUUZ.  CORGE, GRAULT،
 	   GARPLY, WALDO.
 ```
 

CONTRIBUTING.cz.md

@@ -1,15 +1,20 @@
 # Contributing
 
 🎌
-**Čeština**
+**Čeština**,
 [Deutsch][DE],
 [English][EN],
 [Español][ES],
 [Français][FR],
+[Italiano][IT],
 [Kurdi][KU],
+[Lietuvių][LT],
 [Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
 [Português][PT_BR],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [العربية][AR],
 [日本語][JA],
 [正體中文][ZH_TW],
@@ -22,10 +27,15 @@
 [EN]:CONTRIBUTING.md
 [ES]:CONTRIBUTING.es.md
 [FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
 [JA]:CONTRIBUTING.ja.md
 [KO_KR]:CONTRIBUTING.ko_kr.md
 [KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
 [NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
 [PT_BR]:CONTRIBUTING.pt_br.md
 [TR]:CONTRIBUTING.tr.md
 [ZH_CN]:CONTRIBUTING.zh_cn.md

CONTRIBUTING.de.md

@@ -6,10 +6,15 @@
 [English][EN],
 [Español][ES],
 [Français][FR],
+[Italiano][IT],
 [Kurdi][KU],
+[Lietuvių][LT],
 [Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
 [Português][PT_BR],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [العربية][AR],
 [日本語][JA],
 [正體中文][ZH_TW],
@@ -22,10 +27,15 @@
 [EN]:CONTRIBUTING.md
 [ES]:CONTRIBUTING.es.md
 [FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
 [JA]:CONTRIBUTING.ja.md
 [KO_KR]:CONTRIBUTING.ko_kr.md
 [KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
 [NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
 [PT_BR]:CONTRIBUTING.pt_br.md
 [TR]:CONTRIBUTING.tr.md
 [ZH_CN]:CONTRIBUTING.zh_cn.md

CONTRIBUTING.es.md

@@ -6,10 +6,15 @@
 [English][EN],
 **Español**,
 [Français][FR],
+[Italiano][IT],
 [Kurdi][KU],
+[Lietuvių][LT],
 [Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
 [Português][PT_BR],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [العربية][AR],
 [日本語][JA],
 [正體中文][ZH_TW],
@@ -22,10 +27,15 @@
 [EN]:CONTRIBUTING.md
 [ES]:CONTRIBUTING.es.md
 [FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
 [JA]:CONTRIBUTING.ja.md
 [KO_KR]:CONTRIBUTING.ko_kr.md
 [KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
 [NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
 [PT_BR]:CONTRIBUTING.pt_br.md
 [TR]:CONTRIBUTING.tr.md
 [ZH_CN]:CONTRIBUTING.zh_cn.md

CONTRIBUTING.fr.md

@@ -6,10 +6,15 @@
 [English][EN],
 [Español][ES],
 **Français**,
+[Italiano][IT],
 [Kurdi][KU],
+[Lietuvių][LT],
 [Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
 [Português][PT_BR],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [العربية][AR],
 [日本語][JA],
 [正體中文][ZH_TW],
@@ -22,23 +27,28 @@
 [EN]:CONTRIBUTING.md
 [ES]:CONTRIBUTING.es.md
 [FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
 [JA]:CONTRIBUTING.ja.md
 [KO_KR]:CONTRIBUTING.ko_kr.md
 [KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
 [NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
 [PT_BR]:CONTRIBUTING.pt_br.md
 [TR]:CONTRIBUTING.tr.md
 [ZH_CN]:CONTRIBUTING.zh_cn.md
 [ZH_TW]:CONTRIBUTING.zh_tw.md
 
-Le code source de ce dépôt a été numérisé manuellement à partir d’imprimés papier, de sorte que les fautes de frappe et autres anomalies ont été introduites accidentellement. Le code doit être modifié pour être cohérent avec les impressions numérisées:
+Le code source de ce dépôt a été numérisé manuellement à partir de papiers imprimés, les fautes de frappe et autres anomalies ont donc été introduites accidentellement. Le code doit être modifié pour être cohérent avec les impressions numérisées suivantes:
 
 - [Impressions AGC pour Comanche][8]
 - [Impressions AGC pour Luminary][9]
 
 ## Extensions utiles
 
-Github prend en charge nativement la syntaxe pour le langage assembleur AGC. Malheureusement, votre éditeur de texte ne l’aura pas. Mais il y a des extensions pour le langage AGC pour les éditeurs suivants:
+GitHub prend en charge nativement la syntaxe pour le langage assembleur AGC. Malheureusement, votre éditeur de texte ne l’aura pas. Mais il y a des extensions pour le langage AGC pour les éditeurs suivants:
 
 - [Atom][Atom]†
 - [CodeBlocks][CodeBlocks]
@@ -68,18 +78,36 @@ Github prend en charge nativement la syntaxe pour le langage assembleur AGC. Mal
 
 **Note:** GitHub et les extensions marquées ci-dessus vous assureront d'utiliser automatiquement le bon formatage.
 
-- Indenter avec tabulation
-- Les tabulations ont une taille de 8
+- Utiliser tabulation (tab) pour l'indentation
+- Utiliser une largeur de 8 caractères pour la tabulation
 - Pas d'espace à la fin des ligne
 
 ## Comment vérifier ?
 
-Tout écart entre les scans et le code source dans ce référentiel, y compris :
+Tout écart entre les scans et le code source dans ce référentiel.
 
 ### Commentaires
 
-- Les commentaires dans le code transcrit doivent correspondre exactement aux scans
-  - Cela peut impliquer de créer délibérément une erreur de frappe  ou de supprimer/ajouter un commentaire entier.
+- Les commentaires dans le code transcrit **doivent** correspondre **exactement** aux scans.
+  - Les problèmes courants que vous devez rechercher lors de la vérification sont les suivants. Attention la liste n'est pas exhaustive!
+
+#### Erreurs typographiques
+
+À certains endroits, les développeurs originaux ont fait des erreurs typographiques en écrivant des commentaires. Certaines d’entre elles ont été corrigées par erreur lors de la numérisation initiale, mais la numérisation a également introduit des erreurs typographiques qui n’étaient pas présentes dans les scans.
+
+Par exemple, si les commentaires numérisés contiennent `SPACECRAFT`, mais que `SPAECRAFT` a été imprimé dans les scans, la numérisation DOIT être corrigée en `SPAECRAFT` (C manquant).
+
+De même, si un mot a une faute de frappe dans la numérisation mais est correctement orthographié dans les scans, alors la faute de frappe DOIT être corrigée.
+
+#### Espaces
+
+Les espaces entre deux caractères dans les commentaires **DEVRAIENT** correspondre aux scans. Dans la plupart des cas (voir la discussion dans [#316][10]), c'est:
+
+- Espace unique pour les nouveaux mots.
+- Double espace pour les nouvelles phrases.
+- Triple espace pour les indentations.
+
+Toutes les pages des scans ne suivent pas cette généralisation, si les scans n'ont qu'un seul espace au lieu d'un double espace, utiliser un seul espace.
 
 ### Sauts de ligne
 
@@ -87,7 +115,7 @@ Tout écart entre les scans et le code source dans ce référentiel, y compris :
 - Les sauts de ligne *sans* `R0000` dans la colonne 1 ne doivent contenir que 1 ou 2 lignes vides d'affilée.
   - Si il y a plus de 2 lignes vides, supprimer les sauts de ligne supplémentaires.
     - Ne pas prendre en compte les lignes avecc `R0000` dans la cononne 1.
-  - Dans les images sources, il y a digits non imprimés dans la colonne 8. Un 2 force un double espace (une seul ligne vide) et un 3 force une triple espace (double ligne vide). Les valeurs 4-8 ont été définies mais n’ont jamais été utilisées. Pour en savoir plus [#159][7]
+  - Dans les images sources, ceux-ci ont été créés à cause d'un caractère non imprimé dans la colonne 8. Un 2 a forcé un double espace (une seul ligne vide) et un 3 a forcé un triple espace (double ligne vide). Les valeurs 4-8 ont été définies mais n’ont jamais été utilisées. Pour en savoir plus [#159][7]
 
 Par exemple, ce qui suit:
 
@@ -110,30 +138,9 @@ R0820
  0820   LAMPTEST  CS  IMODES33
 ```
 
-### Espaces
-
-- Les espaces entre deux caractères doivent respecter la convention suivante (voir la discussion [#316][10]):
-  - Un seul espace pour un nouveau mot.
-  - Deux espaces pour une nouvelle phrase.
-  - Trois espaces pour l'indentations.
-
-Par exemple, ce qui suit:
-
-```plain
-	1)  FOO BAR BAZ QUX QUUX QUUZ. CORGE, GRAULT,
-	GARPLY, WALDO.
-```
-
-Doit devenir:
-
-```plain
-	1) FOO BAR BAZ QUX QUUX QUUZ.  CORGE, GRAULT,
-	   GARPLY, WALDO.
-```
-
 ## Note
 
-Avant de faire une PR, assurez-vous que vos modifications sont cohérentes avec les scans!
+Avant de faire un PR, assurez-vous que vos modifications sont cohérentes avec les scans!
 
 [0]:https://github.com/chrislgarry/Apollo-11/pull/new/master
 [1]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/

CONTRIBUTING.gr.md

@@ -0,0 +1,153 @@
+# Συνεισφορά
+
+🎌
+[Čeština][CZ],
+[Deutsch][DE],
+[English][EN],
+[Español][ES],
+[Français][FR],
+[Italiano][IT],
+[Kurdi][KU],
+[Lietuvių][LT],
+[Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
+[Português][PT_BR],
+[Türkçe][TR],
+**Ελληνικά**,
+[العربية][AR],
+[日本語][JA],
+[正體中文][ZH_TW],
+[简体中文][ZH_CN],
+[한국어][KO_KR]
+
+[AR]:CONTRIBUTING.ar.md
+[CZ]:CONTRIBUTING.cz.md
+[DE]:CONTRIBUTING.de.md
+[EN]:CONTRIBUTING.md
+[ES]:CONTRIBUTING.es.md
+[FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
+[JA]:CONTRIBUTING.ja.md
+[KO_KR]:CONTRIBUTING.ko_kr.md
+[KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
+[NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
+[PT_BR]:CONTRIBUTING.pt_br.md
+[TR]:CONTRIBUTING.tr.md
+[ZH_CN]:CONTRIBUTING.zh_cn.md
+[ZH_TW]:CONTRIBUTING.zh_tw.md
+
+Ο πηγαίος κώδικας σε αυτό το αποθετήριο ψηφιοποιήθηκε χειροκίνητα (με μη αυτόματο τρόπο) από εκτυπώσεις σε χαρτί, έτσι τυχαία λάθη και άλλες αποκλίσεις μπορεί να έχουν εισαχθεί κατά λάθος. Ο κώδικας πρέπει να τροποποιείται ώστε πάντα να είναι συνεπής με τις παρακάτω σαρωμένες εκτυπώσεις:
+
+- [AGC printouts for Comanche][8]
+- [AGC printouts for Luminary][9]
+
+## Χρήσιμες Επεκτάσεις
+
+Το GitHub διαθέτει υποστήριξη συντακτικού για τη γλώσσα assembly του AGC. Δυστυχώς, ο επεξεργαστής κώδικά σας μπορεί να μην την υποστηρίζει, ωστόσο, υπάρχουν επεκτάσεις για τη γλώσσα assembly AGC που παρέχουν επισήμανση σύνταξης για τους ακόλουθους επεξεργαστές κώδικα:
+
+- [Atom][Atom]†
+- [CodeBlocks][CodeBlocks]
+- [Eclipse][Eclipse]
+- [Kate][Kate]
+- [ProgrammersNotepad][ProgrammersNotepad]
+- [Sublime Text 3][Sublime Text]†
+- [TextPad][TextPad]
+- [Vim][Vim]
+- [Visual Studio Code][VisualStudioCode]†
+- [jEdit][jEdit]
+
+† Υποστηρίζει αυτόματη μορφοποίηση
+
+[Atom]:https://github.com/Alhadis/language-agc
+[CodeBlocks]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/CodeBlocks
+[Eclipse]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/Eclipse
+[Kate]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/Kate
+[ProgrammersNotepad]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/ProgrammersNotepad
+[Sublime Text]:https://github.com/jimlawton/AGC-Assembly
+[TextPad]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/TextPad
+[Vim]:https://github.com/wsdjeg/vim-assembly
+[VisualStudioCode]:https://github.com/wopian/agc-assembly
+[jEdit]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/jEdit
+
+## Mορφοποίηση
+
+Σημείωση: Το GitHub και οι επεκτάσεις που σημειώνονται παραπάνω θα διασφαλίσουν ότι χρησιμοποιείτε τη σωστή μορφοποίηση αυτόματα.
+
+- Χρήση εσοχής με tab
+- 8 χαρακτήες κενού για εσοχή tab
+- Περικοπή τελικών κενών χαρακτήρων γραμμής
+
+## Τί να ελέγξω;
+
+Τυχόν αποκλίσεις μεταξύ των σαρώσεων και του πηγαίου κώδικα σε αυτό το αποθετήριο.
+
+### Σχόλια
+
+Τα σχόλια στον μεταγραμμένο κώδικα **ΠΡΕΠΕΙ** να ταιριάζουν **ακριβώς** με τις σαρώσεις.
+
+Συχνά προβλήματα που θα μπορούσατε να ψάξετε κατά τη διόρθωση περιλεμβάνουν αλλά δεν περιορίζονται σε:
+
+#### Τυπογραφικά λάθη
+
+Σε μερικά σημεία, οι αρχικοί προγραμματιστές έκαναν τυπογραφικά λάθη κατά τη σύνταξη σχολίων. Μερικά από αυτά διορθώθηκαν κατά λάθος κατά την αρχική ψηφιοποίηση, ωστόσο η ψηφιοποίηση έχει επίσης εισαγάγει τυπογραφικά λάθη που δεν υπήρχαν στις σαρώσεις.
+
+Για παράδειγμα, εάν τα ψηφιοποιημένα σχόλια περιείχαν `SPACECRAFT`, αλλά `SPAECRAFT` ήταν γραμμένο στις σαρώσεις, τότε η ψηφιοποίηση **ΠΡΕΠΕΙ** να διορθωθεί σε `SPAECRAFT` (λείπει το `C`).
+
+Αντίστοιχα, αν μια λέξη έχει κάποιο τυπογραφικό λάθος στην ψηφιοποίηση αλλά είναι γραμμένη σωστά στις σαρώσεις τότε αυτό το τυπογραφικό λάθος **ΠΡΕΠΕΙ** να διορθωθεί.
+
+#### Κενά
+
+Τα κενά μεταξύ χαρακτήρων στα σχόλια **ΘΑ ΕΠΡΕΠΕ** να ταιριάζουν με τις σαρώσεις. Τις περισσότερες φορές (δείτε τη συζήτηση στο [#316[10], αυτό σημαίνει:
+
+- Ένα κενό για νέες λέξεις.
+- Δύο κενά για νέες προτάσεις.
+- Τρία κενά για εσοχές.
+
+Αυτή η γενίκευση δεν ακολουθείτε από όλες τις σαρωμένες σελίδες, αν μια σάρωση έχει ένα κενό αντί για δύο, χρησιμοποιήστε ένα.
+
+### Αλλαγές γραμμής
+
+- Οι αλλαγές γραμμής με `R0000` στη στήλη 1 πρέπει να ταιριάζουν ακριβώς με τις σαρώσεις.
+- Οι αλλαγές γραμμής *χωρίς* `R0000` στη στήλη 1 πρέπει να περιέχουν μόνο 1 ή 2 κενές γραμμές στη σειρά.
+  - Εάν υπάρχουν περισσότερες από 2 αλλαγές γραμμών, αφαιρέστε τις επιπλέον αλλαγές γραμμής.
+    - Οι γραμμές με `R0000` στη στήλη 1 δεν υπολογίζονται σε αυτό.
+  - Στις εικόνες προέλευσης, αυτές δημιουργήθηκαν από ένα μη τυπωμένο ψηφίο στη στήλη 8. Ένα 2 ανάγκαζε ένα διπλό διάστημα (μονή κενή γραμμή) και ένα 3 ανάγκαζε ένα τριπλό διάστημα (διπλή κενή γραμμή). Οι τιμές 4-8 ορίστηκαν αλλά δεν χρησιμοποιήθηκαν ποτέ. Διαβάστε περισσότερα σχετικά, στο [#159][7]
+
+Για παράδειγμα το παρακάτω:
+
+```plain
+R0819   SUBROUTINE TO SKIP...
+R0820
+
+
+
+ 0821   LAMPTEST  CS  IMODES33
+```
+
+Πρέπει να γίνει:
+
+```plain
+R0819   SUBROUTINE TO SKIP...
+R0820
+
+
+ 0820   LAMPTEST  CS  IMODES33
+```
+
+## Σημείωση
+
+Πριν κάνετε ένα PR, παρακαλώ βεβαιωθείτε ότι οι αλλαγές σας είναι σύμφωνες με τις σαρώσεις!
+
+[0]:https://github.com/chrislgarry/Apollo-11/pull/new/master
+[1]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/
+[2]:http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/
+[6]:https://github.com/wopian/agc-assembly#user-settings
+[7]:https://github.com/chrislgarry/Apollo-11/issues/159
+[8]:http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/
+[9]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/
+[10]:https://github.com/chrislgarry/Apollo-11/pull/316#pullrequestreview-102892741

CONTRIBUTING.it.md

@@ -0,0 +1,154 @@
+# Contribuire
+
+🎌
+[Čeština][CZ],
+[Deutsch][DE],
+[English][EN],
+[Español][ES],
+[Français][FR],
+**Italiano**
+[Kurdi][KU],
+[Lietuvių][LT],
+[Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
+[Português][PT_BR],
+[Türkçe][TR],
+[Ελληνικά][GR],
+[العربية][AR],
+[日本語][JA],
+[正體中文][ZH_TW],
+[简体中文][ZH_CN],
+[한국어][KO_KR]
+
+[AR]:CONTRIBUTING.ar.md
+[CZ]:CONTRIBUTING.cz.md
+[DE]:CONTRIBUTING.de.md
+[EN]:CONTRIBUTING.md
+[ES]:CONTRIBUTING.es.md
+[FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
+[JA]:CONTRIBUTING.ja.md
+[KO_KR]:CONTRIBUTING.ko_kr.md
+[KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
+[NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
+[PT_BR]:CONTRIBUTING.pt_br.md
+[TR]:CONTRIBUTING.tr.md
+[ZH_CN]:CONTRIBUTING.zh_cn.md
+[ZH_TW]:CONTRIBUTING.zh_tw.md
+
+Il codice sorgente in questa repository è stato digitalizzato manualmente da stampe su carta, quindi errori di battitura e altre differenze sono state aggiunte accidentalmente. Il codice dovrebbe essere modificato per essere consistente con le seguenti scannerizzazioni:
+
+- [AGC stampa per Comanche][8]
+- [AGC stampa per Luminary][9]
+
+## Estensioni utili
+
+GitHub supporta la sintassi dell' assembly AGC nativamente. Se sfortunatamente il tuo editor di codice non dovesse farlo, sono presenti delle estensioni che aggiungono la colorazione della sintassi per i seguenti editor:
+
+- [Atom][Atom]†
+- [CodeBlocks][CodeBlocks]
+- [Eclipse][Eclipse]
+- [Kate][Kate]
+- [ProgrammersNotepad][ProgrammersNotepad]
+- [Sublime Text 3][Sublime Text]†
+- [TextPad][TextPad]
+- [Vim][Vim]
+- [Visual Studio Code][VisualStudioCode]†
+- [jEdit][jEdit]
+
+† Supporta la formattazione automatica
+
+[Atom]:https://github.com/Alhadis/language-agc
+[CodeBlocks]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/CodeBlocks
+[Eclipse]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/Eclipse
+[Kate]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/Kate
+[ProgrammersNotepad]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/ProgrammersNotepad
+[Sublime Text]:https://github.com/jimlawton/AGC-Assembly
+[TextPad]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/TextPad
+[Vim]:https://github.com/wsdjeg/vim-assembly
+[VisualStudioCode]:https://github.com/wopian/agc-assembly
+[jEdit]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/jEdit
+
+## Formattazione
+
+**Nota:** GitHub e le estensioni riportate di sopra assicureranno che tu stia usando automaticamente la formattazione corretta.
+
+- Indenta con le tabulazioni
+- Usa una tabulazione di larghezza 8
+- Elimina spazi a fine riga
+
+## Che cosa devo controllare?
+
+Qualsiasi differenza tra le scannerizzazioni e il codice sorgente in questa repository.
+
+### Commenti
+
+Commenti nel codice trascritto **DEVONO** coincidere **esattamente** con quelli delle scannerizzazioni.
+
+Errori comuni a cui dovresti stare attento mentre verifichi includono, ma non sono limitati a:
+
+#### Errori tipografici
+
+Qualche volta, gli sviluppatori originali hanno fatto degli errori tipografici mentre scrivevano i commenti. Alcuni sono stati erroneamente corretti durante la digitalizzazione iniziale e anche la digitalizzazione stessa ha introdotto altri errori tipografici che non erano presenti nelle scannerizzazioni originali.
+
+Per esempio, se i commenti digitalizzati contengono `SPACEFRAFT`, ma `SPAECRAFT` è stato stampato sulle scannerizzazioni, allora le digitalizzaioni **DEVONO** essere corrette in `SPAECRAFT` (senza `C`).
+
+Analogamente, se una parola ha un errore di battitura ma è scritta correttamente nelle scannerizzazioni allora l'errore **DEVE** essere corretto.
+
+#### Spazi
+
+Spazi tra due caratteri nei commenti **DOVREBBERO** corrispondere alle scannerizzazioni. Nella maggior parte dei casi (Si guardi la discussione in [#316][10]), questo comprende:
+
+- Spazio singolo tra parole.
+- Doppio spazio tra frasi.
+- Triplo spazio per l'indentazione.
+
+Non tutte le pagine nelle scannerizzazioni seguono queste linee guida, se le scannerizzazioni hanno un solo uno spazio, usane uno solo.
+
+### Ritorni a capo
+
+- I ritorni a capo *con* `R0000` nella colonna 1 dovrebbero corrispondere alle scannerizzaioni esattamente.
+- I ritorni a capo *senza* `R0000` nella colonna 1 dovrebbero contenere solo 1 o 2 linee vuote di seguito.
+  - Se ci sono più di 2 ritorni a capo, elimina quelli in eccesso.
+    - Righe con `R0000` nella colonna 1 non seguono questa regola.
+  - Nelle immagini originali, queste sono state create da un numero non stampato nella colonna 8. Un 2 ha forzato un doppio spazio (una singola riga vuota), invece un 3 ha forzato uno spazio triplo (due righe vuote). Valori da 4 a 8 sono
+  stati definiti ma non sono mai stati usati. Puoi leggere di più qui [#159][7]
+
+Per esempio, il seguente:
+
+```plain
+R0819   SUBROUTINE TO SKIP...
+R0820
+
+
+
+ 0821   LAMPTEST  CS  IMODES33
+```
+
+Dovrebbe diventare:
+
+```plain
+R0819   SUBROUTINE TO SKIP...
+R0820
+
+
+ 0820   LAMPTEST  CS  IMODES33
+```
+
+## Note
+
+Prima di fare una PR(Pull Request), per piacere controlla che i tuoi cambiamenti siano consistenti con le scannerizzazioni!
+
+[0]:https://github.com/chrislgarry/Apollo-11/pull/new/master
+[1]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/
+[2]:http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/
+[6]:https://github.com/wopian/agc-assembly#user-settings
+[7]:https://github.com/chrislgarry/Apollo-11/issues/159
+[8]:http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/
+[9]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/
+[10]:https://github.com/chrislgarry/Apollo-11/pull/316#pullrequestreview-102892741

CONTRIBUTING.ja.md

@@ -6,10 +6,15 @@
 [English][EN],
 [Español][ES],
 [Français][FR],
+[Italiano][IT],
 [Kurdi][KU],
+[Lietuvių][LT],
 [Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
 [Português][PT_BR],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [العربية][AR],
 **日本語**,
 [正體中文][ZH_TW],
@@ -22,16 +27,21 @@
 [EN]:CONTRIBUTING.md
 [ES]:CONTRIBUTING.es.md
 [FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
 [JA]:CONTRIBUTING.ja.md
 [KO_KR]:CONTRIBUTING.ko_kr.md
 [KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
 [NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
 [PT_BR]:CONTRIBUTING.pt_br.md
 [TR]:CONTRIBUTING.tr.md
 [ZH_CN]:CONTRIBUTING.zh_cn.md
 [ZH_TW]:CONTRIBUTING.zh_tw.md
 
-このリポジトリのソースコードは紙の印刷物から手動でデジタル化された為、いくつかのタイプミスやその他の不一致が誤って導入されています。スキャンしたプリントアウトと一致する様にコードを変更する必要があります:
+このリポジトリのソースコードは紙の印刷物から手動でデジタル化された為、いくつかのタイプミスやその他の不一致が誤って導入されています。以下のスキャンしたプリントアウトと一致する様にコードを変更する必要があります:
 
 - [AGC printouts for Comanche][8]
 - [AGC printouts for Luminary][9]
@@ -74,12 +84,30 @@ GitHubには、組み込みのAGCアセンブリ言語の構文サポートが
 
 ## 確認方法は?
 
-スキャンとこのリポジトリ内のソースコードとの間の不一致:
+スキャンとこのリポジトリ内のソースコードとの間の不一致がある場合。
 
 ### コメント
 
-- 文字起こしされたコードのコメントはスキャンと正確に一致する必要があります
-  - これには意図的なタイプミス、またはコメント全体の削除/追加が含まれる場合があります。
+文字起こしされたコードのコメントはスキャンと**正確**に一致**しなければなりません**。
+
+校正中に注意する必要がある一般的な問題には、次のものがありますが、これらに限定されません:
+
+#### 誤植
+
+いくつかの場所において、元の開発者がコメントを書いている中で誤植をしています。これらのいくつかは、最初のデジタル化の際に修正がされていますが、デジタル化によってスキャンに存在しなかった誤植も発生してしまいました。
+
+例えば、デジタル化されたコメントに `SPACECRAFT` が含まれているが、 `SPAECRAFT` が印刷されたスキャンの場合、デジタル化は `SPAECRAFT` に修正**しなければなりません**(`C` が抜けている)。
+
+同様に、単語のデジタル化にタイプミスがあるが、スキャンでスペルが正しい場合は、タイプミスを修正**しなければなりません**。
+
+### スペース
+
+- コメント内の2つの文字間のスペースは、スキャンと一致**すべきです**。多くの場合（[#316][10]のディスカッションを参照）、次の規則に従う必要があります:
+  - 新しい単語の為の単一のスペース。
+  - 新しい文章の為の2個のスペース。
+  - インデントの為の3個のスペース。
+
+スキャンのすべてのページがこの一般化に従っている訳ではありません。スキャンに2個のスペースではなく1個のスペースしかない場合、1個のスペースを使用して下さい。
 
 ### 改行
 
@@ -110,27 +138,6 @@ R0820
  0820   LAMPTEST  CS  IMODES33
 ```
 
-### スペース
-
-- 文字列間内の2つの文字間のスペースは、次の規則に従う必要があります（[#316][10]のディスカッションを参照）:
-  - 新しい単語の為の単一のスペース。
-  - 新しい文章の為の2個のスペース。
-  - インデントの為の3個のスペース。
-
-例えば、次の通りです:
-
-```plain
-	1)  FOO BAR BAZ QUX QUUX QUUZ. CORGE, GRAULT,
-	GARPLY, WALDO.
-```
-
-これになるはずです:
-
-```plain
-	1) FOO BAR BAZ QUX QUUX QUUZ.  CORGE, GRAULT,
-	   GARPLY, WALDO.
-```
-
 ## 注意
 
 PRを作成する前に、変更がスキャンと一致していることを確認して下さい！

CONTRIBUTING.ko_kr.md

@@ -6,10 +6,15 @@
 [English][EN],
 [Español][ES],
 [Français][FR],
+[Italiano][IT],
 [Kurdi][KU],
+[Lietuvių][LT],
 [Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
 [Português][PT_BR],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [العربية][AR],
 [日本語][JA],
 [正體中文][ZH_TW],
@@ -22,10 +27,15 @@
 [EN]:CONTRIBUTING.md
 [ES]:CONTRIBUTING.es.md
 [FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
 [JA]:CONTRIBUTING.ja.md
 [KO_KR]:CONTRIBUTING.ko_kr.md
 [KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
 [NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
 [PT_BR]:CONTRIBUTING.pt_br.md
 [TR]:CONTRIBUTING.tr.md
 [ZH_CN]:CONTRIBUTING.zh_cn.md
@@ -61,7 +71,7 @@ GitHub은 내장 에디터에서 AGC문법을 지원합니다. 그러나 불행
 
 ## 포매팅
 
-**참고:** Github 내장 에디터와 위의 세 확장기능들은 이 문단에서 정의하는 포매팅을 자동으로 수행해줍니다.
+**참고:** GitHub 내장 에디터와 위의 세 확장기능들은 이 문단에서 정의하는 포매팅을 자동으로 수행해줍니다.
 
 - 탭 들여쓰기를 사용하십시오.
 - 들여쓰기 크기는 8입니다.

CONTRIBUTING.ku.md

@@ -6,10 +6,15 @@
 [English][EN],
 [Español][ES],
 [Français][FR],
+[Italiano][IT],
 **Kurdî**,
+[Lietuvių][LT],
 [Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
 [Português][PT_BR],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [العربية][AR],
 [日本語][JA],
 [正體中文][ZH_TW],
@@ -22,14 +27,22 @@
 [EN]:CONTRIBUTING.md
 [ES]:CONTRIBUTING.es.md
 [FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
 [JA]:CONTRIBUTING.ja.md
 [KO_KR]:CONTRIBUTING.ko_kr.md
 [KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
 [NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
 [PT_BR]:CONTRIBUTING.pt_br.md
 [TR]:CONTRIBUTING.tr.md
 [ZH_CN]:CONTRIBUTING.zh_cn.md
 [ZH_TW]:CONTRIBUTING.zh_tw.md
+[TR]:CONTRIBUTING.tr.md
+[ZH_CN]:CONTRIBUTING.zh_cn.md
+[ZH_TW]:CONTRIBUTING.zh_tw.md
 
 Koda xwerû di vê depoyê de ji kaxezek çapkirî bi awak destkî hat dîjîtîzkirin, ji ber vê yekê nakokî û cudahiyên din bi şaşî hatine danîn. Pêdivîye ku kod bêne guhertin da ku li gorî çapên şandî li hev bikin:
 

CONTRIBUTING.lt.md

@@ -0,0 +1,152 @@
+# Prisidėjimas
+
+🎌
+[Čeština][CZ],
+[Deutsch][DE],
+[English][EN],
+[Español][ES],
+[Français][FR],
+[Italiano][IT],
+[Kurdi][KU],
+**Lietuvių**,
+[Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
+[Português][PT_BR],
+[Türkçe][TR],
+[Ελληνικά][GR],
+[العربية][AR],
+[日本語][JA],
+[正體中文][ZH_TW],
+[简体中文][ZH_CN],
+[한국어][KO_KR]
+
+[AR]:CONTRIBUTING.ar.md
+[CZ]:CONTRIBUTING.cz.md
+[DE]:CONTRIBUTING.de.md
+[EN]:CONTRIBUTING.md
+[ES]:CONTRIBUTING.es.md
+[FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
+[JA]:CONTRIBUTING.ja.md
+[KO_KR]:CONTRIBUTING.ko_kr.md
+[KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
+[NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
+[PT_BR]:CONTRIBUTING.pt_br.md
+[TR]:CONTRIBUTING.tr.md
+[ZH_CN]:CONTRIBUTING.zh_cn.md
+[ZH_TW]:CONTRIBUTING.zh_tw.md
+
+Šios saugyklos kodas buvo suskaitmenintas rankiniu būdu iš popierinių spausdinių, todėl galima tikėtis klaidų ir kiti neatitikimų. Kodas turi būti pakeistas taip, kad labiau atitiktų šiuos nuskaitytus spausdinius:
+
+- [AGC spausdiniai Comache][8]
+- [AGC spausdiniai Luminary][9]
+
+## Naudingi plėtiniai
+
+GitHub turi integruotą AGC assemblerio kalbos sintakės palaikymą. Dėja, jūsų kodo redaktorius šios assemblerio kalbos nepalaikys, tačiau yra AGC kalbos plėtinių, kurie suteikia sintakės paryškinimą šiems redaktoriams:
+
+- [Atom][Atom]†
+- [CodeBlocks][CodeBlocks]
+- [Eclipse][Eclipse]
+- [Kate][Kate]
+- [ProgrammersNotepad][ProgrammersNotepad]
+- [Sublime Text 3][Sublime Text]†
+- [TextPad][TextPad]
+- [Vim][Vim]
+- [Visual Studio Code][VisualStudioCode]†
+- [jEdit][jEdit]
+
+† Palaiko automatinį formatavimą
+
+[Atom]:https://github.com/Alhadis/language-agc
+[CodeBlocks]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/CodeBlocks
+[Eclipse]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/Eclipse
+[Kate]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/Kate
+[ProgrammersNotepad]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/ProgrammersNotepad
+[Sublime Text]:https://github.com/jimlawton/AGC-Assembly
+[TextPad]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/TextPad
+[Vim]:https://github.com/wsdjeg/vim-assembly
+[VisualStudioCode]:https://github.com/wopian/agc-assembly
+[jEdit]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/jEdit
+
+## Formatavimas
+
+**Pastaba:** GitHub ir plėtiniai nurodyti viršuje automatiškai užtikrins, kad naudotumėte teisingą formatavimą.
+
+- Naudokite skirtuko įtrauką
+- Naudokite skirtuko plotį 8
+- Ištrinkite galinius tarpus
+
+## Ką aš turiu patikrinti?
+
+Betkokius neatitikimus tarp skenuočių ir šaltinio kodo šioje saugykloje.
+
+### Komentarai
+
+- Komentarai perrašytame kode turi **tiksliai** atitikti skenuočių komentarus.
+
+Dažnai pasikartojančios problemos, į kurias turėtumėte atkreipti dėmesį, jomis neapsiribojant:
+
+#### Tipografinės klaidos
+
+Kai kuriose vietose, rašant komentarus, originalūs kūrėjai paliko tipografinių klaidų. Kai kurios iš jų buvo klaidingai ištaisytos per pradinį skaitmenizavimą, tačiau skaitmenizavimas taip pat pridėjo tipografinių klaidų, kurių nebuvo skenuotėse.
+
+Pavyzdžiui, jeigu skaitmenizuotas komentaras turėjo žodį `SPACECRAFT`, bet `SPAECRAFT` buvo išspausdintas skenuotėse, tai ši skaitmenizacija **turi** būti pataisyta į `SPAECRAFT` (be `C`).
+
+Taip pat, jeigu žodis turi klaidą skaitmenizacijoje, bet yra parašytas teisingai skenuotėse, tai ta klaida **turi** būti pataisyta.
+
+### Tarpai
+
+- Tarpai tarp dviejų rašmenų komentaruose **turi** atitikti skenuotes. Dažnu atvėju (žiūrėti diskusiją [#316][10]), tai yra:
+  - Vienas tarpas naujiems žodžiams.
+  - Dvigubas tarpas naujiems sakiniams.
+  - Trigubas tarpas įtraukoms.
+
+Nevisi puslapiai skenuotėse laikosi šių taisykių, jeigu skenuotės turi tik vieną tarpą vietoj dvigubo tarpo, reikia naudoti vieną tarpą.
+
+### Eilučių lūžiai
+
+- Linijų lūžiai su *pločiu* `R0000` pirmame stulpelyje turi tiksliai atitikti skenuotes.
+- Linijų lūžiai su *pločiu**__out__* `R0000` pirmame stulpelyje gali turėti tik vieną arba dvi tuščias eilutes iš eilės.
+  - Jeigu yra daugiau negu dvi tuščios linijos, reikia ištrinti papildomas eilutes.
+    - Linijos su `R0000` pirmame stulpelyje nesiskaičiuoja.
+  - Šaltinių nuotraukose, šios buvo sukurtos nespausdintu skaitmeniu aštuntame stulpelyje. A 2 - ten buvo dvigubas tarpas (viena tuščia eilutė) ir a 3 buvo trigubas tarpas (dviguba tuščia eilutė). Reikšmės nuo 4-8 buvo apibrėžtos, bet niekada nenaudotos. Daugiau apie tai [#159][7]
+
+Pavyzdžiui, šis tekstas:
+
+```plain
+R0819   SUBROUTINE TO SKIP...
+R0820
+
+
+
+ 0821   LAMPTEST  CS  IMODES33
+```
+
+Turėtų patapti:
+
+```plain
+R0819   SUBROUTINE TO SKIP...
+R0820
+
+
+ 0820   LAMPTEST  CS  IMODES33
+```
+
+## Pastabos
+
+Prieš kuriant PR, prašome įsitikinti, kad jūsų pakeitimai atitinka skenuotes!
+
+[0]:https://github.com/chrislgarry/Apollo-11/pull/new/master
+[1]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/
+[2]:http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/
+[6]:https://github.com/wopian/agc-assembly#user-settings
+[7]:https://github.com/chrislgarry/Apollo-11/issues/159
+[8]:http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/
+[9]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/
+[10]:https://github.com/chrislgarry/Apollo-11/pull/316#pullrequestreview-102892741

CONTRIBUTING.md

@@ -6,10 +6,15 @@
 **English**,
 [Español][ES],
 [Français][FR],
+[Italiano][IT],
 [Kurdi][KU],
+[Lietuvių][LT],
 [Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
 [Português][PT_BR],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [العربية][AR],
 [日本語][JA],
 [正體中文][ZH_TW],
@@ -22,16 +27,21 @@
 [EN]:CONTRIBUTING.md
 [ES]:CONTRIBUTING.es.md
 [FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
 [JA]:CONTRIBUTING.ja.md
 [KO_KR]:CONTRIBUTING.ko_kr.md
 [KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
 [NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
 [PT_BR]:CONTRIBUTING.pt_br.md
 [TR]:CONTRIBUTING.tr.md
 [ZH_CN]:CONTRIBUTING.zh_cn.md
 [ZH_TW]:CONTRIBUTING.zh_tw.md
 
-The source code in this repository was digitized manually from paper printouts, so typos and other discrepancies have been introduced accidentally. The code shall be modified to be made consistent with the scanned printouts:
+The source code in this repository was digitized manually from paper printouts, so typos and other discrepancies have been introduced accidentally. The code shall be modified to be made consistent with the following scanned printouts:
 
 - [AGC printouts for Comanche][8]
 - [AGC printouts for Luminary][9]
@@ -74,12 +84,31 @@ GitHub has syntax support for the AGC assembly language built-in. Unfortunately
 
 ## What do I check?
 
-Any discrepancies between the scans and the source code in this repository, including:
+Any discrepancies between the scans and the source code in this repository.
 
 ### Comments
 
-- Comments in the transcribed code should match the scans exactly
-  - This could involve creating a deliberate typo or removing/adding an entire comment.
+Comments in the transcribed code **MUST** match the scans **exactly**.
+
+Common issues you should look out for while proofing include, but not limited to:
+
+#### Typographic Errors
+
+In some places, the original developers made typographic errors while writing comments. Some of these were mistakenly corrected during the initial digitisation, however the digitisation has also introduced typographic errors that were not present in the scans.
+
+For example, if the digitised comments contained `SPACECRAFT`, but `SPAECRAFT` was printed in the scans, then the digitisation **MUST** be corrected to `SPAECRAFT` (missing `C`).
+
+Likewise, if a word has a typo in the digitisation but is spelt correctly in the scans then the typo **MUST** be corrected.
+
+#### Spaces
+
+Spaces between two characters in comments **SHOULD** match the scans. In most cases (see the discussion in [#316][10]), this is:
+
+- Single space for new words.
+- Double space for new sentences.
+- Triple space for indentations.
+
+Not all pages in the scans follow this generalisation, if the scans only have a single space instead of a double space, use a single space.
 
 ### Line breaks
 
@@ -110,27 +139,6 @@ R0820
  0820   LAMPTEST  CS  IMODES33
 ```
 
-### Spaces
-
-- Spaces between two characters in the string should respect the following convention (see the discussion in [#316][10]):
-  - Single space for new words.
-  - Double space for new sentences.
-  - Triple space for indentations.
-
-For example the following:
-
-```plain
-	1)  FOO BAR BAZ QUX QUUX QUUZ. CORGE, GRAULT,
-	GARPLY, WALDO.
-```
-
-Should become:
-
-```plain
-	1) FOO BAR BAZ QUX QUUX QUUZ.  CORGE, GRAULT,
-	   GARPLY, WALDO.
-```
-
 ## Note
 
 Before you make a PR, please make sure your changes are consistent with the scans!

CONTRIBUTING.nl.md

@@ -6,10 +6,15 @@
 [English][EN],
 [Español][ES],
 [Français][FR],
+[Italiano][IT],
 [Kurdi][KU],
+[Lietuvių][LT],
 **Nederlands**,
+[Norsk][NO],
+[Polski][PL],
 [Português][PT_BR],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [العربية][AR],
 [日本語][JA],
 [正體中文][ZH_TW],
@@ -22,14 +27,19 @@
 [EN]:CONTRIBUTING.md
 [ES]:CONTRIBUTING.es.md
 [FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
 [JA]:CONTRIBUTING.ja.md
 [KO_KR]:CONTRIBUTING.ko_kr.md
 [KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
+[NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
 [PT_BR]:CONTRIBUTING.pt_br.md
 [TR]:CONTRIBUTING.tr.md
 [ZH_CN]:CONTRIBUTING.zh_cn.md
 [ZH_TW]:CONTRIBUTING.zh_tw.md
-[NL]:CONTRIBUTING.nl.md
 
 De broncode in deze repository is handmatig gedigitalizeerd van papieren stukken. Typfouten en andere discrepanties kunnen per ongeluk zijn toegevoegd. De code zal worden aangepast om gelijk te worden gemaakt aan de gescande papieren:
 
@@ -38,7 +48,7 @@ De broncode in deze repository is handmatig gedigitalizeerd van papieren stukken
 
 ## Handige extensies
 
-Github heeft syntax ondersteuning voor de AGC assembly taal ingebouwd. Helaas heeft jouw editor dit niet, gelukkig zijn er AGC extensies die de volgende editors kunnen voorzien van syntax ondersteuning:
+GitHub heeft syntax ondersteuning voor de AGC assembly taal ingebouwd. Helaas heeft jouw editor dit niet, gelukkig zijn er AGC extensies die de volgende editors kunnen voorzien van syntax ondersteuning:
 
 - [Atom][Atom]†
 - [CodeBlocks][CodeBlocks]

CONTRIBUTING.no.md

@@ -0,0 +1,153 @@
+# Bidra
+
+🎌
+[Čeština][CZ],
+[Deutsch][DE],
+[English][EN],
+[Español][ES],
+[Français][FR],
+[Italiano][IT],
+[Kurdi][KU],
+[Lietuvių][LT],
+[Nederlands][NL],
+**Norsk**,
+[Polski][PL],
+[Português][PT_BR],
+[Türkçe][TR],
+[Ελληνικά][GR],
+[العربية][AR],
+[日本語][JA],
+[正體中文][ZH_TW],
+[简体中文][ZH_CN],
+[한국어][KO_KR]
+
+[AR]:CONTRIBUTING.ar.md
+[CZ]:CONTRIBUTING.cz.md
+[DE]:CONTRIBUTING.de.md
+[EN]:CONTRIBUTING.md
+[ES]:CONTRIBUTING.es.md
+[FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
+[JA]:CONTRIBUTING.ja.md
+[KO_KR]:CONTRIBUTING.ko_kr.md
+[KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
+[NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
+[PT_BR]:CONTRIBUTING.pt_br.md
+[TR]:CONTRIBUTING.tr.md
+[ZH_CN]:CONTRIBUTING.zh_cn.md
+[ZH_TW]:CONTRIBUTING.zh_tw.md
+
+Kilde koden I dette «repository» var digitalisert manuelt ifra papir utskrifter, om det finnes stavefeil og andre avvik skall koden reflektere dette. Skrivefeil og andre avvik kan ha blitt innført ved et uhell men skal allikevel være identisk med følgende digitalisert papir utskrifter:
+
+- [AGC utskrift for Comanche][8]
+- [AGC utskrift for Luminary][9]
+
+## Nytteprogrammer
+
+GitHub har kildekode støtte for «assembly» programmerings språket AGC ( innebygget ), og de følgene tekst redigerings programmene har også støtte for nøkkel ord fargesetting:
+
+- [Atom][Atom]†
+- [CodeBlocks][CodeBlocks]
+- [Eclipse][Eclipse]
+- [Kate][Kate]
+- [ProgrammersNotepad][ProgrammersNotepad]
+- [Sublime Text 3][Sublime Text]†
+- [TextPad][TextPad]
+- [Vim][Vim]
+- [Visual Studio Code][VisualStudioCode]†
+- [jEdit][jEdit]
+
+† Supporterer automatisk formattering
+
+[Atom]:https://github.com/Alhadis/language-agc
+[CodeBlocks]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/CodeBlocks
+[Eclipse]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/Eclipse
+[Kate]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/Kate
+[ProgrammersNotepad]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/ProgrammersNotepad
+[Sublime Text]:https://github.com/jimlawton/AGC-Assembly
+[TextPad]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/TextPad
+[Vim]:https://github.com/wsdjeg/vim-assembly
+[VisualStudioCode]:https://github.com/wopian/agc-assembly
+[jEdit]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/jEdit
+
+## Formattering
+
+**Merk:** GitHub og redigerings programmene nevnt ovenfor vil sørge for at du bruker korrekt formattering av kilde koden.
+
+-	Bruk Tab for innrykk
+-	Bruk Tab med 8 mellomrom
+-	Ta bort mellomrom og annet som ikke er synlig på slutten av setninger
+
+## Hva må jeg sjekke?
+
+Eventuelle avvik ifra de innskannede bildene og kilde koden i dette «repository»
+
+### Kommentarer
+
+Kommentarer i denne koden **SKAL** stemme **eksakt** med den digitaliserte originalen.
+
+Vanlige feil en bør se etter er blant annet:
+
+#### Typografiske feil
+
+Noen steder skrev original utvikleren feil i kode kommentarene. Noen av disse feilene ble rettet under digitaliseringen, og digitaliseringen har også introdusert nye typografiske feil som ikke kommer ifra papir utskriften.
+
+For eksempel, om de originale dokumentene var feilstavet til ‘SPAECRAFT’ og de digitaliserte dokumentene ble endret til ‘SPACECRAFT’ så **SKAL** dette rettes til og reflektere de originale dokumentene, altså uten ‘C’ i ordet.
+
+På samme måte, om digitaliseringen introduserte stavefeil som ikke var tilstede i de originale dokumentene **SKAL** dette rettes.
+
+#### Mellomrom
+
+Mellomrom mellom to karakterer i teksten **BØR** følge de digitaliserte dokumentene. I de fleste tilfeller (se diskusjon i [#316[10]) betyr dette:
+
+- Enkelt mellomrom for nye ord
+- Dobbelt mellomrom for nye linjer
+- Trippel mellomrom for innrykk
+
+Ikke alle sider i de digitaliserte dokumentene følger denne generaliseringen, så om de digitaliserte dokumentene bruker enkelt mellomrom i stedet for dobbelt mellomrom så skal enkelt mellomrom følges.
+
+### Linje Skift
+
+- Linje skift *med* `R0000` i kolonne 1 skal stemme helt med originalen.
+- Linje skift *uten* `R0000` i kolonne 1 skal bare ha en eller to blanke linjer etter seg.
+  - Om det er flere enn to blanke linjer skal de fjernes
+    - Linjer med `R0000` i kolonne 1 regnes ikke i slike tilfeller
+  - I originalen ble disse skapt av et uskrevet tegn i kolonne 8. Sto det 2 der var der et dobbelt mellomrom ( enkel blank linje ) og om det var 3 så ble det et trippel mellomrom ( to dobble linjer ). Verdiene ifra 4 til 8 var definert, men er ikke i bruk. Les mer om dette i [#159][7]
+
+For eksempel skal følgende kode:
+
+```plain
+R0819   SUBROUTINE TO SKIP...
+R0820
+
+
+
+ 0821   LAMPTEST  CS  IMODES33
+```
+
+Se slik ut:
+
+```plain
+R0819   SUBROUTINE TO SKIP...
+R0820
+
+
+ 0820   LAMPTEST  CS  IMODES33
+```
+
+## Noter
+
+Før en gjør en «Pull Request» bør man være helt sikker på at forandringer er helt lik de digitaliserte bildene!
+
+[0]:https://github.com/chrislgarry/Apollo-11/pull/new/master
+[1]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/
+[2]:http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/
+[6]:https://github.com/wopian/agc-assembly#user-settings
+[7]:https://github.com/chrislgarry/Apollo-11/issues/159
+[8]:http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/
+[9]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/
+[10]:https://github.com/chrislgarry/Apollo-11/pull/316#pullrequestreview-102892741

CONTRIBUTING.pl.md

@@ -0,0 +1,153 @@
+# Contributing
+
+🎌
+[Čeština][CZ],
+[Deutsch][DE],
+[English][EN],
+[Español][ES],
+[Français][FR],
+[Italiano][IT],
+[Kurdi][KU],
+[Lietuvių][LT],
+[Nederlands][NL],
+[Norsk][NO],
+**Polski**,
+[Português][PT_BR],
+[Türkçe][TR],
+[Ελληνικά][GR],
+[العربية][AR],
+[日本語][JA],
+[正體中文][ZH_TW],
+[简体中文][ZH_CN],
+[한국어][KO_KR]
+
+[AR]:CONTRIBUTING.ar.md
+[CZ]:CONTRIBUTING.cz.md
+[DE]:CONTRIBUTING.de.md
+[EN]:CONTRIBUTING.md
+[ES]:CONTRIBUTING.es.md
+[FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
+[JA]:CONTRIBUTING.ja.md
+[KO_KR]:CONTRIBUTING.ko_kr.md
+[KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
+[NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
+[PT_BR]:CONTRIBUTING.pt_br.md
+[TR]:CONTRIBUTING.tr.md
+[ZH_CN]:CONTRIBUTING.zh_cn.md
+[ZH_TW]:CONTRIBUTING.zh_tw.md
+
+Kod źródłowy w tym repozytorium został zdigitalizowany ręcznie na podstawie wydruków papierowych, więc literówki i inne rozbieżności zostały wprowadzone przypadkowo. Kod należy zmodyfikować, aby był zgodny z zeskanowanymi wydrukami:
+
+- [AGC printouts for Comanche][8]
+- [AGC printouts for Luminary][9]
+
+## Przydatne rozszerzenia
+
+GitHub obsługuje składnię wbudowanego języka asemblera AGC. Niestety twój edytor kodu prawdopodobnie nie będzie go obsługiwał, jednak istnieją rozszerzenia języka AGC, które zapewniają obsługę składni tego języka dla następujących edytorów:
+
+- [Atom][Atom]†
+- [CodeBlocks][CodeBlocks]
+- [Eclipse][Eclipse]
+- [Kate][Kate]
+- [ProgrammersNotepad][ProgrammersNotepad]
+- [Sublime Text 3][Sublime Text]†
+- [TextPad][TextPad]
+- [Vim][Vim]
+- [Visual Studio Code][VisualStudioCode]†
+- [jEdit][jEdit]
+
+† Wspiera automatyczne formatowanie
+
+[Atom]:https://github.com/Alhadis/language-agc
+[CodeBlocks]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/CodeBlocks
+[Eclipse]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/Eclipse
+[Kate]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/Kate
+[ProgrammersNotepad]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/ProgrammersNotepad
+[Sublime Text]:https://github.com/jimlawton/AGC-Assembly
+[TextPad]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/TextPad
+[Vim]:https://github.com/wsdjeg/vim-assembly
+[VisualStudioCode]:https://github.com/wopian/agc-assembly
+[jEdit]:https://github.com/virtualagc/virtualagc/tree/master/Contributed/SyntaxHighlight/jEdit
+
+## Formatowanie
+
+**Uwaga:** GitHub wraz z powyższymi rozszerzeniami zapewniają automatyczne użycie prawidłowego formatowana
+
+- Tabulacja
+- Szerokość tabulacji wynosząca 8
+- Niepozostawianie spacji na końcu wierszy
+
+## Co mam sprawdzać?
+
+Wszelkie rozbieżności między skanami a kodem źródłowym tego repozytorium.
+
+### Komentarze
+
+Komentarze w transkrybowanym kodzie **MUSZĄ DOKŁADNIE** odpowiadać skanom.
+
+Typowe problemy, na które należy zwrócić uwagę podczas sprawdzania, obejmują między innymi:
+
+#### Literówki
+
+W niektórych miejscach pierwotni programiści popełnili błędy typograficzne podczas pisania komentarzy. Niektóre z nich zostały błędnie poprawione podczas wstępnej digitalizacji, jednak digitalizacja wprowadziła również błędy typograficzne, których nie było w skanach.
+
+Na przykład, jeśli zdigitalizowane komentarze zawierały słowo „SPACECRAFT”, ale na skanach odczytano „SPAECRAFT”, wówczas digitalizacja **MUSI** zostać poprawiona na „SPAECRAFT” (brakujące „C”).
+
+Podobnie, jeśli słowo zawiera literówkę w digitalizacji, ale jest poprawnie napisane na skanach, wówczas literówka **MUSI** zostać poprawiona.
+
+#### Spacje
+
+Spacje pomiędzy dwoma znakami w danym ciągu powinny być zgodne z następującą konwencją (patrz na [#316][10]):
+
+- Pojedyńcza spacja dla nowego słowa.
+- Podwójna spacja dla nowego zdania.
+- Potrójna spacja dla akapitu.
+
+Nie wszystkie strony w skanach są zgodne z tym uogólnieniem, jeśli skany mają tylko jedną spację zamiast podwójnej, użyj jednej spacji.
+
+### Rozdzielanie wierszy
+
+- Wiersz *rozpoczynający się od* `R0000` w kolumnie 1 powinien dokładnie pasować do skanów.
+- Wiersz *nierozpoczynający się od* `R0000` w kolumnie 1 powinien zawierać tylko 1 lub 2 puste wiersze z rzędu.
+  - Jeżeli są więcej niż 2 puste wiersze - usuń ich nadmiar.
+    - Wiersze rozpoczynające się od `R0000` w kolumnie 1 nie są zaliczane jako pusty wiersz.
+  - W obrazach źródłowych puste linie zostały utworzone przez niezadrukowaną cyfrę w kolumnie 8. 2 wymusiło podwójną spację (pojedyncza pusta linia), a 3 wymusiło potrójną spację (podwójna pusta linia). Wartości 4-8 zostały zdefiniowane, ale nigdy nie były używane. Więcej na ten temat w [#159][7]
+
+Na przykład:
+
+```plain
+R0819   SUBROUTINE TO SKIP...
+R0820
+
+
+
+ 0821   LAMPTEST  CS  IMODES33
+```
+
+Zostaje zmienione na:
+
+```plain
+R0819   SUBROUTINE TO SKIP...
+R0820
+
+
+ 0820   LAMPTEST  CS  IMODES33
+```
+
+## Uwaga
+
+Zanim utworzysz PR, upewnij się, że zmiany są zgodne ze skanami!
+
+[0]:https://github.com/chrislgarry/Apollo-11/pull/new/master
+[1]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/
+[2]:http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/
+[6]:https://github.com/wopian/agc-assembly#user-settings
+[7]:https://github.com/chrislgarry/Apollo-11/issues/159
+[8]:http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/
+[9]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/
+[10]:https://github.com/chrislgarry/Apollo-11/pull/316#pullrequestreview-102892741

CONTRIBUTING.pt_br.md

@@ -6,10 +6,15 @@
 [English][EN],
 [Español][ES],
 [Français][FR],
+[Italiano][IT],
 [Kurdi][KU],
+[Lietuvių][LT],
 [Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
 **Português**,
 [Türkçe][TR],
+[Ελληνικά][GR],
 [العربية][AR],
 [日本語][JA],
 [正體中文][ZH_TW],
@@ -22,10 +27,15 @@
 [EN]:CONTRIBUTING.md
 [ES]:CONTRIBUTING.es.md
 [FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
 [JA]:CONTRIBUTING.ja.md
 [KO_KR]:CONTRIBUTING.ko_kr.md
 [KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
 [NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
 [PT_BR]:CONTRIBUTING.pt_br.md
 [TR]:CONTRIBUTING.tr.md
 [ZH_CN]:CONTRIBUTING.zh_cn.md
@@ -38,7 +48,7 @@ O código-fonte neste repositório foi digitado manualmente a partir de impress
 
 ## Extensões úteis
 
-Github possui suporte de sintaxe nativo para a linguagem assembly AGC.
+GitHub possui suporte de sintaxe nativo para a linguagem assembly AGC.
 Infelizmente, seu editor de texto não o terá. Portanto, existem extensões para a linguagem AGC que providenciam destaque de sintaxe para os seguintes editores:
 
 - [Atom][Atom]†
@@ -67,7 +77,7 @@ Infelizmente, seu editor de texto não o terá. Portanto, existem extensões par
 
 ## Formatando
 
-**Nota:** Github e as três extensões listadas acima garantirão que você estará usando a formatação correta automaticamente.
+**Nota:** GitHub e as três extensões listadas acima garantirão que você estará usando a formatação correta automaticamente.
 
 - Use indentação por tab
 - Use largura de tab em 8

CONTRIBUTING.tr.md

@@ -6,10 +6,15 @@
 [English][EN],
 [Español][ES],
 [Français][FR],
+[Italiano][IT],
 [Kurdi][KU],
+[Lietuvių][LT],
 [Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
 [Português][PT_BR],
 **Türkçe**,
+[Ελληνικά][GR],
 [العربية][AR],
 [日本語][JA],
 [正體中文][ZH_TW],
@@ -22,10 +27,15 @@
 [EN]:CONTRIBUTING.md
 [ES]:CONTRIBUTING.es.md
 [FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
 [JA]:CONTRIBUTING.ja.md
 [KO_KR]:CONTRIBUTING.ko_kr.md
 [KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
 [NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
 [PT_BR]:CONTRIBUTING.pt_br.md
 [TR]:CONTRIBUTING.tr.md
 [ZH_CN]:CONTRIBUTING.zh_cn.md
@@ -38,7 +48,7 @@ Bu repodaki kaynak kodu kağıt çıktılarından elle dijitalleştirilmiştir.
 
 ## Yararlı Eklentiler
 
-Github, AGC assembly dili için sentaks desteği sağlıyor ama sizin kodu düzenlemek için kullandığınız editör sağlamayacaktır. Aşağıdaki editörler AGC dili sentaks vurgulaması için eklentiler sunmaktadır:
+GitHub, AGC assembly dili için sentaks desteği sağlıyor ama sizin kodu düzenlemek için kullandığınız editör sağlamayacaktır. Aşağıdaki editörler AGC dili sentaks vurgulaması için eklentiler sunmaktadır:
 
 - [Atom][Atom]†
 - [CodeBlocks][CodeBlocks]
@@ -74,12 +84,31 @@ Github, AGC assembly dili için sentaks desteği sağlıyor ama sizin kodu düze
 
 ## Neyi kontrol edeyim?
 
-Taratılmış çıktılar ve bu repodaki kaynak kodu arasındaki aşağıdakileri kapsayan herhangi bir tutarsızlığı:
+Taratılmış çıktılar ve bu repodaki kaynak kodu arasındaki herhangi bir tutarsızlığı.
 
 ### Yorumlar
 
-- Uyarlanan koddaki yorum satırları, çıktılar ile tamamen eşleşmelidir
-  - Bu bilerek yazım hatası koymayı veya bir yorumun tamamını kaldırıp/eklemeyi içerebilir.
+Uyarlanan koddaki yorum satırları, çıktılar ile **tamamen** **eşleşmelidir**.
+
+Düzeltmek için bakmanız gereken bazı temel sorunlar şunlardır:
+
+#### Yazım Hataları
+
+Bazı yerlerde, orijinal geliştiriciler yorum yazarken yazım hataları yapmış. Bunların bazıları dijitalleştirme sürecinin başlarında yanlışlıkla düzeltildi fakat dijitalleştirme süreci taratılmış çıktılarda olmayan yeni yazım hatalarına da sebep oldu.
+
+Örneğin, dijitalleştirilmiş yorumlar `SPACECRAFT` kelimesini içeriyorsa ama taratılmış çıktılarda `SPAECRAFT` yazıyorsa, dijitalleştirilmiş yorum `SPAECRAFT` (`C` eksik) olarak **düzeltilmelidir**.
+
+Aynı şekilde, eğer dijitalleştirmiş yorumlarda bir yazım hatası varsa ama taratılmış çıktılarda doğru yazılmışsa, yazım hatası **düzeltilmelidir**.
+
+### Boşluklar
+
+Yorumlar arasındaki iki karakterin arasındaki boşluklar taratılmış çıktılar ile **uyuşmalıdır**. Bir çok durumda ([#316][10]'daki tartışmayı inceleyin) boşluklar şu şekildedir:
+
+- Yeni kelimeler arası tek boşluk.
+- Yeni cümleler arası iki boşluk.
+- Yeni girintiler için üç boşluk.
+
+Taratılmış çıktılarda bütün sayfalar bu genellemelere uymaz. Eğer çıktılarda iki boşluk yerine bir boşluk varsa, bir boşluk kullanın.
 
 ### Satır sonları
 
@@ -87,7 +116,7 @@ Taratılmış çıktılar ve bu repodaki kaynak kodu arasındaki aşağıdakiler
 - Birinci sütunu `R0000` *__olmadan__* biten satır sonları arka arkaya sadece 1 ya da 2 boş satır içermelidir.
   - Eğer 2'den fazla satır sonu varsa ekstra olan satır sonlarını kaldırın.
     - Birinci sütunu `R0000` *ile* biten satırlar bu kural dahilinde değildir.
-  - Kaynak resimlerde bunlar 8. satırındaki basamak bastırılmamış halde oluşturulmuştur. Bir 2 kullanımı iki boşluğu (tek boş satırı) temsil ederken, bir 3 kullanımı üç boşluğu (iki boş satırı) ifade eder. 4 ve 8 tanımlanmıştır fakat hiç kullanılmamıştır. Bunun hakkında daha fazla okumak için: [#159][7].
+  - Kaynak resimlerde bunlar 8. satırındaki basamak bastırılmamış halde oluşturulmuştur. Bir 2 kullanımı iki boşluğu (tek boş satırı) temsil ederken, bir 3 kullanımı üç boşluğu (iki boş satırı) ifade eder. 4 ve 8 tanımlanmıştır fakat hiç kullanılmamıştır. Bunun hakkında daha fazla okumak için: [#159][7]
 
 Örneğin bu:
 
@@ -110,27 +139,6 @@ R0820
  0820   LAMPTEST  CS  IMODES33
 ```
 
-### Boşluklar
-
-- Bir string'deki iki karakterin arasındaki boşluklar şu kurallara uymalıdır ([#316][10]'daki tartışmayı inceleyin):
-  - Yeni kelimeler arası tek boşluk.
-  - Yeni cümleler arası iki boşluk.
-  - Yeni girintiler için üç boşluk.
-
-Örneğin bu:
-
-```plain
-	1)  FOO BAR BAZ QUX QUUX QUUZ. CORGE, GRAULT,
-	GARPLY, WALDO.
-```
-
-Buna dönüşmeli:
-
-```plain
-	1) FOO BAR BAZ QUX QUUX QUUZ.  CORGE, GRAULT,
-	   GARPLY, WALDO.
-```
-
 ## Not
 
 PR yapmadan önce lütfen yaptığınız değişikliklerin çıktılar ile tutarlı olduğundan emin olun!

CONTRIBUTING.zh_cn.md

@@ -6,10 +6,15 @@
 [English][EN],
 [Español][ES],
 [Français][FR],
+[Italiano][IT],
 [Kurdi][KU],
+[Lietuvių][LT],
 [Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
 [Português][PT_BR],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [العربية][AR],
 [日本語][JA],
 [正體中文][ZH_TW],
@@ -22,10 +27,15 @@
 [EN]:CONTRIBUTING.md
 [ES]:CONTRIBUTING.es.md
 [FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
 [JA]:CONTRIBUTING.ja.md
 [KO_KR]:CONTRIBUTING.ko_kr.md
 [KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
 [NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
 [PT_BR]:CONTRIBUTING.pt_br.md
 [TR]:CONTRIBUTING.tr.md
 [ZH_CN]:CONTRIBUTING.zh_cn.md

CONTRIBUTING.zh_tw.md

@@ -6,10 +6,15 @@
 [English][EN],
 [Español][ES],
 [Français][FR],
+[Italiano][IT],
 [Kurdi][KU],
+[Lietuvių][LT],
 [Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
 [Português][PT_BR],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [العربية][AR],
 [日本語][JA],
 **正體中文**,
@@ -22,10 +27,15 @@
 [EN]:CONTRIBUTING.md
 [ES]:CONTRIBUTING.es.md
 [FR]:CONTRIBUTING.fr.md
+[GR]:CONTRIBUTING.gr.md
+[IT]:CONTRIBUTING.it.md
 [JA]:CONTRIBUTING.ja.md
 [KO_KR]:CONTRIBUTING.ko_kr.md
 [KU]:CONTRIBUTING.ku.md
+[LT]:CONTRIBUTING.lt.md
 [NL]:CONTRIBUTING.nl.md
+[NO]:CONTRIBUTING.no.md
+[PL]:CONTRIBUTING.pl.md
 [PT_BR]:CONTRIBUTING.pt_br.md
 [TR]:CONTRIBUTING.tr.md
 [ZH_CN]:CONTRIBUTING.zh_cn.md
@@ -38,7 +48,7 @@
 
 ## 實用套件
 
-GitHub 內建 AGC 組語語法支援，但你的編輯器本身並沒有。不過，某些編輯器有提供 AGC 語法突顯的語言套件：
+GitHub 內建 AGC 組語語法支援，但你的編輯器本身並沒有。不過，以下編輯器有提供 AGC 語法突顯的語言套件：
 
 - [Atom][Atom]†
 - [CodeBlocks][CodeBlocks]
@@ -66,7 +76,7 @@ GitHub 內建 AGC 組語語法支援，但你的編輯器本身並沒有。不
 
 ## 格式化
 
-**注意：**GitHub 與上面列出的套件，會自動確保您使用正確的格式。
+**注意：** GitHub 與上面列出的套件，會自動確保您使用正確的格式。
 
 - 用 tab 縮排
 - tab 寬度為 8
@@ -78,8 +88,27 @@ GitHub 內建 AGC 組語語法支援，但你的編輯器本身並沒有。不
 
 ### 註解
 
-- 抄寫的註解要和掃描一模一樣。
-  - 這包括刻意的拼寫錯誤、或是刪除/增加整個註解。
+抄寫的註解**必須**和掃描**一模一樣**。
+
+在檢查程式時需要留心，但不限於的問題有：
+
+#### 拼寫錯誤
+
+有時候，原始程式的開發者會撰寫時，出現若干拼寫錯誤。有時可能會在初次數位化時，被錯誤地更正；不過數位化本身，也可能產出在原始稿沒出現的拼寫錯誤。
+
+比方說，數位化的註解如果是 `SPACECRAFT`、但掃描原稿是 `SPAECRAFT` 的話，數位化就**必須**更正為沒有 C 的 `SPAECRAFT`。
+
+同樣地，如果是數位化的註解錯了、但掃描稿正確的話，就**必須**更正數位化的程式。
+
+#### 空格
+
+在字元內，兩個單字之間的空白**必須**與掃描相同。大多數時（請參閱 [#316][10] 的討論）慣例如下：
+
+- 單字間空一格。
+- 句子間空兩格。
+- 縮排間空三格。
+
+不是所有掃描都遵照這個慣例。如果不空兩格，而是空一格，那就空一格。
 
 ### 換行
 
@@ -110,27 +139,6 @@ R0820
  0820   LAMPTEST  CS  IMODES33
 ```
 
-### 空白
-
-- 在字元內，兩個單字之間的空白必須遵照以下慣例（請參閱 [#316][10] 的討論）：
-  - 單字間空一格。
-  - 句子間空兩格。
-  - 縮排間空三格。
-
-例如以下程式：
-
-```plain
-	1)  FOO BAR BAZ QUX QUUX QUUZ. CORGE, GRAULT,
-	GARPLY, WALDO.
-```
-
-要改寫成：
-
-```plain
-	1) FOO BAR BAZ QUX QUUX QUUZ.  CORGE, GRAULT,
-	   GARPLY, WALDO.
-```
-
 ## 注意
 
 在發 PR 前，請確保您的修改與掃描輸出一模一樣！

Comanche055/EXTENDED_VERBS.agc

@@ -10,7 +10,7 @@
 # Website:	http://www.ibiblio.org/apollo.
 # Mod history:	2009-05-18 FB	Transcription Batch 3 Assignment.
 #		2009-05-20 RSB	Corrections:  POODOO -> P00DOO,
-#				GOTOPOOH -> GOTOP00H, added a couple of
+#				GOTOPOOH -> GOTOPOOH, added a couple of
 #				missing instructions in Verb 96.
 #		2009-05-23 RSB	In SYSTEST, corrected TC FLAGWRD1 to
 #				CA FLAGWRD1.  Added a variety of SBANK=
@@ -462,7 +462,7 @@ VNLODDT		VN	2524		# V25N24 FOR LOAD DELTA TIME
 
 		COUNT	04/EXTVB
 
-SYSTEST		TC	CHKP00H
+SYSTEST		TC	CHKPOOH
 		CA	FLAGWRD1	# IS NODOP01 FLAGBIT ON? (SET BY P11)
 		MASK	NOP01BIT
 		EXTEND
@@ -524,7 +524,7 @@ CHAZFOGC	TC	CHECKMM		# IS IT PRELAUNCH
 #	   TRANSFER LOADED VALUES TO REGISTERS, AND SEND COMMANDS.
 #	6. IF BUSY FLAG SET, RESET IT TO RELEASE EXT VERB DISPLAY.
 
-IMUATTCK	TC	CHKP00H
+IMUATTCK	TC	CHKPOOH
 
 		CAF	OCTAL30		# CHECK IF IMU ZERO AND IMU COARSE ARE ON
 		EXTEND
@@ -586,7 +586,7 @@ CKLFTBTS	CAF	GRRBKBIT	# HAS LIFTOFF OCCURRED
 XACT0Q		TC	Q		# YES
 
 OCTAL30		OCT	30
-VB64		TC	CHKP00H		# DEMAND PROGRAM 00.
+VB64		TC	CHKPOOH		# DEMAND PROGRAM 00.
 		TC	TESTXACT	# IF DISPLAY SYS. NOT BUSY,MAKE IT BUSY.
 		INHINT
 		CAF	PRIO4
@@ -675,7 +675,7 @@ STABLISH	CAF	EBANK6		# V46 	- SET EBANK TO E6
 #	   C. ENTER
 #	      1. REPEAT FLASHING V06,N22.
 
-CREWMANU	TC	CHKP00H		# DEMAND P00
+CREWMANU	TC	CHKPOOH		# DEMAND P00
 
 		TC	TESTXACT
 
@@ -1004,7 +1004,7 @@ LFTFLGON	TC	UPFLAG		# VB 75 - SET LIFTOFF FLAG BIT
 		TC	GOPIN
 
 # Page 261
-CHKP00H		CA	MODREG
+CHKPOOH		CA	MODREG
 		EXTEND
 		BZF	TCQ
 		TCF	ALM/END
@@ -1058,7 +1058,7 @@ IDLECADR	2CADR	T5IDLOC
 #    TERMINATE-  EXIT R63 ROUTINE
 #    PROCEED-  RESET 3AXISFLG AND CALL R60CSM FOR ATTITUDE MANEUVER.
 
-V89PERF		TC	CHKP00H		# DEMAND P00
+V89PERF		TC	CHKPOOH		# DEMAND P00
 		TC	TESTXACT
 		INHINT
 		CAF	PRIO10
@@ -1078,7 +1078,7 @@ WMATRXNG	TC	DOWNFLAG	# RESET RENDWFLG
 
 GOSHOSUM	EQUALS	SHOWSUM
 
-SHOWSUM		TC	CHKP00H
+SHOWSUM		TC	CHKPOOH
 		TC	TESTXACT	# *
 		CAF	S+1		# *
 		TS	SKEEP6		# * SHOWSUM OPTION

Comanche055/FRESH_START_AND_RESTART.agc

@@ -116,7 +116,7 @@
 #			CADR 	SLAP1
 
 #		ENEMA -	TC 	POSTJUMP	*** DO NOT CALL ENEMA WITHOUT ***
-#			CADR 	ENEMA		*** CONSULTING P00H PEOPLE   ***
+#			CADR 	ENEMA		*** CONSULTING POOH PEOPLE   ***
 
 #	B. OUTPUT
 
@@ -471,7 +471,7 @@ PTBAD		TC	ALARM		# SET ALARM TO SHOW PHASE TABLE FAILURE.
 
 # ******** ****** ******
 #
-# DO NOT USE GOPROG2 OR ENEMA WITHOUT CONSULTING P00H PEOPLE
+# DO NOT USE GOPROG2 OR ENEMA WITHOUT CONSULTING POOH PEOPLE
 #
 GOPROG2		EQUALS	ENEMA
 OCT10000	=	BIT13
@@ -945,12 +945,12 @@ DUMMYAD		EXIT
 		TC	DOWNFLAG
 		ADRES	R21MARK
 
-		CCS	MMNUMBER		# IS THIS A P00H REQUEST
+		CCS	MMNUMBER		# IS THIS A POOH REQUEST
 		TCF	NOUVEAU			# NO, PICK UP NEW PROGRAM
 
 		COUNT	04/P00
 
-P00H		TC	RELDSP			# RELEASE DISPLAY SYSTEM
+POOH		TC	RELDSP			# RELEASE DISPLAY SYSTEM
 
 		CAF	PRIO5			# SET VARIABLE RESTART REGISTER FOR P00.
 		TS	PHSPRDT2
@@ -985,7 +985,7 @@ SEUDOP00	TS	DNLSTCOD		# SET UP APPROPRIATE DOWNLIST.
 GROUPKIL	TC	IBNKCALL		# KILL GROUPS 3(5,6
 		CADR	V37KLEAN
 
-		CCS	MMNUMBER		# IS IT P00H
+		CCS	MMNUMBER		# IS IT POOH
 		TCF	RENDV00			# NO
 # Page 201
 		TC	IBNKCALL

Comanche055/INTEGRATION_INITIALIZATION.agc

@@ -742,13 +742,13 @@ DT/2COMP	DLOAD	DSU
 			GETMAXDT
 		DSU	BMN		# IS TIME TO INTEG. TO GR THAN MAXTIME
 			12D
-			P00HCHK
+			POOHCHK
 USEMAXDT	DLOAD	SIGN
 			12D
 			DT/2
 # Page 1324
 		STCALL	DT/2
-			P00HCHK
+			POOHCHK
 MAXDT		DLOAD	PDDL		# EXCHANGE DT/2MAX WITH COMPUTED MAX.
 			DT/2MAX
 		GOTO
@@ -757,7 +757,7 @@ GETMAXDT	RTB
 			SIGNMPAC
 		STCALL	DT/2
 			USEMAXDT
-P00HCHK		DLOAD	ABS
+POOHCHK		DLOAD	ABS
 			DT/2
 		DSU	BMN
 			DT/2MIN

Comanche055/P20-P25.agc

@@ -11,7 +11,7 @@
 #				of the same name, using Comanche055 page
 #				images.
 #		2009-05-20 RSB	Corrections:  P2OS -> P20S, STO -> STQ,
-#				GOTOPOOH -> GOTOP00H, a duplicated EXTEND
+#				GOTOPOOH -> GOTOPOOH, a duplicated EXTEND
 #				was fixed, P23.10 -> R23.10,
 #				S22B0X44 -> S22BOX44, S22SUBSCL -> 22SUBSCL,
 #				S22DPP -> S22DSPP, changed some instructions in
@@ -2685,7 +2685,7 @@ S22UOFF		=	LEMPOS		# 6	U SUB OFF
 #
 # CALLING SEQUENCE:	V 89 E
 #
-# SUBROUTINES CALLED:  CHKP00H, R02BOTH, GOXDSPF, R63COMP, R60CSM
+# SUBROUTINES CALLED:  CHKPOOH, R02BOTH, GOXDSPF, R63COMP, R60CSM
 #
 # ALARMS	1.  OPERATOR ERROR IF NOT IN P00
 #		2.  PROGRAM ALARM IF IMU IS OFF

Comanche055/P32-P33_P72-P73.agc

@@ -189,7 +189,7 @@
 #	 GOFLASH
 #	 GOTOPOOH
 # Page 652
-#	 VNP00H
+#	 VNPOOH
 #	 GOFLASHR
 #	 BLANKET
 #	 ENDOFJOB
@@ -237,7 +237,7 @@ P32/P72A	TC	P20FLGON
 		STORE	NN
 		EXIT
 		CAF	V06N11		# TCSI
-		TC	VNP00H
+		TC	VNPOOH
 		CAF	V06N55		# NN. ELEV(RGL05)
 # Page 653
 		TC	BANKCALL
@@ -246,7 +246,7 @@ P32/P72A	TC	P20FLGON
 		TC	+2
 		TC	-5
 		CAF	V06N37		# TTPI
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		DLOAD
 			TCSI
@@ -295,7 +295,7 @@ P32/P72F	STORE	T2TOT3
 			P32/P72F
 		EXIT
 		CAF	V06N75
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		VLOAD	CALL
 			DELVEET1
@@ -453,7 +453,7 @@ P32/P72F	STORE	T2TOT3
 #	 AVFLAGA
 #	 AVFLAGP
 #	 P20FLGON
-#	 VNP00H
+#	 VNPOOH
 #	 SELECTMU
 #	 ADVANCE
 #	 CDHMVR
@@ -476,7 +476,7 @@ P33		TC	AVFLAGA
 P73		TC	AVFLAGP
 P33/P73A	TC	P20FLGON
 		CAF	V06N13		# TCDH
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		DLOAD
 			TTPIO
@@ -560,7 +560,7 @@ P33/P73F	ABS	DSU
 		STORE	T2TOT3
 		EXIT
 		CAF	V06N75
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		VLOAD	CALL
 			DELVEET2
@@ -578,7 +578,7 @@ P33/P73F	ABS	DSU
 # SUBROUTINES USED
 
 #	 S32/33.X
-#	 VNP00H
+#	 VNPOOH
 
 		SETLOC	CDHTAG3
 		BANK
@@ -595,7 +595,7 @@ DISDVLVC	STORE	DELVLVC
 		STORE	DELVLVC
 		EXIT
 		CA	VERBNOUN
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		GOTO
 			NORMEX

Comanche055/P34-35_P74-75.agc

@@ -159,7 +159,7 @@
 #	AVFLAGA
 # Page 463
 #	AVFLAGP
-#	VNP00H
+#	VNPOOH
 #	DISPLAYE
 #	SELECTMU
 #	PRECSET
@@ -185,7 +185,7 @@ P34		TC	AVFLAGA
 P74		TC	AVFLAGP
 P34/P74A	TC	P20FLGON	# SET UPDATFLG, TRACKFLG
 		CAF	V06N37		# TTPI
-		TC	VNP00H		# Onno: The scans look like O not zero
+		TC	VNPOOH		# Onno: The scans look like O not zero
 		TC	INTPRET
 		SSP	EXIT
 			NN
@@ -240,7 +240,7 @@ SWCHCLR		BONCLR	BON
 		TC	P34/P74E
 P34/P74D	EXIT
 		CAF	V06N37		# TTPI
-		TC	VNP00H
+		TC	VNPOOH
 P34/P74E	TC	INTPRET
 		SETPD	DLOAD
 			0D
@@ -287,7 +287,7 @@ P34/P74E	TC	INTPRET
 		STORE	TIG
 		EXIT
 		CAF	V06N58
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		CALL
 			S34/35.5
@@ -821,7 +821,7 @@ ALLSET		STOVL	TET
 #	GOTOPOOH
 #	S34/35.3
 #	S34.35.4
-#	VNP00H
+#	VNPOOH
 
 S34/35.5	STQ	BON
 			SUBEXIT
@@ -835,7 +835,7 @@ FLAGON		VLOAD
 		STORE	DVLOS		# SAVE DELTA V BEFORE DISPLAY
 		EXIT
  		CAF	V06N81
- 		TC	VNP00H
+ 		TC	VNPOOH
  		TC	INTPRET
  		VLOAD	VSU		# TEST FOR OVERWRITE OF COMPUTED
  			DELVLVC		#                      DELTA V
@@ -852,7 +852,7 @@ FLAGOFF		CALL
 			S34/35.4
 		EXIT
 		CAF	V06N59
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		GOTO
 			SUBEXIT
@@ -955,7 +955,7 @@ P3XORP7X	CAF	HIGH9
 		INCR	Q
 		RETURN
 
-# ***** VNP00H *****
+# ***** VNPOOH *****
 #
 # SUBROUTINES USED
 #	BANKCALL
@@ -965,7 +965,7 @@ P3XORP7X	CAF	HIGH9
 		SETLOC P30SUBS
 		BANK
 
-VNP00H		EXTEND
+VNPOOH		EXTEND
 		QXCH	RTRN
 		TS	VERBNOUN
 		CAF	VNBANK		# ***** THIS ROUTINE MUST REMAIN IN

Comanche055/P51-P53.agc

@@ -10,7 +10,7 @@
 # Mod history:  2009-05-12 RSB	Adapted from Colossus249 file of the same
 #				name, and Comanche 055 page images.
 #		2009-05-20 RSB	Corrections: SETI/PDT -> SET1/PDT,
-#				GOTOPOOH -> GOTOP00H, R33EXIT -> R53EXIT,
+#				GOTOPOOH -> GOTOPOOH, R33EXIT -> R53EXIT,
 #				V853 -> VB53, R56A -> R56A1 (some places
 #				only), added missing R56A1 label, added a
 #				missing CAF in COARSTYP, corrected a SETLOC

Comanche055/P61-P67.agc

@@ -447,7 +447,7 @@ P66		TC	NEWMODEX		# ENTER VIA RTB WHEN D < Q7 FPSS
 # MOD BY:	R. HIRSCHKOP
 # FUNCTION:	TO TERMINATE STEERING WHEN THE CM VELOCITY WRT EARTH = 1000 FT/SEC
 # CALLING SEQUENCE:
-# EXIT:		TO P00H
+# EXIT:		TO POOH
 # SUBROUTINE CALLS:  GOFLASH
 
 # THIS DISPLAY IS CALLED EACH PASS THROUGH STEERING.  RESTART PROTECTION IS VIA STEERING.

Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.agc

@@ -11,7 +11,7 @@
 #				of the same name, using Comanche055 page
 #				images.  Finished through page 329.
 #		2009-05-09 RSB	Finished first draft.
-#		2009-05-20 RSB	Corrected a CHKPOOH to CHKP00H.
+#		2009-05-20 RSB	Corrected a CHKPOOH to CHKPOOH.
 #
 # This source code has been transcribed or otherwise adapted from digitized
 # images of a hardcopy from the MIT Museum.  The digitization was performed
@@ -3605,7 +3605,7 @@ PINTEST		EQUALS	LST2FAN
 		COUNT	41/PIN
 
 VBTSTLTS	TC	BANKCALL
-		CADR	CHKP00H
+		CADR	CHKPOOH
 
 		INHINT
 		CS	BIT1		# SET BIT 1 OF IMODES33 SO IMUMON WON'T

Comanche055/TPI_SEARCH.agc

@@ -476,7 +476,7 @@ P17		TC	AVFLAGA			# AVFLAG = CSM , SET TRACK + UPDATE FLAGS
 P77		TC	AVFLAGP			# AVFLAG = LEM , SET TRACK + UPDATE FLAGS
 P17.1		TC	P20FLGON		#	SET UPDATE FLAG
 		CAF	V06N37			#	DISPLAY TTPI TIME
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		CLEAR	CALL
 			UPDATFLG

Luminary099/AOSTASK_AND_AOSJOB.agc

@@ -85,7 +85,7 @@
 
 		EBANK=	AOSQ
 
-# ENTRY IS THROUGH 1/ACCJOB OR 1/ACCSIT WHEN 1/ACCS IS TO BE DONE AS A SEPARATE NOVAC JOB.
+# ENTRY IS THROUGH 1/ACCJOB OR 1/ACCSET WHEN 1/ACCS IS TO BE DONE AS A SEPARATE NOVAC JOB.
 # IT IS POSSIBLE FOR MORE THAN ONE OF THESE JOBS TO BE SET UP CONCURRENTLY.  HOWEVER, SINCE THERE IS NO CHECK OF
 # NEWJOB, A SECOND MANIFESTATION CANNOT BE STARTED UNTIL THE FIRST IS COMPLETED.
 

Luminary099/BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.agc

@@ -745,7 +745,7 @@ VB97DEX		=	OCT35		# NEGATIVE OF THIS IS PROPER FOR DISPDEX
 		CA	NVWORD 	+2	# NVWORD+2 CONTAINS V06 & APPROPRIATE NOUN
 		TC	BANKCALL
 		CADR	CLOCPLAY
-		TCF	STOPCLOK	# TERMINATE CLOKTASK ON THE WAY TO P00H
+		TCF	STOPCLOK	# TERMINATE CLOKTASK ON THE WAY TO POOH
 		TCF	COMFAIL1
 		TCF	COMFAIL2
 

Luminary099/DAPIDLER_PROGRAM.agc

@@ -27,10 +27,9 @@
 #	16:27 JULY 14, 1969
 
 # Page 1410
-# THE DAPIDLER PROGRAM IS STARTED BY FRESH START AND RESTART.  THE DAPIDLER PROGRAM IS DONE 10 TIMES
+# THE DAPIDLER PROGRAM IS STARTED BY FRESH START AND RESTART.		  THE DAPIDLER PROGRAM IS DONE 10 TIMES
 # PER SECOND UNTIL THE ASTRONAUT DESIRES THE DAP TO WAKE UP, AND THE IMU AND CDUS ARE READY FOR USE BY THE DAP.
 # THE NECESSARY INITIALIZATION OF THE DAP IS DONE BY THE DAPIDLER PROGRAM.
-
 		BANK	16
 		SETLOC	DAPS1
 		BANK
@@ -78,20 +77,20 @@ DAPIDLER	LXCH	BANKRUPT	# INTERRUPT LEAD INS (CONTINUED)
 		ADS	RCSFLAGS	# BIT 13 IS 1.
 		CAF	PRIO27
 		TC	NOVAC		# SET UP JOB TO DO A LITTLE INITIALIZATION
-		EBANK=	AOSQ		#	AND EXECUTE 1/ACCS.
+		EBANK=	AOSQ		#   AND EXECUTE 1/ACCS.
 		2CADR	1/ACCSET	# (WILL BRANCH TO MOREIDLE ON ACCSOKAY)
 
 CHECKUP		TC	CHEKBITS	# CHECK TO SEE IF LM DAP IS TO GO ON AND
-					#	DO ERROR DISPLAY.
+					#   DO ERROR DISPLAY.
 
 		CAE	DAPBOOLS	# IF 1/ACCS HAS NOT BEEN COMPLETED, IDLE.
-		MASK	ACCSOKAY	#	NOTE:	ONLY FRESH START AND RESTART
-		EXTEND			#		KNOCK THIS BIT DOWN.
+		MASK	ACCSOKAY	#   NOTE: ONLY FRESH START AND RESTART
+		EXTEND			# 	  KNOCK THIS BIT DOWN.
 		BZF	MOREIDLE
 
 STARTDAP	TC	IBNKCALL	# ZERO ATTITUDE ERROR AND DESIRED RATES.
 		FCADR	ZATTEROR
-		CAF	ZERO		# ************ INITIALIZE: *************
+		CAF	ZERO		# ********** INITIALIZE: **********
 		TS	TJP
 		TS	TJU
 		TS	TJV
@@ -118,7 +117,7 @@ STARTDAP	TC	IBNKCALL	# ZERO ATTITUDE ERROR AND DESIRED RATES.
 		TS	COTROLER	# DO TRYGTS ON FIRST PASS (WILL GO TO RCS)
 		TS	INGTS		# RECOGNIZE FIRST GTS PASS AS SUCH.
 		TS	QGIMTIMR	# STOP GIMBAL DRIVES.  (PROBABLY WOULD BE
-		TS	RGIMTIMR	#	GOOD ENOUGH JUST TO INACTIVATE TIMERS)
+		TS	RGIMTIMR	#   GOOD ENOUGH JUST TO INACTIVATE TIMERS)
 		TS	OLDPMIN		# MINIMUM IMPULSE MODE ERASABLES
 		TS	OLDQRMIN
 		TS	PJETCTR		# INITIALIZE DOCKED JET INHIBITION
@@ -212,36 +211,38 @@ DSPCADR		2CADR	ALTDSPLY
 		BANK
 		COUNT*	$$/NEEDL
 
-# PROGRAM:	ALTDSPLY
-# MOD 0.	6 DEC 1967
-# AUTHOR:	CRAIG WORK, DON KEENE, MIT IL
-# MOD 3 BY DON KEENE AUG 1, 1968 -- MOVED PROGRAM TO BANK 20
+# PROGRAM: ALTDSPLY
+#
+# MOD 0.  6 DEC 1967
+#
+# AUTHOR:  CRAIG WORK, DON KEENE, MIT IL
+#
+# MOD 3 BY DON KEENE AUG 1, 1968 MOVED PROGRAM TO BANK 20
 #
 # PROGRAM DESCRIPTION:
-#	ALTDSPLY REVERSES THE DSPLYALT BIT OF RCSFLAGS EACH TIME IT IS CALLED, WHICH IS PRESUMABLY EVERY 100 MS.
-# 	IF THE REVERSED BIT IS ONE, NEEDLER IS CALLED TO DISPLAY ATTITUDE ERRORS.  IF THE BIT IS ZERO, THE ATTITUDE ERR-
-#	ORS ARE CALCULATED AS 1) DAP FOLLOWING ERRORS, IF NEEDLFLG = 0, AND 2) TOTAL ATTITUDE ERRORS FOR NEEDLFLG = 1.
 #
+# ALTDSPLY REVERSES THE DSPLYALT BIT OF RCSFLAGS EACH TIME IT IS CALLED, WHICH IS PRESUMABLY EVERY 100 MS.
+# IF THE REVERSED BIT IS ONE, NEEDLER IS CALLED TO DISPLAY ATTITUDE ERRORS.  IF THE BIT IS ZERO, THE ATTITUDE ERR-
+# ORS ARE CALCULATED AS 1) DAP FOLLOWING ERRORS, IF NEEDLFLG = 0, AND 2) TOTAL ATTITUDE ERRORS FOR NEEDLFLG = 1.
 #
-# WARNING:	ALTDSPLY MAY ONLY BE CALLED WITH INTERRUPT INHIBITED
+# WARNING:  ALTDSPLY MAY ONLY BE CALLED WITH INTERRUPT INHIBITED.
 #
-# WARNING:	EBANK MUST BE SET TO 6 WHEN USING THIS ROUTINE.
+# WARNING:  EBANK MUST BE SET TO 6 WHEN USING THIS ROUTINE.
 #
-# INPUT:	RCSFLAGS AND	1) IF NEEDLFLG = 0, INPUT PERROR, QERROR, RERROR.
-#				2) IF NEEDLFLG = 1, INPUT CPHI,CTHETA,CPSI,CDUX,CDUY,CDUZ,M11,M21,M32,M22,M32.  (GPMATRIX)
+# INPUT:  RCSFLAGS AND 1) IF NEEDLFLG=0, INPUT PERROR,QERROR,RERROR.
+# 		       2) IF NEEDLFLG=1, INPUT CPHI,CTHETA,CPSI,CDUX,CDUY,CDUZ,M11,M21,M32,M22,M32. (GPMATRIX)
 #
+# OUTPUTS:  RCSFLAGS WITH DSPLYALT REVERSED,AK,AK1,AK2,+ NEEDLER OUTPUTS.
 #
-# OUTPUTS:	RCSFLAGS WITH DSPLYALT REVERSED, AK, AK1, AK2, + NEEDLER OUTPUTS.
+# ENTRY:   TCF    ALTDSPLY
 #
-# ENTRY:	TCF	ALTDSPLY
+# EXIT:    TCF    CHEKMORE
 #
-# EXIT:		TCF	CHEKMORE
+# ALARM OR ABORT EXITS:  NONE
 #
-# ALARM OR ABORT EXITS:	NONE
+# SUBPROGRAMS CALLED: NEEDLER, OVERSUB2
 #
-# SUBPROGRAMS CALLED:  NEEDLER, OVERSUB2
-#
-# DEBRIS:	A, L, AND NEEDLER DEBRIS.
+# DEBRIS:  A,L,AND NEEDLER DEBRIS.
 
 ALTDSPLY	CA	RCSFLAGS	# INVERT THE DISPLAY ALTERNATION BIT.
 		TS	L
@@ -258,9 +259,9 @@ ALTDSPLY	CA	RCSFLAGS	# INVERT THE DISPLAY ALTERNATION BIT.
 # Page 1415
 		MASK	NEEDLBIT	# TITUDE ERROR DISPLAY REQUEST.
 		CCS	A
-		TCF	DSPLYTOT	# TOTAL ERROR IS NEEDED IN AK, AK +1, AK +2
+		TCF	DSPLYTOT	# TOTAL ERROR IS NEEDED IN AK,AK +1,AK +2
 
-		CS	QERROR		# YES.  DISPLAY ATT ERRORS ON THE -BALL.
+		CS	QERROR		# YES. DISPLAY ATT ERRORS ON THE ,-BALL.
 		TS	AK +1		# ERROR COMPLEMENTS ARE INPUT TO NEEDLER.
 		CS	RERROR
 		TS	AK +2
@@ -279,9 +280,9 @@ DSPLYTOT	EXTEND
 		MSU	CDUY		# DIFFERENCE SCALED AT PI, 1'S COMP.
 		TS	AK		# SAVE FOR R-ERROR CALCULATION.
 		EXTEND
-		MP	M21		# (CTHETA-CDUY)*M21 SCALED AT PI RADIANS.
+		MP	M21		# (CHTETA-CDUY)*M21 SCALED AT PI RADIANS.
 		XCH	AK +1		# STORE FIRST TERM OF Q ERROR.
-		CA	CPSI		# DESIRED ATTITUDE, Z-AXIS, 2'S COMP.
+		CA	CPSI		# DESIRED ATTITUDE,Z-AXIS, 2'S COMP.
 		EXTEND			# SUBTRACT CURRENT ATTITUDE.
 		MSU	CDUZ		# DIFFERENCE SCALED AT PI, 1'S COMP.
 		TS	AK +2		# SAVE Z-AXIS TERM FOR R ERROR CALCULATION
@@ -316,7 +317,7 @@ DSPLYTOT	EXTEND
 
 # M13 = 1, SO BYPASS THE MULTIPLICATION.
 #		EXTEND
-#		MP	M13		# (CPHI-CDUX)*M13 SCALED AT PI RADIANS.
+#		MP	M13		  (CPHI-CDUX)*M13 SCALED AT PI RADIANS.
 
 		AD	AK		# P ERROR COMPLETE	, SCALED AT PI RAD
 		TC	OVERSUB2	# PIN NEEDLES IN CASE OF OVERFLOW.
@@ -330,55 +331,67 @@ DSPLYTOT	EXTEND
 # Page 1417
 # FDAI ATTITUDE ERROR DISPLAY SUBROUTINE
 #
-# PROGRAM DESCRIPTION:		D. KEENE	5/24/67
-# MOD 1 BY CRAIG WORK, 12 DEC 67
-# MOD 2 BY CRAIG WORK, 6 APRIL 68, CONVERTS ATTITUDE ERROR DISPLAY SCALING FROM 16 7/8 DEG. TO 42 3/16 DEGREES.
+# PROGRAM DESCRIPTION:    D. KEENE   5/24/67
 #
-# THIS SUBROUTINE IS USED TO DISPLAY ATTITUDE ERRORS ON THE FDAI VIA THE DIGITAL TO ANALOG CONVERTERS (DACS)
+# MOD 1 BY CRAIG WORK, 12 DEC 67
+#
+# MOD 2 BY CRAIG WORK, 6 APRIL 68 CONVERTS ATTITUDE ERROR DISPLAY SCALING FROM 16 7/8 DEG. TO 42 3/16 DEGREES.
+#
+#     THIS SUBROUTINE IS USED TO DISPLAY ATTITUDE ERRORS ON THE FDAI VIA THE DIGITAL TO ANALOG CONVERTERS (DACS)
 # IN THE CDUS.  CARE IS TAKEN TO METER OUT THE APPROPRIATE NUMBER OF PULSES TO THE IMU ERROR COUNTERS AND PREVENT
 # OVERFLOW, TO CONTROL THE RELAY SEQUENCING, AND TO AVOID INTERFERENCE WITH THE COARSE ALIGN LOOP WHICH ALSO USES
 # THE DACS.
 #
-# CALLING SEQUENCE:
-#	DURING THE INITIALIZATION SECTION OF THE USER'S PROGRAM, BIT3 OF RCSFLAGS SHOULD BE SET TO INITIATE THE
-#	TURN-ON SEQUENCE WITHIN THE NEEDLES PROGRAM:
-#		CS	RCSFLAGS	# IN EBANK6
-#		MASK	BIT3
-#		ADS	RCSFLAGS
-#	THEREAFTER, THE ATTITUDE ERRORS GENERATED BY THE USER SHOULD BE TRANSFERRED TO THE FOLLOWING LOCATIONS IN EBANK6:
-#		AK	SCALED 180 DEGREES	NOTE:	THESE LOCATIONS ARE SUBJECT
-#		AK1	SCALED 180 DEGREES		TO CHANGE
-#		AK2	SCALED 180 DEGREES
-#	FULL SCALED DEFLECTION OF THE NEEDLES CORRESPONDS TO 5 1/16 DEGREES, WHILE 384 BITS IN THE IMU ERROR COUNTER
-#	CORRESPONDS TO 42 3/16 DEGREES.  (DAC MAXIMUM CAPACITY IS 384 BITS.)  46 BITS EFFECTIVELY PIN THE NEEDLES.
 #
-#	A CALL TO NEEDLER WILL THE UPDATE THE DISPLAY:
-#		INHINT
-#		TC	IBNKCALL	# NOTE:  EBANK SHOULD BE SET TO E6
-#		CADR	NEEDLER
-#		RELINT
-#	THIS PROCESS SHOULD BE REPEATED EACH TIME THE ERRORS ARE UPDATED.  AT LEAST 3 PASSES THRU THE PROGRAM ARE
-#	REQUIRED BEFORE ANYTHING IS ACTUALLY DISPLAYED ON THE ERROR METERS.
-#	NOTE:  EACH CALL TO NEEDLER MUST BE SEPARATED BY AT LEAST 50 MS. TO ASSURE PROPER RELAY SEQUENCING.
+# CALLING SEQUENCE:
+#
+#     DURING THE INITIALIZATION SECTION OF THE USER'S PROGRAM, BIT3 OF RCSFLAGS SHOULD BE SET TO INITIATE THE
+# TURN-ON SEQUENCE WITHIN THE NEEDLES PROGRAM:
+#
+#	   CS	  RCSFLAGS	  IN EBANK6
+#	   MASK	  BIT3
+#	   ADS	  RCSFLAGS
+#
+# THEREAFTER, THE ATTITUDE ERRORS GENERATED BY THE USER SHOULD BE TRANSFERRED TO THE FOLLOWING LOCATIONS IN EBANK6:
+#
+#	   AK	  SCALED 180 DEGREES  NOTE: THESE LOCATIONS ARE SUBJECT
+#	   AK1	  SCALED 180 DEGREES	    TO CHANGE
+#	   AK2	  SCALED 180 DEGREES
+#
+# FULL SCALED DEFLECTION OF THE NEEDLES CORRESPONDS TO 5 1/16 DEGREES, WHILE 384 BITS IN THE IMU ERROR COUNTER
+# CORRESPONDS TO 42 3/16 DEGREES.  (DAC MAXIMUM CAPACITY IS 384 BITS.) 46 BITS EFFECTIVELY PIN THE NEEDLES.
+#
+# A CALL TO NEEDLER WILL THEN UPDATE THE DISPLAY:
+#
+#	   INHINT
+#	   TC	  IBNKCALL	 NOTE: EBANK SHOULD BE SET TO E6
+#	   CADR	  NEEDLER
+#	   RELINT
+#
+#     THIS PROCESS SHOULD BE REPEATED EACH TIME THE ERRORS ARE UPDATED.  AT LEAST 3 PASSES THRU THE PROGRAM ARE
+# REQUIRED BEFORE ANYTHING IS ACTUALLY DISPLAYED ON THE ERROR METERS.
+# NOTE: EACH CALL TO NEEDLER MUST BE SEPARATED BY AT LEAST 50MS TO ASSURE PROPER RELAY SEQUENCING.
 #
 # ERASABLES USED:
-#	AK		CDUXCMD
-#	AK1		CDUYCMD
-#	AK2		CDUZCMD
-#	EDRIVEX		A,L,Q
-#	EDRIVEY		T5TEMP
-#	EDRIVEZ		DINDX
+#		       AK	  CDUXCMD
+#		       AK1	  CDUYCMD
+#		       AK2	  CDUZCMD
+#		       EDRIVEX	  A,L,Q
+#		       EDRIVEY	  T5TEMP
+#		       EDRIVEZ	  DINDX
 # Page 1418
 #
-# SWITCHES:		RCSFLAGS  BITS 3,2
+# SWITCHES:	       RCSFLAGS	  BITS 3,2
 #
-# I/O CHANNELS:		CHAN12	BIT 4 (COARSE ALIGN -- READ ONLY)
-#			CHAN12	BIT 6 (IMU ERROR COUNTER ENABLE)
-#			CHAN14	BIT 13,14,15 (DAC ACTIVITY)
+# I/O CHANNELS:	       CHAN12	  BIT 4 (COARSE ALIGN - READ ONLY)
+#		       CHAN12	  BIT 6 (IMU ERROR COUNTER ENABLE)
+#		       CHAN14	  BIT 13,14,15 (DAC ACTIVITY)
 #
-# SIGN CONVENTION:	AK = THETAC - THETA
-#			WHERE	THETAC = COMMAND ANGLE
-#				THETA = PRESENT ANGLE
+#
+# SIGN CONVENTION<   AK = THETAC - THETA
+#	    WHERE    THETAC = COMMAND ANGLE
+#		     THETA  = PRESENT ANGLE
+
 
 NEEDLER		CA	RCSFLAGS
 		MASK	SIX
@@ -411,8 +424,8 @@ NEEDLER2	CAF	BIT6		# ENABLE IMU ERROR COUNTERS
 		EXTEND
 		WOR	CHAN12
 		CS	SIX		# RESET RCSFLAGS TO DISPLAY ATTITUDE
-		MASK	RCSFLAGS	# ERRORS.  WAIT AT LEAST 4 MS FOR
-		TS	RCSFLAGS	# RELAY CLOSURE.
+		MASK	RCSFLAGS	# ERRORS    WAIT ATLEAST 4 MS FOR
+		TS	RCSFLAGS	# RELAY CLOSURE
 		TCF	RETNMORE
 
 NEEDLES3	CAF	BIT6		# CHECK TO SEE IF IMU ERROR COUNTER
@@ -465,11 +478,11 @@ DACLIMIT	DEC	16000
 ONETENTH	OCT	03146		# DECIMAL +0.1, SCALED AT 1.
 DSPLYALT	EQUALS	BIT4		# 100 MS ALTERNATION BIT IN RCSFLAGS
 
-OVERSUB2	TS	7		# RETURNS A UNCHANGED OR LIMITED TO
+OVERSUB2	TS	7		# RETURNS  A  UNCHANGED  OR LIMITED TO
 		TC	Q		# POSMAX OR NEGMAX IF A HAS OVERFLOW
 		INDEX	A
 # Page 1420
-		CS	LIMITS		# DUPLICATE CODING IN BANK 16
+		CS	LIMITS		# DUPLICATE CODING IN  BANK 16
 		TC	Q
 
 RETNMORE	EXTEND			# RETURN TO CHEKMORE

Luminary099/EXTENDED_VERBS.agc

@@ -146,7 +146,7 @@ ALM/END		TC	FALTON		# TURN ON OPERATOR ERROR LIGHT
 GOPIN		TC	POSTJUMP
 		CADR	PINBRNCH
 
-CHKP00H		CA	MODREG		# CHECK FOR P00 OR P00-.
+CHKPOOH		CA	MODREG		# CHECK FOR P00 OR P00-.
 		EXTEND
 		BZF	TCQ
 		TC	ALM/END
@@ -827,7 +827,7 @@ DEC22		DEC	22
 
 		COUNT* 	$$/EXTVB
 
-VB64		TC	CHKP00H		# DEMAND PROGRAM 00.
+VB64		TC	CHKPOOH		# DEMAND PROGRAM 00.
 		TC	TESTXACT	# IF DISPLAY SYS. NOT BUSY MAKE IT BUSY.
 		CAF	PRIO4
 		TC	FINDVAC
@@ -846,7 +846,7 @@ VB64		TC	CHKP00H		# DEMAND PROGRAM 00.
 #	4.	REQUEST LOAD OF N22 (VALUES TO BE DISPLAYED).
 #	5.	ON PROCEED OR ENTER RE-DISPLAY V43 AND SEND PULSES.
 
-IMUATTCK	TC	CHKP00H		# VB 76 -- LOAD IMU ATT. ERROR METERS
+IMUATTCK	TC	CHKPOOH		# VB 76 -- LOAD IMU ATT. ERROR METERS
 
 		CAF	BITS4&5		# SEE IF COARSE ALIGN ENABLE AND ZERO IMU
 		EXTEND			# CDUS BITS ARE ON
@@ -1002,7 +1002,7 @@ V83PERF		TC	TESTXACT
 #    	TERMINATE -- EXIT R63.
 #	PROCEED -- RESET 3AXISFLG AND CALL R60LEM FOR ATTITUDE MANEUVER.
 
-V89PERF		TC	CHKP00H
+V89PERF		TC	CHKPOOH
 		TC	TESTXACT
 		CAF	PRIO10
 		TC	FINDVAC
@@ -1080,7 +1080,7 @@ NOMINIMP	INHINT
 #		C.	ENTER
 #			1.	REPEAT FLASHING V06,N22.
 
-CREWMANU	TC	CHKP00H		# DEMAND P00
+CREWMANU	TC	CHKPOOH		# DEMAND P00
 
 		TC	TESTXACT
 
@@ -1096,7 +1096,7 @@ CREWMANU	TC	CHKP00H		# DEMAND P00
 #	TERMINATE TRACKING (P20 AND P25).
 #
 #	1.	KNOCK DOWN RENDEZVOUS, TRACK, AND UPDATE FLAGS.
-#	2.	REQUIRE P20 OR P25 NOT RUNNING ALONE OR GO TO GOGOP00H (REQUEST PROGRAM 00).
+#	2.	REQUIRE P20 OR P25 NOT RUNNING ALONE OR GO TO GOGOPOOH (REQUEST PROGRAM 00).
 #	3.	SCHEDULE V56TOVAC WITH PRIORITY 30.
 #
 #	V56TOVAC
@@ -1223,7 +1223,7 @@ UPDATOFF	TC	UPFLAG		# VB 95 SET NOUPFLAG
 
 		EBANK=	QPLACE
 
-SYSTEST		TC	CHKP00H		# DEMAND P00
+SYSTEST		TC	CHKPOOH		# DEMAND P00
 
 		TC	TESTXACT
 
@@ -1246,7 +1246,7 @@ WMATRXNG	INHINT
 
 GOSHOSUM	EQUALS	SHOWSUM
 
-SHOWSUM		TC	CHKP00H		# *
+SHOWSUM		TC	CHKPOOH		# *
 		TC	TESTXACT	# *
 		CAF	PRIO7		# * ALLOW OTHER CHARINS.
 		TC	PRIOCHNG	# *

Luminary099/FIXED_FIXED_CONSTANT_POOL.agc

@@ -28,9 +28,9 @@
 
 # Page 1095
 		BLOCK	02
-		COUNT*	$$/FCONS
 
-# THE FOLLOWING TABLE OF 18 VALUES IS INDEXED.  DO NOT INSERT OR REMOVE ANY QUANTITIES
+		COUNT*	$$/FCONS
+# THE FOLLOWING TABLE OF 18 VALUES IS INDEXED. DO NOT INSERT OR REMOVE ANY QUANTITIES
 
 DPOSMAX		OCT	37777		# MUST PRECEDE POSMAX
 POSMAX		OCT	37777
@@ -71,7 +71,7 @@ SEVEN		OCT	7
 # BIT4		OCT	00010
 # R2D1		OCT	11		# PINBALL
 OCT11		=	R2D1		# P20S
-# BINCON	DEC	10		# PINBALL		(OCTAL 12)
+# BINCON	DEC	10		# PINBALL	     (OCTAL 12)
 ELEVEN		DEC	11
 # OCT14		OCT	14		# ALARM AND ABORT (FILLER)
 OCT15		OCT	15
@@ -79,21 +79,21 @@ OCT15		OCT	15
 LOW4		OCT	17
 # Page 1096
 # BIT5		OCT	00020
-# NC1		OCT	21		# PINBALL
+# ND1		OCT	21		# PINBALL
 # VD1		OCT	23		# PINBALL
 # OCT24		OCT	24		# SERVICE ROUTINES
 # MD1		OCT	25		# PINBALL
 BITS4&5		OCT	30
 # OCT31		OCT	31		# SERVICE ROUTINES
 OCT33		OCT	33
-# DEC27		=	OCT33
+DEC27		=	OCT33
 OCT35		OCT	35
-# DEC29		=	OCT35
+DEC29		=	OCT35
 CALLCODE	OCT	00032
 # LOW5		OCT	37		# PINBALL
-# 33DEC		DEC	33		# PINBALL		(OCTAL 41)
-# 34DEC		DEC	34		# PINBALL		(OCTAL 42)
-TBUILDFX	DEC	37		# BUILDUP FOR CONVENIENCE IN DAPTESTING
+# 33DEC		DEC	33		# PINBALL	     (OCTAL 41)
+# 34DEC		DEC	34		# PINBALL	     (OCTAL 42)
+TBUILDFX	DEC	37		# BUILDUP FOR CONVIENCE IN DAPTESTING
 TDECAYFX	DEC	38		# CONVENIENCE FOR DAPTESTING
 # BIT6		OCT	00040
 OCT50		OCT	50
@@ -108,7 +108,7 @@ SUPER101	OCT	120		# BITS FOR SUPERBNK SETTING 101
 # OCT121	OCT	121		# SERVICE ROUTINES
 					# (FIRST 8K OF ACM)
 SUPER110	OCT	140		# BITS FOR SUPERBNK SETTING 110.
-					# (LAST BK OF ACM)
+					# (LAST 8K OF ACM)
 1SEC		DEC	100
 # LOW7		OCT	177		# INTERPRETER
 # BIT8		OCT	00200
@@ -122,9 +122,9 @@ GN/CCODE	OCT	00401		# SET S/C CONTROL SWITCH TO G/N
 4SECS		DEC	400
 LOW9		OCT	777
 # BIT10		OCT	01000
-# 5.5DEGS	DEC	.03056		# P20-P25 SUNDANCE 	(OCTAL 00765)
+# 5.5DEGS	DEC	.03056		# P20-P25 SUNDANCE   (OCTAL 00765)
 # OCT1103	OCT	1103		# ALARM AND ABORT
-C5/2		DEC	.0363551	#		   	(OCTAL 01124)
+C5/2		DEC	.0363551	#		     (OCTAL 01124)
 V05N09		VN	0509		# (SAME AS OCTAL 1211)
 OCT1400		OCT	01400
 V06N22		VN	0622
@@ -134,7 +134,7 @@ BITS2-10	OCT	1776
 LOW10		OCT	1777
 # BIT11		OCT	02000
 # 2K+3		OCT	2003		# PINBALL
-LOW7+2K		OCT	2177		# OP CODE MASK + BANK 1 FBANK SETTING
+LOW7+2K		OCT	2177		# OP CODE MASK + BANK 1 FBANK SETTING.
 EBANK5		OCT	02400
 PRIO3		OCT	03000
 EBANK7		OCT	03400
@@ -146,20 +146,20 @@ PRIO6		OCT	06000
 PRIO7		OCT	07000
 
 # BIT13		OCT	10000
-#		OCT	10003		# T4RUPT	RELTAB +1D
+#		OCT	10003		# T4RUPT     RELTAB +1D
 # 13,7,2	OCT	10102		# P20-P25 SUNDANCE
 PRIO11		OCT	11000
 # PRIO12	OCT	12000		# BANKCALL
 PRIO13		OCT	13000
 PRIO14		OCT	14000
-#		OCT	14031		# T4RUPT	RELTAB +2D
+#		OCT	14031		# T4RUPT     RELTAB +2D
 PRIO15		OCT	15000
 PRIO16		OCT	16000
-# 85DEGS	DEC	.45556		# P20-P25 SUNDANCE	(OCTAL 16450)
+# 85DEGS	DEC	.45556		# P20-P25 SUNDANCE   (OCTAL 16450)
 PRIO17		OCT	17000
 OCT17770	OCT	17770
 # BIT14		OCT	20000
-#		OCT	20033		# T4RUPT	RELTAB +3D
+#		OCT	20033		# T4RUPT     RELTAB +3D
 PRIO21		OCT	21000
 		BLOCK	03
 		COUNT*	$$/FCONS
@@ -167,18 +167,18 @@ PRIO22		OCT	22000		# SERVICE ROUTINES
 PRIO23		OCT	23000
 PRIO24		OCT	24000
 # 5/8+1		OCT	24001		# SINGLE PRECISION SUBROUTINES
-#		OCT	24017		# T4RUPT	RELTAB +4D
+#		OCT	24017		# T4RUPT     RELTAB +4D
 PRIO25		OCT	25000
 PRIO26		OCT	26000
 PRIO27		OCT	27000
 # CHRPRIO	OCT	30000		# PINBALL
-#		OCT	30036		# T4RUPT	RELTAB +5D
+#		OCT	30036		# T4RUPT     RELTAB +5D
 PRIO31		OCT	31000
-C1/2		DEC	.7853134	#			(OCTAL 31103)
+C1/2		DEC	.7853134	#		     (OCTAL 31103)
 PRIO32		OCT	32000
 PRIO33		OCT	33000
 PRIO34		OCT	34000
-#		OCT	34034		# T4RUPT	RELTAB +6D
+#		OCT	34034		# T4RUPT     RELTAB +6D
 # Page 1098
 PRIO35		OCT	35000
 PRIO36		OCT	36000
@@ -190,27 +190,27 @@ OCT37774	OCT	37774
 OCT37776	OCT	37776
 # DPOSMAX	OCT	37777
 # BIT15		OCT	40000
-# OCT40001	OCT	40001		# INTERPRETER (CS 1 INSTRUCTION)
+# OCT40001	OCT	40001		# INTERPRETER  ( CS   1   INSTRUCTION)
 DLOADCOD	OCT	40014
 DLOAD*		OCT	40015
-#		OCT	40023		# T4RUPT	RELTAB +7D
+#		OCT	40023		# T4RUPT     RELTAB +7D
 BIT15+6		OCT	40040
 OCT40200	OCT	40200
-#		OCT	44035		# T4RUPT	RELTAB +8D
-#		OCT	50037		# T4RUPT	RELTAB +9D
-#		OCT	54000		# T4RUPT	RELTAB +10D
+#		OCT	44035		# T4RUPT    RELTAB +8D
+#		OCT	50037		# T4RUPT     RELTAB +9D
+#		OCT	54000		# T4RUPT     RELTAB +10D
 -BIT14		OCT	57777
 # RELTAB11	OCT	60000		# T4RUPT
-C3/2		DEC	-.3216147	#			(OCTAL 65552)
+C3/2		DEC	-.3216147	#		     (OCTAL 65552)
 13,14,15	OCT	70000
 -1/8		OCT	73777
 HIGH4		OCT	74000
--ENDERAS	DEC	-2001		#			(OCTAL 74056)
+-ENDERAS	DEC	-2001		#		     (OCTAL 74056)
 # HI5		OCT	76000		# PINBALL
 HIGH9		OCT	77700
-# -ENDVAC	DEC	-45		# INTERPRETER		(OCTAL 77722)
-# -OCT10	OCT	-10		#			(OCTAL 77767)
-# NEG4		DEC	-4		#			(OCTAL 77773)
+# -ENDVAC	DEC	-45		# INTERPRETER	     (OCTAL 77722)
+# -OCT10	OCT	-10		#		      (OCT 77767)
+# NEG4		DEC	-4		#		     (OCTAL 77773)
 NEG3		DEC	-3
 NEG2		OCT	77775
 NEGONE		DEC	-1
@@ -254,7 +254,7 @@ PRIO20		=	BIT14
 HALF		=	BIT14
 PRIO30		=	CHRPRIO
 BIT13-14	=	PRIO30		# INTERPRETER USES IN PROCESSING STORECODE
-OCT30002	=	TLOAD 	+1
+OCT30002	=	TLOAD +1
 B12T14		=	PRIO34
 NEGMAX		=	BIT15
 VLOADCOD	=	BIT15

Luminary099/FRESH_START_AND_RESTART.agc

@@ -350,7 +350,7 @@ PTBAD		TC	ALARM		# SET ALARM TO SHOW PHASE TABLE FAILURE.
 		TCF	DOFSTRT1
 #******** ****** ******
 # Page 218
-# DO NOT USE GOPROG2 OR ENEMA WITHOUT CONSULTING P00H PEOPLE.
+# DO NOT USE GOPROG2 OR ENEMA WITHOUT CONSULTING POOH PEOPLE.
 
 OCT10000	=	BIT13
 OCT30000	=	PRIO30
@@ -844,10 +844,10 @@ DUMMYAD		EXIT
 
 		TC	DOWNFLAG		# ALLOW X-AXIS OVERRIDE.
 		ADRES	XOVINFLG
-		CCS	MMNUMBER		# IS THIS A P00H REQUEST
+		CCS	MMNUMBER		# IS THIS A POOH REQUEST
 		TCF	NOUVEAU			# NO, PICK UP NEW PROGRAM
 
-P00H		TC	RELDSP			# RELEASE DISPLAY SYSTEM
+POOH		TC	RELDSP			# RELEASE DISPLAY SYSTEM
 
 		CAF	PRIO5			# SET VARIABLE RESTART PRIORITY FOR
 		TS	PHSPRDT2		# P00 INTEGRATION.
@@ -887,7 +887,7 @@ SEUDOP00	TS	DNLSTCOD		# SET UP APPROPRIATE DOWNLIST CODE
 		TC	IBNKCALL		# KILL GROUPS 1,3,5,6
 		CADR	V37KLEAN
 
-		CCS	MMNUMBER		# IS IT P00H
+		CCS	MMNUMBER		# IS IT POOH
 		TCF	RENDV00			# NO
 GOMOD		TC	IBNKCALL		# REDUNDANT EXCEPT FOR GROUP 4
 		CADR	P00KLEAN

Luminary099/GENERAL_LAMBERT_AIMPOINT_GUIDANCE.agc

@@ -25,75 +25,75 @@
 # Notations on the hardcopy document read, in part:
 #
 #	Assemble revision 001 of AGC program LMY99 by NASA 2021112-061
-#	16:27 JULY 14, 1969
+#	16:27 JULY 14,1969
 
 # Page 651
 
-# GENERAL LAMBERT AIMPOINT GUIDANCE **
-# WRITTEN BY RAMA M AIYAWAR
+# GENERAL  LAMBERT AIMPOINT GUIDANCE **
+# WRITTEN  BY RAMA M AIYAWAR
 
 # PROGRAM P-31 DESCRIPTION **
 #
-# 1.	TO ACCEPT TARGETING PARAMETERS OBTAINED FROM A SOURCE EXTERNAL
-#	TO THE LEM AND COMPUTE THERE FROM THE REQUIRED-VELOCITY AND
-#	OTHER INITIAL CONDITIONS REQUIRED BY LM FOR DESIRED MANEUVER.
-#	THE TARGETING PARAMETERS ARE TIG (TIME OF IGNITION), TARGET
-#	VECTOR (RTARG), AND THE TIME FROM TIG UNTIL THE TARGET IS
-#	REACHED (DELLT4), DESIRED TIME OF FLIGHT FROM RINIT TO RTARG.
+# 1.	   TO ACCEPT TARGETING PARAMETERS OBTAINED FROM A SOURCE EXTERNAL
+#	   TO THE LEM AND COMPUTE THERE FROM THE REQUIRED-VELOCITY AND
+#	   OTHER INITIAL CONDITIONS REQUIRED BY LM FOR DESIRED MANEUVER.
+#	   THE TARGETING PARAMETERS ARE TIG (TIME OF IGNITION), TARGET
+#	   VECTOR (RTARG), AND THE TIME FROM TIG UNTIL THE TARGET IS
+#	   REACHED(DELLT4),DESIRED TIME OF FLIGHT FROM  RINIT TO RTARG..
 
 # ASSUMPTIONS **
 #
-# 1.	THE TARGET PARAMETERS MAY HAVE BEEN LOADED PRIOR TO THE
-#	EXECUTION OF THIS PROGRAM.
-# 2.	THIS PROGRAM IS APPLICABLE IN EITHER EARTH OR LUNAR ORBIT.
-# 3.	THIS PROGRAM IS DESIGNED FOR ONE-MAN OPERATION, AND SHOULD
-#	BE SELECTED BY THE ASTRONAUT BY DSKY ENTRY V37 E31.
+# 1.	   THE TARGET PARAMETERS MAY HAVE BEEN LOADED PRIOR TO THE
+#	   EXECUTION OF THIS PROGRAM.
+# 2.	   THIS PROGRAM IS APPLICABLE IN EITHER EARTH OR LUNAR ORBIT.
+# 3.	   THIS PROGRAM IS DESIGNED FOR ONE-MAN OPERATION, AND SHOULD
+#	   BE SELECTED BY THE ASTRONAUT BY DSKY ENTRY  V37 E31.
 
 # SUBROUTINES USED **
 #
 # MANUPARM, TTG/N35, R02BOTH, MIDGIM, DISPMGA, FLAGDOWN, BANKCALL,
 # GOTOPOOH, ENDOFJOB, PHASCHNG, GOFLASHR, GOFLASH.
 #
-# MANUPARM	CALCULATES APOGEE, PERIGEE ALTITUDES AND DELTAV DESIRED
-#		FOR THE MANEUVER.
+# MANUPARM	  CALCULATES APOGEE, PERIGEE ALTITUDES AND DELTAV DESIRED
+#		  FOR THE MANEUVER.
 #
-# TTG/N35	CLOCKTASK - UPDATES CLOCK.
+# TTG/N35	  CLOCKTASK - UPDATES CLOCK.
 #
-# MIDGIM	CALCULATES MIDDLE GIMBAL ANGLE FOR DISPLAY.
+# MIDGIM	  CALCULATES MIDDLE GIMBAL ANGLE FOR DISPLAY.
 #
-# R02BOTH	IMU - STATUS CHECK ROUTINE.
+# R02BOTH	  IMU - STATUS CHECK ROUTINE.
 
 # DISPLAYS USED IN P-31LM **
 #
-# V06N33	DISPLAY SOTRED TIG (IN HRS. MINS. SECS.)
-# V06N42	DISPLAY APOGEE, PERIGEE, DELTAV.
-# V16N35	DISPLAY TIME FROM TIG.
-# V06N45	TIME FROM IGNITION AND MIDDLE GIMBAL ANGLE.
+# V06N33	  DISPLAY SOTRED  TIG (IN HRS. MINS. SECS)
+# V06N42	  DISPLAY APOGEE, PERIGEE, DELTAV.
+# V16N35	  DISPLAY TIME FROM TIG.
+# V06N45	  TIME FROM IGNITION AND MIDDLE GIMBAL ANGLE.
 
 # ERASABLE INITIALIZATION REQUIRED **
 #
-# TIG		TIME OF IGNITION		DP	(B+28) CS.
+# TIG		  TIME OF IGNITION    DP    (B+28) CS.
 #
-# DELLT4	DESIRED TIME OF FLIGHT		DP	(B+28) CS
-#		FROM RINIT TO RTARG.
+# DELLT4	  DESIRED TIME OF FLIGHT   DP  (B+28) CS
+#		  FROM RINIT TO RTARG .
 #
-# RTARG		RADIUS VECTOR OF TARGET POSITION VECTOR
-#		RADIUS VECTOR SCALED TO (B+29)METERS IF EARTH ORBIT
+# RTARG		  RADIUS VECTOR OF TARGET POSITION VECTOR
+#		  RADIUS VECTOR   SCALED TO  (B+29)METERS IF EARTH ORBIT
 # Page 652
-#		RADIUS VECTOR SCALED TO (B+27)METERS IF MOON ORBIT
+#		  RADIUS VECTOR SCALED TO    (B+27)METERS IF MOON  ORBIT
 
 # OUTPUT **
 #
-# HAPO		APOGEE ALTITUDE
-# HPER		PERIGEE ALTITUDE
-# VGDISP	MAG. OF DELTAV FOR DISPLAY, SCALING	B+7 M/CS EARTH
-# 		MAG. OF DELTAV FOR DISPLAY, SCALING	B+5 M/CS MOON
-# MIDGIM	MIDDLE GIMBAL ANGLE
-# XDELVFLG	RESETS XDELVFLG FOR LAMBERT VG COMPUTATIONS
+# HAPO		  APOGEE ALTITUDE
+# HPER		  PERIGEE ALTITUDE
+# VGDISP	  MAG.OF DELTAV FOR DISPLAY ,SCALING	  B+7 M/CS EARTH
+#		  MAG.OF DELTAV FOR DISPLAY,SCALING	  B+5 M/CS MOON
+# MIDGIM	  MIDDLE GIMBAL ANGLE
+# XDELVFLG	  RESETS XDELVFLG FOR LAMBERT VG COMPUTATIONS
 
-# ALARMS OR ABORTS	NONE **
+# ALARMS OR ABORTS  NONE **
 
-# RESTARTS ARE VIA GROUP 4 **
+# RESTARTS  ARE VIA GROUP 4 **
 
 		SETLOC	GLM
 		BANK
@@ -102,8 +102,8 @@
 
 		COUNT*	$$/P31
 P31		TC	P20FLGON
-		CAF	V06N33		# T16
-		TC	VNP00H
+		CAF	V06N33		# TIG
+		TC	VNPOOH
 		TC	INTPRET
 		CLEAR	DLOAD
 			UPDATFLG
@@ -154,9 +154,9 @@ P31		TC	P20FLGON
 		STORE	HAPO
 		EXIT
 		CAF	V06N81		# DELVLVC
-		TC	VNP00H
+		TC	VNPOOH
 		CAF	V06N42		# HAPO, HPER, VGDISP
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 REVN1645	SET	CALL		# TRKMKCNT, TTOGO, +MGA
 			FINALFLG
@@ -166,4 +166,3 @@ REVN1645	SET	CALL		# TRKMKCNT, TTOGO, +MGA
 
 
 # *** END OF LEMP30S .103 ***
-

Luminary099/IMU_COMPENSATION_PACKAGE.agc

@@ -45,34 +45,34 @@
 		TCF	IRIG1		# RETURN
 
 1/PIPA1		CAF	FOUR		# PIPAZ, PIPAY, PIPAX
-		TS	BUF	+2
+		TS	BUF +2
 
-		INDEX	BUF 	+2
+		INDEX	BUF +2
 		CA	PIPASCF		# (P.P.M.) X 2(-9)
 		EXTEND
-		INDEX	BUF 	+2
+		INDEX	BUF +2
 		MP	DELVX		# (PP) X 2(+14) NOW (PIPA PULSES) X 2(+5)
 		TS	Q		# SAVE MAJOR PART
 
 		CA	L		# MINOR PART
 		EXTEND
-		MP	BIT6		# SCALE 2(+9)	SHIFT RIGHT 9
-		INDEX 	BUF 	+2
-		TS	DELVX 	+1	# FRACTIONAL PIPA PULSES SCALED 2(+14)
+		MP	BIT6		# SCALE 2(+9)   SHIFT RIGHT 9
+		INDEX 	BUF +2
+		TS	DELVX +1	# FRACTIONAL PIPA PULSES SCALED 2(+14)
 
 		CA	Q		# MAJOR PART
 		EXTEND
 		MP	BIT6		# SCALE 2(+9)	SHIFT RIGHT 9
-		INDEX	BUF 	+2
-		DAS	DELVX		# (PIPAI) + (PIPAI)(SF)
+		INDEX	BUF  +2
+		DAS	DELVX		# (PIPAI) + (PIPAI)(SFE)
 
-		INDEX	BUF 	+2
-		CS	PIPABIAS	# (PIPA PULSES)/(CS) X 2(-5)		 *			*
+		INDEX	BUF +2
+		CS	PIPABIAS	# (PIPA PULSES)/(CS) X 2(-5)		 *
 		EXTEND
-		MP	1/PIPADT	# (CS) X 2(+8) NOW (PIPA PULSES) X 2(+5) *
+		MP	1/PIPADT	# (CS) X 2(+8)  NOW (PIPA PULSES) X 2(+3)*
 		EXTEND
-		MP	BIT4		# SCALE 2(+11) SHIFT RIGHT 11		 *
-		INDEX	BUF 	+2
+		MP	BIT4		# SCALE 2(+11)  SHIFT RIGHT 11		 *
+		INDEX	BUF +2
 		DAS	DELVX		# (PIPAI) + (PIPAI)(SFE) - (BIAS)(DELTAT)
 
 		CCS	BUF 	+2	# PIPAZ, PIPAY, PIPAX
@@ -83,79 +83,79 @@
 
 # Page 328
 IRIGCOMP	TS	GCOMPSW		# INDICATE COMMANDS 2 PULSES OR LESS.
-		TS	BUF		# INDEX COUNTER.  IRIGX, IRIGY, IRIGZ.
+		TS	BUF		# INDEX COUNTER .  IRIGX, IRIGY, IRIGZ.
 
 		TC	IRIGX		# COMPENSATE ACCELERATION TERMS
 
 		CS	NBDX		# (GYRO PULSES)/(CS) X 2(-5)
-		TC	DRIFTSUB	# -(NBOX)(DELTAT)	(GYRO PULSES) X 2(+14)
+		TC	DRIFTSUB	# -(NBOX)(DELTAT)   (GYRO PULSES) X 2(+14)
 
 		TC	IRIGY		# COMPENSATE ACCELERATION TERMS
 
 		CS	NBDY		# (GYRO PULSES)/(CS) X 2(-5)
-		TC	DRIFTSUB	# +(NBDY)(DELTAT)	(GYRO PULSES) X 2(+14)
+		TC	DRIFTSUB	# -(NBDY)(DELTAT)   (GYRO PULSES) X 2(+14)
 
 		TC	IRIGZ		# COMPENSATE ACCELERATION TERMS
 
 		CA	NBDZ		# (GYRO PULSES)/(CS) X 2(-5)
-		TC	DRIFTSUB	# +(NBDZ)(DELTAT)	(GYRO PULSES) X 2(+14)
+		TC	DRIFTSUB	# +(NBDZ)(DELTAT)   (GYRO PULSES) X 2(+14)
 
 		CCS	GCOMPSW		# ARE GYRO COMMANDS GREATER THAN 2 PULSES
-		TCF	+2		# YES	SEND OUT GYRO TORQUING COMMANDS.
-		TCF	IRIG1		# NO	RETURN
+		TCF	+2		# YES  SEND OUT GYRO TORQUING COMMANDS.
+		TCF	IRIG1		# NO  RETURN
 
-		CA	PRIO21		# PRIO GREATER THAN SERVICER.
+		CA	PRIO21		# PRIO GREATER THAN SERVICER
 		TC	NOVAC		# SEND OUT GYRO TORQUING COMMANDS.
 		EBANK=	NBDX
 		2CADR	1/GYRO
 
 		RELINT
-IRIG1		CA	MODE		# RESTORE CALLER'S EBANK
+IRIG1		CA	MODE		# RESTORE CALLERS EBANK
 		TS	EBANK
 		TCF	SWRETURN
 
 # Page 329
 IRIGX		EXTEND
-		QXCH	MPAC	+2	# SAVE Q
+		QXCH	MPAC +2	        # SAVE Q
 		EXTEND
 		DCS	DELVX		# (PIPA PULSES) X 2(+14)
 		DXCH	MPAC
-		CA	ADIAX		# (GYRO PULSES)/(PIPA PULSE) X 2(-6)		*
-		TC	GCOMPSUB	# -(ADIAX)(PIPAX)	   (GYRO PULSES) X 2(+14)
+		CA	ADIAX		# (GYRO PULSES)/(PIPA PULSE) X 2(-6)     *
+		TC	GCOMPSUB	# -(ADIAX)(PIPAX)   (GYRO PULSES) X 2(+14)
 
 		EXTEND			#
-		DCS	DELVY		# 	(PIPA PULSES) X 2(+14)
+		DCS	DELVY		# (PIPA PULSES) X 2(+14)
 		DXCH	MPAC		#
-		CS	ADSRAX		# 	(GYRO PULSES)/(PIPA PULSE) X 2(-6)	*
-		TC	GCOMPSUB	# 	-(ADSRAX)(PIPAY)   (GYRO PULSES) X 2(+14)
+		CS	ADSRAX		# (GYRO PULSES)/(PIPA PULSE) X 2(-6)	 *
+		TC	GCOMPSUB	# +(ADSRAX)(PIPAY)  (GYRO PULSES) X 2(+14)
 
-#		EXTEND			# ***
-#		DCS	DELVY		# ***	(PIPA PULSES) X 2(+14)
-#		DXCH	MPAC		# ***
-#		CA	ADOAX		# ***	(GYRO PULSES)/(PIPA PULSE) X 2(-6)	*
-#		TC	GCOMPSUB	# ***	-(ADOAX)(PIPAZ)	   (GYRO PULSES) X 2(+14)
+#		EXTEND		 # ***
+#		DCS	DELVZ	 # ***    (PIPA PULSES) X 2(+14)
+#		DXCH	MPAC	 # ***
+#		CA	ADOAX	 # ***    (GYRO PULSES)/(PIPA PULSE) X 2(-6)	 *
+#		TC	GCOMPSUB # ***    -(ADOAX)(PIPAZ)   (GYRO PULSES) X 2(+14)
 
-		TC	MPAC	+2
+		TC	MPAC  +2
 
 IRIGY		EXTEND
-		QXCH	MPAC	+2	# SAVE Q
+		QXCH	MPAC  +2	# SAVE Q
 		EXTEND
 		DCS	DELVY		# (PIPA PULSES) X 2(+14)
 		DXCH	MPAC
-		CA	ADIAY		# (GYRO PULSES)/(PIPA PULSE) X 2(-6)		*
-		TC	GCOMPSUB	# -(ADIAY)(PIPAY)	   (GYRO PULSES) X 2(+14)
+		CA	ADIAY		# (GYRO PULSES)/(PIPA PULSE) X 2(-6)     *
+		TC	GCOMPSUB	# -(ADIAY)(PIPAY)   (GYRO PULSES) X 2(+14)
 
 		EXTEND
 		DCS	DELVZ		# (PIPA PULSES) X 2(+14)
 		DXCH	MPAC
-		CS	ADSRAY		# (GYRO PULSES)/(PIPA PULSE) X 2(-6)		*
-		TC	GCOMPSUB	# +(ADSRAY)(PIPAZ)      	(GYRO PULSES) X 2(+14)
+		CS	ADSRAY		# (GYRO PULSES)/(PIPA PULSE) X 2(-6)	 *
+		TC	GCOMPSUB	# +(ADSRAY)(PIPAZ)  (GYRO PULSES) X 2(+14)
 
-#		EXTEND			# ***
-#		DCS	DELVX		# ***	(PIPA PULSES) X 2(+14)
-#		DXCH	MPAC		# ***
-#		CA	ADOAY		# ***	(GYRO PULSES)/(PIPA PULSE) X 2(-6)	*
-#		TC	GCOMPSUB	# ***	-(ADOAY)(/PIPAX)   (GYRO PULSES) X 2(+14)
+#		EXTEND		 # ***
+#		DCS	DELVX	 # ***    (PIPA PULSES) X 2(+14)
+#		DXCH	MPAC	 # ***
+#		CA	ADOAY	 # ***    (GYRO PULSES)/(PIPA PULSE) X 2(-6)	 *
+#		TC	GCOMPSUB # ***    -(ADOAY)(PIPAX)   (GYRO PULSES) X 2(+14)
 
 		TC	MPAC +2
 
@@ -164,46 +164,46 @@ IRIGZ		EXTEND
 		EXTEND
 		DCS	DELVY		# (PIPA PULSES) X 2(+14)
 		DXCH	MPAC
-		CA	ADSRAZ		# (GYRO PULSES)/(PIPA PULSE) X 2(-6)		*
+		CA	ADSRAZ		# (GYRO PULSES)/(PIPA PULSE) X 2(-6)	 *
 # Page 330
-		TC	GCOMPSUB	# -(ADSRAZ)(PIPAY)	  (GYRO PULSES) X 2(+14)
+		TC	GCOMPSUB	# -(ADSRAZ)(PIPAY)  (GYRO PULSES) X 2(+14)
 
 		EXTEND
 		DCS	DELVZ		# (PIPA PULSES) X 2(+14)
 		DXCH	MPAC
-		CA	ADIAZ		# (GYRO PULSES)/(PIPA PULSE) X 2(-6)		*
-		TC	GCOMPSUB	# -(ADIAZ)(PIPAZ)	   (GYRO PULSES) X 2(+14)
+		CA	ADIAZ		# (GYRO PULSES)/(PIPA PULSE) X 2(-6)	 *
+		TC	GCOMPSUB	# -(ADIAZ)(PIPAZ)   (GYRO PULSES) X 2(+14)
 
-#		EXTEND			# ***
-#		DCS	DELVX		# ***	(PIPA PULSE) X 2(+14)
-#		DXCH	MPAC		# ***
-#		CS	ADOAZ		# ***	(GYRO PULSES)/(PIPA PULSE) X 2(-6)	*
-#		TC	GCOMPSUB	# ***	+(ADOAZ)(PIPAX)	   (GYRO PULSES) X 2(+14)
+#		EXTEND		 # ***
+#		DCS	DELVX	 # ***	  (PIPA PULSE) X 2(+14)
+#		DXCH	MPAC	 # ***
+#		CS	ADOAZ	 # ***	  (GYRO PULSES)/(PIPA PULSE) X 2(-6)     *
+#		TC	GCOMPSUB # ***	  +(ADOAZ)(PIPAX)   (GYRO PULSES) X 2(+14)
 
 		TC	MPAC +2
 
 # Page 331
 GCOMPSUB	XCH	MPAC		# ADIA OR ADSRA COEFFICIENT ARRIVES IN A
 		EXTEND			# C(MPAC) = (PIPA PULSES) X 2(+14)
-		MP	MPAC		# (GYRO PULSES)/(PIPA PULSE) X 2(-6)		*
-		DXCH	VBUF		# NOW = (GYRO PULSES) X 2(+8)			*
+		MP	MPAC		# (GYRO PULSES)/(PIPA PULSE) X 2(-6)	 *
+		DXCH	VBUF		# NOW = (GYRO PULSES) X 2(+8)		 *
 
 		CA	MPAC +1		# MINOR PART OF PIPA PULSES
 		EXTEND
 		MP	MPAC		# ADIA OR ADSRA
 		TS	L
 		CAF	ZERO
-		DAS	VBUF		# NOW = (GYRO PULSES) X 2(+8)			*
+		DAS	VBUF		# NOW = (GYRO PULSES) X 2(+8)		 *
 
-		CA	VBUF		# PARTIAL RESULT -- MAJOR
+		CA	VBUF		# PARTIAL RESULT - MAJOR
 		EXTEND
-		MP	BIT9		# SCALE 2(+6)	SHIFT RIGHT 6			*
+		MP	BIT9		# SCALE 2(+6)	   SHIFT RIGHT           *
 		INDEX	BUF		# RESULT = (GYRO PULSES) X 2(+14)
-		DAS	GCOMP		# HI(ADIA)(PIPAI) OR HI(ADSRA)(PIPAI)
+		DAS	GCOMP		# HI(ADIA)(PIPAI)  OR  HI(ADSRA)(PIPAI)
 
-		CA	VBUF +1		# PARTIAL RESULT -- MINOR
+		CA	VBUF +1		# PARTIAL RESULT - MINOR
 		EXTEND
-		MP	BIT9		# SCALE 2(+6)	SHIFT RIGHT 6			*
+		MP	BIT9		# SCALE 2(+6)	SHIFT RIGHT 6		 *
 		TS	L
 		CAF	ZERO
 		INDEX	BUF		# RESULT = (GYRO PULSES) X 2(+14)
@@ -213,23 +213,23 @@ GCOMPSUB	XCH	MPAC		# ADIA OR ADSRA COEFFICIENT ARRIVES IN A
 
 # Page 332
 DRIFTSUB	EXTEND
-		QXCH	BUF 	+1
+		QXCH	BUF +1
 
 		EXTEND			# C(A) = NBD	(GYRO PULSES)/(CS) X 2(-5)
-		MP	1/PIPADT	# (CS) X 2(+8)	NO (GYRO PULSES) X 2(+3)
-		LXCH	MPAC 	+1	# SAVE FOR FRACTIONAL COMPENSATION
+		MP	1/PIPADT	# (CS) X 2(+8)	 NOW (GYRO PULSES) X 2(+3)
+		LXCH	MPAC +1	        # SAVE FOR FRACTIONAL COMPENSATION
 		EXTEND
-		MP	BIT4		# SCALE 2(+11)	SHIFT RIGHT 11
+		MP	BIT4		# SCALE 2(+11)	   SHIFT RIGHT 11
 		INDEX	BUF
-		DAS	GCOMP		# HI(NBD)(DELTAT)	(GYRO PULSES) X 2(+14)
+		DAS	GCOMP		# HI(NBD)(DELTAT)   (GYRO PULSES) X 2(+14)
 
-		CA	MPAC 	+1	# NO MINOR PART
+		CA	MPAC +1	        # NOW MINOR PART
 		EXTEND
-		MP	BIT4		# SCALE 2(+11)		SHIFT RIGHT 11
+		MP	BIT4		# SCALE 2(+11)	   SHIFT RIGHT 11
 		TS	L
 		CAF	ZERO
 		INDEX	BUF		# ADD IN FRACTIONAL COMPENSATION
-		DAS	GCOMP		# (NBD)(DELTAT)		(GYRO PULSES) X 2(+14)
+		DAS	GCOMP		# (NBD)(DELTAT)     (GYRO PULSES) X 2(+14)
 
 DRFTSUB2	CAF	TWO		# PIPAX, PIPAY, PIPAZ
 		AD	BUF
@@ -237,23 +237,23 @@ DRFTSUB2	CAF	TWO		# PIPAX, PIPAY, PIPAZ
 		INDEX	A
 		CCS	GCOMP		# ARE GYRO COMMANDS 1 PULSE OR GREATER
 		TCF	+2		# YES
-		TC	BUF 	+1	# NO
+		TC	BUF +1	        # NO
 
 		MASK	COMPCHK		# DEC -1
 		CCS	A		# ARE GYRO COMMANDS GREATER THAN 2 PULSES
-		TS	GCOMPSW		# YES -- SET GCOMPSW POSITIVE
-		TC	BUF 	+1	# NO
+		TS	GCOMPSW		# YES - SET GCOMPSW POSITIVE
+		TC	BUF +1	        # NO
 
 # Page 333
 1/GYRO		CAF	FOUR		# PIPAZ, PIPAY, PIPAX
 		TS	BUF
 
 		INDEX	BUF		# SCALE GYRO COMMANDS FOR IMUPULSE
-		CA	GCOMP	+1	# FRACTIONAL PULSES
+		CA	GCOMP  +1	# FRACTIONAL PULSES
 		EXTEND
 		MP	BIT8		# SHIFT RIGHT 7
 		INDEX	BUF
-		TS	GCOMP	+1	# FRACTIONAL PULSES SCALED
+		TS	GCOMP  +1	# FRACTIONAL PULSES SCALED
 
 		CAF	ZERO		# SET GCOMP = 0 FOR DAS INSTRUCTION
 		INDEX	BUF
@@ -265,7 +265,7 @@ DRFTSUB2	CAF	TWO		# PIPAX, PIPAY, PIPAZ
 
 		CCS	BUF		# PIPAZ, PIPAY, PIPAX
 		AD	NEG1
-		TCF	1/GYRO 	+1
+		TCF	1/GYRO +1
 LGCOMP		ECADR	GCOMP		# LESS THAN ZERO IMPOSSIBLE
 
 		CAF	LGCOMP
@@ -281,7 +281,7 @@ GCOMP1		CAF	FOUR		# PIPAZ, PIPAY, PIPAX
 		INDEX	BUF		# RESCALE
 		CA	GCOMP +1
 		EXTEND
-		MP	BIT8		# SHIFT MINOR PART LEFT 7 -- MAJOR PART = 0
+		MP	BIT8		# SHIFT MINOR PART LEFT 7 - MAJOR PART = 0
 		INDEX	BUF
 		LXCH	GCOMP +1	# BITS 8-14 OF MINOR PART WERE = 0
 
@@ -319,16 +319,16 @@ NBDONLY		CCS	GCOMPSW		# BYPASS IF GCOMPSW NEGATIVE
 		AD	1/PIPADT	# PRESENT TIME - PREVIOUS TIME
 NBD2		AD	HALF		# CORRECT FOR POSSIBLE TIME1 TICK
 		AD	HALF
-		XCH	L		# IF TIME1 DID NOT DICK, REMOVE RESULTING
+		XCH	L		# IF TIME1 DID NOT TICK, REMOVE RESULTING
 		XCH	L		# OVERFLOW.
 
-NBD3		EXTEND			# C(A) = DELTAT		(CS) X 2(+14)
+NBD3		EXTEND			# C(A) = DELTAT    (CS) X 2(+14)
 		MP	BIT10		# SHIFT RIGHT 5
 		DXCH	VBUF +2
 
 		CA	ZERO
 		TS	GCOMPSW		# INDICATE COMMANDS 2 PULSES OR LESS.
-		TS	BUF		# INDEX X, Y, Z.
+		TS	BUF		# INDEX  X, Y, Z.
 
 		CCS	TEM1		# IF SURFACE FLAG IS SET,
 		TC	IRIGX		# COMPENSATE ACCELERATION TERMS.
@@ -338,7 +338,7 @@ NBD3		EXTEND			# C(A) = DELTAT		(CS) X 2(+14)
 		DXCH	MPAC		# DELTAT NOW SCALED (CS) X 2(+19)
 
 		CS	NBDX		# (GYRO PULSES)/(CS) X 2(-5)
-		TC	FBIASSUB	# -(NBOX)(DELTAT) 	(GYRO PULSES) X 2(+14)
+		TC	FBIASSUB	# -(NBDX)(DELTAT)   (GYRO PULSES) X 2(+14)
 
 		CCS	TEM1		# IF SURFACE FLAG IS SET,
 		TC	IRIGY		# COMPENSATE ACCELERATION TERMS.
@@ -347,16 +347,16 @@ NBD3		EXTEND			# C(A) = DELTAT		(CS) X 2(+14)
 		DCS	VBUF +2
 		DXCH	MPAC		# DELTAT SCALED (CS) X 2(+19)
 		CA	NBDY		# (GYRO PULSES)/(CS) X 2(-5)
-		TC	FBIASSUB	# -(NBDY)(DELTAT)	(GYRO PULSES) X 2(+14)
+		TC	FBIASSUB	# -(NBDY)(DELTAT)   (GYRO PULSES) X 2(+14)
 
-		CCS	TEM1		# IF SURFACE FLAG IS SET,
+		CCS	TEM1		# IF SURFACE FLAG IS SET.
 		TC	IRIGZ		# COMPENSATE ACCELERATION TERMS
 
 		EXTEND
 		DCS	VBUF +2
 		DXCH	MPAC		# DELTAT SCALED (CS) X 2(+19)
 		CS	NBDZ		# (GYRO PULSES)/(CS) X 2(-5)
-		TC	FBIASSUB	# +(NBDZ)(DELTAT)	(GYRO PULSES) X 2(+14)
+		TC	FBIASSUB	# +(NBDZ)(DELTAT)   (GYRO PULSES) X 2(+14)
 
 		CCS	GCOMPSW		# ARE GYRO COMMANDS GREATER THAN 2 PULSES
 		TCF	1/GYRO		# YES
@@ -370,7 +370,7 @@ FBIASSUB	XCH	Q
 		EXTEND
 		MP	MPAC		# DELTAT SCALED (CS) X 2(+19)
 		INDEX	BUF
-		DAS	GCOMP		# HI(NBD)(DELTAT)	(GYRO PULSES) X 2(+14)
+		DAS	GCOMP		# HI(NBD)(DELTAT)   (GYRO PULSES) X 2(+14)
 
 		CA	Q		# NOW FRACTIONAL PART
 		EXTEND
@@ -378,7 +378,7 @@ FBIASSUB	XCH	Q
 		TS	L
 		CAF	ZERO
 		INDEX	BUF
-		DAS	GCOMP		# (NBD)(DELTAT)		(GYRO PULSES) X 2(+14)
+		DAS	GCOMP		# (NBD)(DELTAT)     (GYRO PULSES) X 2(+14)
 
 		TCF	DRFTSUB2	# CHECK MAGNITUDE OF COMPENSATION
 
@@ -415,4 +415,3 @@ GCOMPZER	CAF	LGCOMP		# ROUTINE TO ZERO GCOMP BEFORE FIRST
 		TS	GCOMP +5
 
 		TCF	IRIG1		# RESTORE EBANK AND RETURN
-

Luminary099/INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.agc

@@ -26,199 +26,198 @@
 
 # Page 54
 
-# *** CHANNEL DESCRIPTION WORDS ARE ALLOCATED IN ERASABLE ASSIGNMENTS ***
+# ***	CHANNEL DESCRIPTIONSF WORDS ARE ALLOCATED IN ERASABLE ASSIGNMENTS ***
 
-# CHANNEL 1	IDENTICAL TO COMPUTER REGISTER L (0001)
+#	CHANNEL 1	IDENTICAL TO COMPUTER REGISTER L (0001)
 
-# CHANNEL 2	IDENTICAL TO COMPUTER REGISTER Q (0002)
+#	CHANNEL 2	IDENTICAL TO COMPUTER REGISTER Q (0002)
 
-# CHANNEL 3	HISCALAR: INPUT CHANNEL; MOST SIGNIFICANT 14 BITS FROM 33 STAGE BINARY COUNTER. SCALE
-#		FACTOR IS B23 IN CSEC, SO MAX VALUE ABOUT 23.3 HOURS AND LEAST SIGNIFICANT BIT 5.12 SECS.
+#	CHANNEL 3	HISCALAR; INPUT CHANNEL; MOST SIGNIFICANT 14 BITS FROM 33 STAGE BINARY COUNTER. SCALE
+#			FACTOR IS B23 IN CSEC, SO MAX VALUE ABOUT 23.3 HOURS AND LEAST SIGNIFICANT BIT 5.12 SECS.
 
-# CHANNEL 4	LOSCALAR: INPUT CHANNEL; NEXT MOST SIGNIFICANT 14 BITS FROM THE 33 STAGE BINARY COUNTER
-#		ASSOCIATED WITH CHANNEL 3. SCALE FACTOR IS B9 IN CSEC. SO MAX VAL IS 5.12 SEC AND LEAST
-#		SIGNIFICANT BIT IS 1/3200 SEC. SCALE FACTOR OF D.P. WORD WITH CHANNEL 3 IS B23 CSEC.
+#	CHANNEL 4	LOSCALAR; INPUT CHANNEL; NEXT MOST SIGNIFICANT 14 BITS FROM THE 33 STAGE BINARY COUNTER
+#			ASSOCIATED WITH CHANNEL 3. SCALE FACTOR IS B9 IN  CSEC. SO MAX VAL IS 5.12 SEC AND LEAST
+#			SIGNIFICANT BIT IS 1/3200 SEC. SCALE FACTOR OF D.P. WORD WITH CHANNEL 3 IS B23 CSEC.
 
-# CHANNEL 5	PYJETS:  OUTPUT CHANNEL; PITCH RCS JET CONTROL.  (REACTION CONTROL SYSTEM) USES BITS 1-8.
+#	CHANNEL 5	PYJETS; OUTPUT CHANNEL; PITCH RCS JET CONTROL.   (REACTION CONTROL SYSTEM) USES BITS 1-8.
 
-# CHANNEL 6	ROLLJETS: OUTPUT CHANNEL; ROLL RCS JET CONTROL.  (REACTION CONTROL SYSTEM) USES BIT 1-8.
+#	CHANNEL 6	ROLLJETS; OUTPUT CHANNEL; ROLL RCS JET CONTROL.   (REACTION CONTROL SYSTEM) USES BIT 1-8.
 
-# CHANNEL 7	SUPERBNK: OUTPUT CHANNEL; NOT RESET BY RESTART; FIXED EXTENSION BITS USED TO SELECT THE
-#		APPROPRIATE FIXED MEMORY BANK IF FBANK IS 30 OCTAL OR MORE.  USES BITS 5-7.
+#	CHANNEL 7	SUPERBNK; OUTPUT CHANNEL; NOT RESET BY RESTART;   FIXED EXTENSION BITS USED TO SELECT THE
+#			APPROPRIATE FIXED MEMORY BANK IF FBANK IS 30 OCTAL OR MORE. USES BITS 5-7.
 
-# CHANNEL 10	OUT0: OUTPUT CHANNEL; REGISTER USED TO TRANSMIT LATCHING-RELAY DRIVING INFORMATION FOR
-#		THE DISPLAY SYSTEM.  BITS 15-12 ARE SET TO THE ROW NUMBER (1-14 OCTAL) OF THE RELAY TO BE
-#		CHANGED AND BITS 11-1 CONTAIN THE REQUIRED SETTINGS FOR THE RELAYS IN THE ROW.
+#	CHANNEL 10	OUT0; OUTPUT CHANNEL; REGISTER USED TO TRANSMIT    LATCHING-RELAY DRIVING INFORMATION FOR
+#			THE DISPLAY SYSTEM.  BITS 15-12 ARE SET TO THE ROW NUMBER (1-14 OCTAL) OF THE RELAY TO BE
+#			CHANGED AND BITS 11-1 CONTAIN THE REQUIRED SETTINGS FOR THE RELAYS IN THE ROW.
 
-# CHANNEL 11	DSALMOUT: OUTPUT CHANNEL; REGISTER WHOSE BITS ARE USED FOR ENGINE ON-OFF CONTROL AND TO
-#		DRIVE INDIVIDUAL INDICATORS OF THE DISPLAY SYSTEM.  BITS 1-7 ARE A RELAYS.
+#	CHANNEL 11	DSALMOUT; OUTPUT CHANNEL; REGISTER WHOSE BITS ARE USED FOR ENGINE ON-OFF CONTROL AND TO
+#			DRIVE INDIVIDUAL INDICATORS OF THE DISPLAY SYSTEM. BITS 1-7 ARE A RELAYS.
 #
-#		BIT 1		ISS WARNING
-#		BIT 2		LIGHT COMPUTER ACTIVITY LAMP
-#		BIT 3		LIGHT UPLINK ACTIVITY LAMP
-#		BIT 4		LIGHT TEMP CAUTION LAMP
-#		BIT 5		LIGHT KEYBOARD RELEASE LAMP
-#		BIT 6		FLASH VERB AND NOUN LAMPS
-#		BIT 7		LIGHT OPERATOR ERROR LAMP
+#	  BIT 1		ISS WARNING
+#	  BIT 2		LIGHT COMPUTER ACTIVITY LAMP
+#	  BIT 3		LIGHT UPLINK ACTIVITY LAMP
+#	  BIT 4		LIGHT TEMP CAUTION LAMP
+#	  BIT 5		LIGHT KEYBOARD RELEASE LAMP
+#	  BIT 6		FLASH VERB AND NOUN LAMPS
+#	  BIT 7		LIGHT OPERATOR ERROR LAMP
 # Page 55
-#		BIT 8		SPARE
-#		BIT 9		TEST CONNECTOR OUTBIT
-#		BIT 10		CAUTION RESET
-#		BIT 11		SPARE
-#		BIT 12		SPARE
-#		BIT 13		ENGINE ON
-#		BIT 14		ENGINE OFF
-#		BIT 15		SPARE
+#	  BIT 8		SPARE
+#	  BIT 9		TEST CONNECTOR OUTBIT
+#	  BIT 10	CAUTION RESET
+#	  BIT 11	SPARE
+#	  BIT 12	SPARE
+#	  BIT 13	ENGINE ON
+#	  BIT 14	ENGINE OFF
+#	  BIT 15	SPARE
 
-# CHANNEL 12	CHAN12: OUTPUT CHANNEL; BITS USED TO DRIVE NAVIGATION AND SPACECRAFT HARDWARE.
+#	CHANNEL 12	CHAN12; OUTPUT CHANNEL; BITS USED TO DRIVE NAVIGATION AND SPAECRAFT HARDWARE
 #
-#		BIT 1		ZERO RR CDU; CDU'S GIVE RRADAR INFORMATION FOR LM
-#		BIT 2		ENABLE CDU RADAR ERROR COUNTERS
-#		BIT 3		NOT USED
-#		BIT 4		COARSE ALIGN ENABLE OF IMU
-#		BIT 5		ZERO IMU CDU'S
-#		BIT 6		ENABLE IMU ERROR COUNTER, CDU ERROR COUNTER.
-#		BIT 7		SPARE
-#		BIT 8		DISPLAY INERTIAL DATA
-#		BIT 9		-PITCH GIMBAL TRIM (BELL MOTION) DESCENT ENGINE
-#		BIT 10		+PITCH GIMBAL TRIM (BELL MOTION) DESCENT ENGINE
-#		BIT 11		-ROLL GIMBAL TRIM (BELL MOTION) DESCENT ENGINE
-#		BIT 12		+ROLL GIMBAL TRIM (BELL MOTION) DESCENT ENGINE
-#		BIT 13		LR POSITION 2 COMMAND
-#		BIT 14		ENABLE RENDEZVOUS RADAR LOCK-ON; AUTO ANGLE TRACK'G
-#		BIT 15		ISS TURN ON DELAY COMPLETE
+#	  BIT 1		ZERO RR CDU; CDU'S GIVE RRADAR INFORMATION FOR LM
+#	  BIT 2		ENABLE CDU RADAR ERROR COUNTERS
+#	  BIT 3		NOT USED
+#	  BIT 4		COARSE ALIGN ENABLE OF IMU
+#	  BIT 5		ZERO IMU CDU'S
+#	  BIT 6		ENABLE IMU ERROR COUNTER, CDU ERROR COUNTER.
+#	  BIT 7		SPARE
+#	  BIT 8		DISPLAY INERTIAL DATA
+#	  BIT 9		-PITCH GIMBAL TRIM (BELL MOTION) DESCENT ENGINE
+#	  BIT 10	+PITCH GIMBAL TRIM (BELL MOTION) DESCENT ENGINE
+#	  BIT 11	-ROLL  GIMBAL TRIM (BELL MOTION) DESCENT ENGINE
+#	  BIT 12	+ROLL  GIMBAL TRIM (BELL MOTION) DESCENT ENGINE
+#	  BIT 13	LR POSITION 2 COMMAND
+#	  BIT 14	ENABLE RENDESVOUS RADAR LOCK-ON;AUTO ANGLE TRACK'G
+#	  BIT 15	ISS TURN ON DELAY COMPLETE
 
 # Page 56
-# CHANNEL 13	CHAN13: OUTPUT CHANNEL.
+#	CHANNEL 13	CHAN13; OUTPUT CHANNEL.
 #
-#		BIT 1		RADAR C		PROPER SETTING OF THE A,B,C MATRIX
-#		BIT 2		RADAR B		SELECTS CERTAIN RADAR
-#		BIT 3		RADAR A		PARAMETERS TO BE READ.
-#		BIT 4		RADAR ACTIVITY
-#		BIT 5		NOT USED (CONNECTS AN ALTERNATE INPUT TO UPLINK)
-#		BIT 6		BLOCK INPUTS TO UPLINK CELL
-#		BIT 7		DOWNLINK TELEMETRY WORD ORDER CODE BIT
-#		BIT 8		RHC COUNTER ENABLE (READ HAND CONTROLLER ANGLES)
-#		BIT 9		START RHC READ INTO COUNTERS IS BIT 8 SET
-#		BIT 10		TEST ALARMS, TEST DSKY LIGHTS
-#		BIT 11		ENABLE STANDBY
-#		BIT 12		RESET TRAP 31-A		ALWAYS APPEAR TO BE SET TO 0
-#		BIT 13		RESET TRAP 31-B		ALWAYS APPEAR TO BE SET TO 0
-#		BIT 14		RESET TRAP 32		ALWAYS APPEAR TO BE SET TO 0
-#		BIT 15		ENABLE T6 RUPT
+#	  BIT 1		RADAR C		PROPER SETTING OF THE A,B,C MATRIX
+#	  BIT 2		RADAR B		SELECTS CERTAIN RADAR
+#	  BIT 3		RADAR A		PARAMETERS TO BE READ.
+#	  BIT 4		RADAR ACTIVITY
+#	  BIT 5		NOT USED (CONNECTS AN ALTERNATE INPUT TO UPLINK)
+#	  BIT 6		BLOCK INPUTS TO UPLINK CELL
+#	  BIT 7		DOWNLINK TELEMETRY WORD ORDER CODE BIT
+#	  BIT 8		RHC COUNTER ENABLE (READ HAND CONTROLLER ANGLES)
+#	  BIT 9		START RHC READ INTO COUNTERS IF BIT 8 SET
+#	  BIT 10	TEST ALARMS, TEST DSKY LIGHTS
+#	  BIT 11	ENABLE STANDBY
+#	  BIT 12	RESET TRAP 31-A		ALWAYS APPEAR TO BE SET TO 0
+#	  BIT 13	RESET TRAP 31-B		ALWAYS APPEAR TO BE SET TO 0
+#	  BIT 14	RESET TRAP 32		ALWAYS APPEAR TO BE SET TO 0
+#	  BIT 15	ENABLE T6 RUPT
 
-# CHANNEL 14	CHAN14: OUTPUT CHANNEL; USED TO CONTROL COMPUTER COUNTER CELLS (CDU, GYRO, SPACECRAFT FUNC).
+#	CHANNEL 14	CHAN14; OUTPUT CHANNEL; USED TO CONTROL COMPUTER  COUNTER CELLS (CDU,GYRO,SPACECRAFT FUNC.
 #
-#		BIT 1		OUTLINK ACTIVITY (NOT USED)
-#		BIT 2		ALTITUDE RATE OR ALTITUDE SELECTOR
-#		BIT 3		ALTITUDE METER ACTIVITY
-#		BIT 4		THRUST DRIVE ACTIVITY FOR DESCENT ENGINE
-#		BIT 5		SPARE
-#		BIT 6		GYRO ENABLE POWER FOR PULSES
-#		BIT 7		GYRO SELECT B		PAIR OF BITS IDENTIFIES AXIS OF
-#		BIT 8		GYRO SELECT A		GYRO SYSTEM TO BE TORQUED.
-#		BIT 9		GYRO TORQUING COMMAND IN NEGATIVE DIRECTION.
+#	  BIT 1		OUTLINK ACTIVITY (NOT USED)
+#	  BIT 2		ALTITUDE RATE OR ALTITIDE SELECTOR
+#	  BIT 3		ALTITUDE METER ACTIVITY
+#	  BIT 4		THRUST DRIVE ACTIVITY FOR DESCENT ENGINE
+#	  BIT 5		SPARE
+#	  BIT 6		GYRO ENABLE POWER FOR PULSES
+#	  BIT 7		GYRO SELECT B		PAIR OF BITS IDENTIFIES AXIS OF -
+#	  BIT 8		GYRO SELECT A		GYRO SYSTEM TO BE TORQUED.
+#	  BIT 9		GYRO TORQUING COMMAND IN NEGATIVE DIRECTION
 # Page 57
-#		BIT 10		GYRO ACTIVITY
-#		BIT 11		DRIVE CDU S
-#		BIT 12		DRIVE CDU T
-#		BIT 13		DRIVE CDU Z
-#		BIT 14		DRIVE CDU Y
-#		BIT 15		DRIVE CDU X
+#	  BIT 10	GYRO ACTIVITY
+#	  BIT 11	DRIVE CDU S
+#	  BIT 12	DRIVE CDU T
+#	  BIT 13	DRIVE CDU Z
+#	  BIT 14	DRIVE CDU Y
+#	  BIT 15	DRIVE CDU X
 
-# CHANNEL 15	MNKEYIN: INPUT CHANNEL; KEY CODE INPUT FROM KEYBOARD OF DSKY, SENSED BY PROGRAM WHEN
-#		PROGRAM INTERRUPT #5 IS RECEIVED.  USED BITS 5-1
+#	CHANNEL 15	MNKEYIN; INPUT CHANNEL;KEY CODE INPUT FROM KEYBOARD OF DSKY, SENSED BY PROGRAM WHEN
+#			PROGRAM INTERRUPT #5 IS RECEIVED. USES BITS 5-1
 
-# CHANNEL 16	NAVKEYIN: INPUT CHANNEL; OPTICS MARK INFORMATION AND NAVIGATION PANEL DSKY (CM) OR THRUST
-#		CONTROL (LM) SENSED BY PROGRAM THEN PROGRAM INTERRUPT #6 IS RECEIVED.  USES BITS 3-7 ONLY.
+#	CHANNEL 16	NAVKEYIN; INPUT CHANNEL; OPTICS MARK INFORMATION AND NAVIGA ION PANEL DSKY (CM) OR THRUST
+#			CONTROL (LM) SENSED BY PROGRAM WHEN PROGRAM INTER-RUPT #6 IS RECEIVED. USES BITS 3-7 ONLY.
 #
-#		BIT 1		NOT ASSIGNED
-#		BIT 2		NOT ASSIGNED
-#		BIT 3		OPTICS X-AXIS MARK SIGNAL FOR ALIGN OPTICAL TSCOPE
-#		BIT 4		OPTICS Y-AXIS MARK SIGNAL FOR AOT
-#		BIT 5		OPTICS MARK REJECT SIGNAL
-#		BIT 6		DESCENT+ ; CREW DESIRED SLOWING RATE OF DESCENT
-#		BIT 7		DESCENT- ; CREW DESIRED SPEEDING UP RATE OF D'CENT
+#	  BIT 1		NOT ASSIGNED
+#	  BIT 2		NOT ASSIGNED
+#	  BIT 3		OPTICS X-AXIS MARK SIGNAL FOR ALIGN OPTICAL TSCOPE
+#	  BIT 4		OPTICS Y-AXIS MARK SIGNAL FOR AOT
+#	  BIT 5		OPTICS MARK REJECT SIGNAL
+#	  BIT 6		DESCENT+ ; CREW DESIRED SLOWING RATE OF DESCENT
+#	  BIT 7		DESCENT- ; CREW DESIRED SPEEDING UP RATE OF D'CENT
 
-# NOTE: ALL BITS IN CHANNELS 30-33 ARE INVERTED AS SENSED BY THE PROGRAM, SO THAT A VALUE OF ZERO MEANS
+# NOTE: ALL BITS IN CHANNELS 30-33 ARE INVERTED AS SENSED BY THE  PROGRAM, SO THAT A VALUE OF ZERO MEANS
 # THAT THE INDICATED SIGNAL IS PRESENT.
 
-# CHANNEL 30	INPUT CHANNEL
+#	CHANNEL 30	INPUT CHANNEL
 #
-#		BIT 1		ABORT WITH DESCENT STAGE
-#		BIT 2		UNUSED
-#		BIT 3		ENGINE ARMED SIGNAL
-#		BIT 4		ABORT WITH ASCENT ENGINE STAGE
-#		BIT 5		AUTO THROTTLE; COMPUTER CONTROL OF DESCENT ENGINE
+#	  BIT 1		ABORT WITH DESCENT STAGE
+#	  BIT 2		   UNUSED
+#	  BIT 3		ENGINE ARMED SIGNAL
+#	  BIT 4		ABORT WITH ASCENT ENGINE STAGE
+#	  BIT 5		AUTO THROTTLE; COMPUTER CONTROL OF DESCENT ENGINE
 # Page 58
-#		BIT 6		DISPLAY INERTIAL DATA
-#		BIT 7		RR CDU FAIL
-#		BIT 8		SPARE
-#		BIT 9		IMU OPERATE WITH NO MALFUNCTION
-#		BIT 10		LM COMPUTER (NOT AGS) HAS CONTROL OF LM.
-#		BIT 11		IMU CAGE COMMAND TO DRIVE IMU GIMBAL ANGLES TO 0.
-#		BIT 12		IMU CDU FAIL (MALFUNCTION OF IMU CDU,S)
-#		BIT 13		IMU FAIL (MALFUNCTION OF IMU STABILIZATION LOOPS)
-#		BIT 14		ISS TURN ON REQUESTED
-#		BIT 15		TEMPERATURE OF STABLE MEMBER WITHIN DESIGN LIMITS
+#	  BIT 6		DISPLAY INERTIAL DATA
+#	  BIT 7		RR CDU FAIL
+#	  BIT 8		SPARE
+#	  BIT 9		IMU OPERATE WITH NO MALFUNCTION
+#	  BIT 10	LM COMPUTER (NOT AGS) HAS CONTROL OF LM
+#	  BIT 11	IMU CAGE COMMAND TO DRIVE IMU GIMBAL ANGLES TO 0.
+#	  BIT 12	IMU CDU FAIL (MALFUNCTION OF IMU CDU,S)
+#	  BIT 13	IMU FAIL (MALFUNCTION OF IMU STABILIZATION LOOPS)
+#	  BIT 14	ISS TURN ON REQUESTED
+#	  BIT 15	TEMPERATURE OF STABLE MEMBER WITHIN DESIGN LIMITS
 
-# CHANNEL 31	INPUT CHANNEL; BITS ASSOCIATED WITH THE ATTITUDE CONTROLLER, TRANSLATIONAL CONTROLLER,
-#		AND SPACECRAFT ATTITUDE CONTROL; USED BY RCS DAP.
+#	CHANNEL 31	INPUT CHANNEL; BITS ASSOCIATED WITH THE ATTITUDE  CONTROLLER, TRANSLATIONAL CONTROLLER,
+#			AND SPACECRAFT ATTITUDE CONTROL; USED BY RCS DAP
 #
-#		BIT 1		ROTATION (BY RHC) COMMANDED IN POSITIVE PITCH DIRECTION; MUST BE IN MINIMUM IMPULSE MODE.
-#				ALSO POSITIVE ELEVATION CHANGE FOR LANDING POINT DESIGNATOR
-#		BIT 2		AS BIT 1 EXCEPT NEGATIVE PITCH AND ELEVATION.
-#		BIT 3		ROTATION (BY RHC) COMMANDED IN POSITIVE YAW DIRECTION; MUST BE IN MINIMUM IMPULSE MODE.
-#		BIT 4		AS BIT 3 EXCEPT NEGATIVE YAW
-#		BIT 5		ROTATION (BY RHC) COMMANDED IN POSITIVE ROLL DIRECTION; MUST BE IN MINIMUM IMPULSE MODE.
-#				ALSO POSITIVE AZIMUTH CHANGE FOR LANDING POINT DESIGNATOR.
-#		BIT 6		AS BIT 5 EXCEPT NEGATIVE ROLL AND AZIMUTH
-#		BIT 7		TRANSLATION IN +X DIRECTION COMMANDED BY THC
-#		BIT 8		TRANSLATION IN -X DIRECTION COMMANDED BY THC
-#		BIT 9		TRANSLATION IN +Y DIRECTION COMMANDED BY THC
-#		BIT 10		TRANSLATION IN -Y DIRECTION COMMANDED BY THC
-#		BIT 11		TRANSLATION IN +Z DIRECTION COMMANDED BY THC
-#		BIT 12		TRANSLATION IN -Z DIRECTION COMMANDED BY THC
+#	  BIT 1		ROTATION (BY RHC) COMMANDED IN POSITIVE PITCH DIRECTION; MUST BE IN MINIMUM IMPULSE MODE.
+#			ALSO POSITIVE ELEVATION CHANGE FOR LANDING POINT  DESIGNATOR
+#	  BIT 2		AS BIT 1 EXCEPT NEGATIVE PITCH AND ELEVATION
+#	  BIT 3		ROTATION (BY RHC) COMMANDED IN POSITIVE YAW DIRECTION; MUST BE IN MINIMUM IMPULSE MODE.
+#	  BIT 4		AS BIT 3 EXCEPT NEGATIVE YAW
+#	  BIT 5		ROTATION (BY RHC) COMMANDED IN POSITIVE ROLL DIRECTION; MUST BE IN MINIMUM IMPULSE MODE.
+#			ALSO POSITIVE AZIMUTH CHANGE FOR LANDING POINT DESIGNATOR
+#	  BIT 6		AS BIT 5 EXCEPT NEGATIVE ROLL AND AZIMUTH
+#	  BIT 7		TRANSLATION IN +X DIRECTION COMMANDED BY THC
+#	  BIT 8		TRANSLATION IN -X DIRECTION COMMANDED BY THC
+#	  BIT 9		TRANSLATION IN +Y DIRECTION COMMANDED BY THC
+#	  BIT 10	TRANSLATION IN -Y DIRECTION COMMANDED BY THC
+#	  BIT 11	TRANSLATION IN +Z DIRECTION COMMANDED BY THC
+#	  BIT 12	TRANSLATION IN -Z DIRECTION COMMANDED BY THC
 # Page 59
-#		BIT 13		ATTITUDE HOLD MODE ON SCS MODE CONTROL SWITCH
-#		BIT 14		AUTO STABILIZATION OF ATTITUDE ON SCS MODE SWITCH
-#		BIT 15		ATTITUDE CONTROL OUT OF DETENT (RHC NOT IN NEUTRAL)
+#	  BIT 13	ATTITUDE HOLD MODE ON SCS MODE CONTROL SWITCH
+#	  BIT 14	AUTO STABILIZATION OF ATTITUDE ON SCS MODE SWITCH
+#	  BIT 15	ATTITUDE CONTROL OUT OF DETENT (RHC NOT IN NEUTRAL
 
-# CHANNEL 32	INPUT CHANNEL.
+#	CHANNEL 32	   INPUT CHANNEL.
 #
-#		BIT 1		THRUSTERS 2 & 4 DISABLED BY CREW
-#		BIT 2		THRUSTERS 5 & 8 DISABLED BY CREW
-#		BIT 3		THRUSTERS 1 & 3 DISABLED BY CREW
-#		BIT 4		THRUSTERS 6 & 7 DISABLED BY CREW
-#		BIT 5		THRUSTERS 14 & 16 DISABLED BY CREW
-#		BIT 6		THRUSTERS 13 & 15 DISABLED BY CREW
-#		BIT 7		THRUSTERS 9 & 12 DISABLED BY CREW
-#		BIT 8		THRUSTERS 10 & 11 DISABLED BY CREW
-#		BIT 9		DESCENT ENGINE DISABLED BY CREW
-#		BIT 10		APPARENT DESCENT ENGINE GIMBAL FAILURE
-#		BIT 14		INDICATES PROCEED KEY IS DEPRESSED
+#	  BIT 1		   THRUSTERS 2 & 4 DISABLED BY CREW
+#	  BIT 2		   THRUSTERS 5 & 8 DISABLED BY CREW
+#	  BIT 3		   THRUSTERS 1 & 3 DISABLED BY CREW
+#	  BIT 4		   THRUSTERS 6 & 7 DISABLED BY CREW
+#	  BIT 5		   THRUSTERS 14 & 16 DISABLED BY CREW
+#	  BIT 6		   THRUSTERS 13 & 15 DISABLED BY CREW
+#	  BIT 7		   THRUSTERS 9 & 12 DISABLED BY CREW
+#	  BIT 8		   THRUSTERS 10 & 11 DISABLED BY CREW
+#	  BIT 9		   DESCENT ENGINE GIMBALS DISABLED BY CREW
+#	  BIT 10	   APPARENT DESCENT ENGINE GIMBAL FAILURE
+#	  BIT 14	INDICATES PROCEED KEY IS DEPRESSED
 
-# CHANNEL 33	CHAN33: INPUT CHANNEL; FOR HARDWARE STATUS AND COMMAND INFORMATION.  BITS 15-11 ARE FLIP-
-#		FLOP BITS RESET BY A CHANNEL "WRITE" COMMAND THAT ARE RESET BY A RESTART & BY T4RUPT LOOP.
+#	CHANNEL 33	CHAN33; INPUT CHANNEL; FOR HARDWARE STATUS AND COMMAND INFORMATION. BITS 15-11 ARE FLIP-
+#			FLOP BITS RESET BY A CHANNEL "WRITE" COMMAND THAT ARE RESET BY A RESTART & BY T4RUPT LOOP.
 #
-#		BIT 1		SPARE
-#		BIT 2		RR AUTO-POWER ON
-#		BIT 3		RR RANGE LOW SCALE
-#		BIT 4		RR DATA GOOD
-#		BIT 5		LR RANGE DATA GOOD
-#		BIT 6		LR POS1
-#		BIT 7		LR POS2
+#	  BIT 1		SPARE
+#	  BIT 2		RR AUTO-POWER ON
+#	  BIT 3		RR RANGE LOW SCALE
+#	  BIT 4		RR DATA GOOD
+#	  BIT 5		LR RANGE DATA GOOD
+#	  BIT 6		LR POS1
+#	  BIT 7		LR POS2
 # Page 60
-#		BIT 8		LR VEL DATA GOOD
-#		BIT 9		LR RANGE LOW SCALE
-#		BIT 10		BLOCK UPLINK INPUT
-#		BIT 11		UPLINK TOO FAST
-#		BIT 12		DOWNLINK TOO FAST
-#		BIT 13		PIPA FAIL
-#		BIT 14		WARNING OF REPEATED ALARMS: RESTART, COUNTER FAIL, VOLTAGE FAIL, AND SCALAR DOUBLE.
-#		BIT 15		LGC OSCILLATOR STOPPED
-
-# CHANNEL 34	DNT M1: OUTPUT CHANNEL; DOWNLINK 1: FIRST OF TWO WORDS SERIALIZATION.
-# CHANNEL 35	DNT M2: OUTPUT CHANNEL; DOWNLINK 2: SECOND OF TWO WORDS SERIALIZATION.
+#	  BIT 8		LR VEL DATA GOOD
+#	  BIT 9		LR RANGE LOW SCALE
+#	  BIT 10	BLOCK UPLINK INPUT
+#	  BIT 11	UPLINK TOO FAST
+#	  BIT 12	DOWNLINK TOO FAST
+#	  BIT 13	PIPA FAIL
+#	  BIT 14	WARNING OF REPEATED ALARMS: RESTART,COUNTER FAIL, VOLTAGE FAIL,AND SCALAR DOUBLE.
+#	  BIT 15	LGC OSCILLATOR STOPPED
 
+#	CHANNEL 34	DNT M1; OUTPUT CHANNEL; DOWNLINK 1  FIRST OF TWO WORDS SERIALIZATION.
+#	CHANNEL 35	DNT M2; OUTPUT CHANNEL DOWNLINK 2 SOCOND OF TWO   WORDS SERIALIZATION.
 

Luminary099/INTEGRATION_INITIALIZATION.agc

@@ -729,13 +729,13 @@ DT/2COMP	DLOAD	DSU
 			GETMAXDT
 		DSU	BMN		# IS TIME TO INTEG. TO GR THAN MAXTIME
 			12D
-			P00HCHK
+			POOHCHK
 USEMAXDT	DLOAD	SIGN
 			12D
 			DT/2
 # Page 1219
 		STCALL	DT/2
-			P00HCHK
+			POOHCHK
 MAXDT		DLOAD	PDDL		# EXCHANGE DT/2MAX WITH COMPUTED MAX.
 			DT/2MAX
 		GOTO
@@ -744,7 +744,7 @@ GETMAXDT	RTB
 			SIGNMPAC
 		STCALL	DT/2
 			USEMAXDT
-P00HCHK		DLOAD	ABS
+POOHCHK		DLOAD	ABS
 			DT/2
 		DSU	BMN
 			DT/2MIN

Luminary099/INTER-BANK_COMMUNICATION.agc

@@ -28,8 +28,8 @@
 #	16:27 JULY 14, 1969
 
 # Page 998
-# THE FOLLOWING ROUTINE CAN BE USED TO CALL A SUBROUTINE IN ANOTHER BANK. IN THE BANKCALL VERSION, THE
-# CADR OF THE SUBROUTINE IMMEDIATELY FOLLOWS THE TC BANKCALL INSTRUCTION, WITH C(A) AND C(L) PRESERVED.
+# 	   THE FOLLOWING ROUTINE CAN BE USED TO CALL A SUBROUTINE IN ANOTHER BANK. IN THE BANKCALL VERSION, THE
+# CADR OF THE SUBROUTINE IMMEDIATELY FOLLOWS THE  TC BANKCALL  INSTRUCTION, WITH C(A) AND C(L) PRESERVED.
 
 		BLOCK	02
 		COUNT*	$$/BANK
@@ -38,7 +38,7 @@ BANKCALL	DXCH	BUF2		# SAVE INCOMING A,L.
 		CA	0
 		INCR	Q		# SO WE RETURN TO THE LOC. AFTER THE CADR.
 
-# SWCALL IS  IDENTICAL TO BANKCALL, EXCEPT THAT THE CADR ARRIVES IN A.
+# 	   SWCALL IS IDENTICAL TO BANKCALL, EXCEPT THAT THE CADR ARRIVES IN A.
 
 SWCALL		TS	L
 		LXCH	FBANK		# SWITCH BANKS, SAVING RETURN.
@@ -53,23 +53,23 @@ SWRETURN	XCH	BUF2 	+1	# COMES HERE TO RETURN TO CALLER. C(A,L)
 		XCH	BUF2 	+1
 		TC	BUF2
 
-# THE FOLLOWING ROUTINE CAN BE USED AS A UNILATERAL JUMP WITH C(A,L) PRESERVED AND THE CADR IMMEDIATELY
+# 	   THE FOLLOWING ROUTINE CAN BE USED AS A UNILATERAL JUMP WITH C(A,L) PRESERVED AND THE CADR IMMEDIATELY
 # FOLLOWING THE TC POSTJUMP INSTRUCTION.
 
 POSTJUMP	XCH	Q		# SAVE INCOMING C(A).
 		INDEX	A		# GET CADR.
 		CA	0
 
-# BANKJUMP IS THE SAME AS POSTJUMP, EXCEPT THAT THE CADR ARRIVES IN A.
+# 	   BANKJUMP IS THE SAME AS POSTJUMP, EXCEPT THAT THE CADR ARRIVES IN A.
 
 BANKJUMP	TS	FBANK
 		MASK	LOW10
 		XCH	Q		# RESTORING INPUT C(A) IF THIS WAS A
 Q+10000		INDEX	Q		# POSTJUMP.
-PRIO12		TCF	10000		# PRIO12 = TCF	10000 = 12000
+PRIO12		TCF	10000		# PRIO12 = TCF	 10000 = 12000
 
 # Page 999
-# THE FOLLOWING ROUTINE GETS THE RETURN CADR SAVED BY SWCALL OR BANKCALL AND LEAVES IT IN A.
+# 	   THE FOLLOWING ROUTINE GETS THE RETURN CADR SAVED BY SWCALL OR BANKCALL AND LEAVES IT IN A.
 
 MAKECADR	CAF	LOW10
 		MASK	BUF2
@@ -80,9 +80,9 @@ SUPDACAL	TS	MPTEMP
 		XCH	FBANK		# SET FBANK FOR DATA.
 		EXTEND
 		ROR	SUPERBNK	# SAVE FBANK IN BITS 15-11, AND
-		XCH	MPTEMP		# SUPERBANK IN BITS 7-5.
+		XCH	MPTEMP		#  SUPERBANK IN BITS  7-5.
 		MASK	LOW10
-		XCH	L		# SAVE REL. ADR. IN BANK, FETCH SUPERBITS
+		XCH	L		# SAVE REL. ADR. IN BANK, FETCH SUPERBITS.
 		INHINT			# BECAUSE RUPT DOES NOT SAVE SUPERBANK.
 		EXTEND
 		WRITE	SUPERBNK	# SET SUPERBANK FOR DATA.
@@ -97,7 +97,7 @@ SUPDACAL	TS	MPTEMP
 		RETURN			# 24 WDS. DATACALL 516 MU, SUPDACAL 432 MU
 
 # Page 1000
-# THE FOLLOWING ROUTINES ARE IDENTICAL TO BANKCALL AND SWCALL EXCEPT THAT THEY ARE USED IN INTERRUPT.
+# 	   THE FOLLOWING ROUTINES ARE IDENTICAL TO BANKCALL AND SWCALL EXCEPT THAT THEY ARE USED IN INTERRUPT.
 
 IBNKCALL	DXCH	RUPTREG3	# USES RUPTREG3,4 FOR DP RETURN ADDRESS.
 		INDEX	Q
@@ -118,9 +118,10 @@ ISWRETRN	XCH	RUPTREG4
 		TC	RUPTREG3
 
 # 2. USPRCADR ACCESSES INTERPRETIVE CODING IN OTHER THAN THE USER'S FBANK.  THE CALLING SEQUENCE IS AS FOLLOWS:
-#	L	TC	USPRCADR
-#	L+1	CADR	INTPRETX	# INTPRETX IS THE INTERPRETIVE CODING
-#					# RETURN IS TO L+2
+
+# L		TC	USPRCADR
+# L+1		CADR	INTPRETX	  INTPRETX IS THE INTERPRETIVE CODING
+#					  RETURN IS TO L+2
 
 USPRCADR	TS	LOC		# SAVE A
 		CA	BIT8
@@ -136,40 +137,41 @@ USPRCADR	TS	LOC		# SAVE A
 		TCF	Q+10000
 
 # Page 1001
-# THERE ARE FOUR POSSIBLE SETTINGS FOR CHANNEL 07.  (CHANNEL 07 CONTAINS SUPERBANK SETTING.)
+# THERE ARE FOUR POSSIBLE SETTINGS FOR CHANNEL 07. (CHANNEL 07 CONTAINS SUPERBANK SETTING.)
+#					    PSEUDO-FIXED      OCTAL PSEUDO
+# SUPERBANK	SETTING	    S-REG. VALUE    BANK NUMBERS      ADDRESSES
+# ----------	-------	    ------------     ------------      ------------
 #
-#					PSEUDO-FIXED	  OCTAL PSEUDO
-# SUPERBANK	SETTING	S-REG. VALUE	BANK NUMBERS	   ADDRESSES
-# ---------	-------	------------	------------	   ---------
-# SUPERBANK 3	  OXX	 2000 - 3777	   30 - 37	 70000 - 107777		(WHERE XX CAN BE ANYTHING AND
+# SUPERBANK 3	  OXX	    2000 - 3777	       30 - 37	      70000 - 107777	(WHERE XX CAN BE ANYTHING AND
 #										WILL USUALLY BE SEEN AS 11)
-# SUPERBANK 4	  100	 2000 - 3777	   40 - 47	110000 - 127777		(AS FAR AS IT CAN BE SEEN,
+# SUPERBANK 4	  100	    2000 - 3777        40 - 47	      110000 - 127777	(AS FAR AS IT CAN BE SEEN,
 #										ONLY BANKS 40-43 WILL EVER BE
 #										AND ARE PRESENTLY AVAILABLE)
-# SUPERBANK 5	  101	 2000 - 3777	   50 - 57	130000 - 147777		(PRESENTLY NOT AVAILABLE TO
+# SUPERBANK 5	  101	    2000 - 3777	       50 - 57	      130000 - 147777	(PRESENTLY NOT AVAILABLE TO
 #										THE USER)
-# SUPERBANK 6	  110	 2000 - 3777	   60 - 67	150000 - 167777		(PRESENTLY NOT AVAILABLE TO
+# SUPERBANK 6	  110	    2000 - 3777	       60 - 67	      150000 - 167777	(PRESENTLY NOT AVAILABLE TO
 #										THE USER)
-# *** THIS ROUTINE MAY BE CALLED BY ANY PROGRAM LOCATED IN BANKS 00 - 27.  I.E., NO PROGRAM LIVING IN ANY
-# SUPERBANK SHOULD USE SUPERSW. ***
+# ***  THIS ROUTINE MAYBE CALLED BY ANY PROGRAM LOCATED IN BANKS 00 - 27.  I.E., NO PROGRAM LIVING IN ANY
+# SUPERBANK SHOULD USE SUPERSW.  ***
 #
-# SUPERSW MAY BE CALLED IN THIS FASHION:
-#	CAF	ABBCON		WHERE -- ABBCON  BBCON  SOMETHING --
-#	TCR	SUPERSW		(THE SUPERBNK BITS ARE IN THE BBCON)
-#	...	  ...
-#	 .	   .
-#	 .	   .
-# OR IN THIS FASHION:
-#	CAF	SUPERSET	WHERE SUPERSET IS ONE OF THE FOUR AVAILABLE
-#	TCR	SUPERSW		SUPERBANK BIT CONSTANTS:
-#	...	  ...			SUPER011 OCTAL  60
-#	 .	   .			SUPER100 OCTAL 100
-#	 .	   .			SUPER101 OCTAL 120
-#					SUPER110 OCTAL 140
+# SUPERSW MAYBE CALLED IN THIS FASHION:
+#
+#	   CAF	  ABBCON	  WHERE  --  ABBCON   BBCON  SOMETHIN  --
+#	   TCR	  SUPERSW	  (THE SUPERBNK BITS ARE IN THE BBCON)
+#	   ...	    ...
+#	    .	     .
+#	    .	     .
+# OR IN THIS FASHION :
+#	   CAF	  SUPERSET	  WHERE SUPERSET IS ONE OF THE FOUR AVAILABLE
+#	   TCR	  SUPERSW	  SUPERBANK BIT CONSTANTS:
+#	   ...	    ...					  SUPER011 OCTAL  60
+#	    .	     .					  SUPER100 OCTAL 100
+#	    .	     .					  SUPER101 OCTAL 120
+#							  SUPER110 OCTAL 140
 
 SUPERSW		EXTEND
 		WRITE	SUPERBNK	# WRITE BITS 7-6-5 OF THE ACCUMULATOR INTO
 					# CHANNEL 07
 		TC	Q		# TC TO INSTRUCTION FOLLOWING
-					# 	TC SUPERSW
+					#   TC  SUPERSW
 

Luminary099/INTERRUPT_LEAD_INS.agc

@@ -39,7 +39,7 @@
 		DCA	T6ADR
 		DTCB
 
-		DXCH	ARUPT		# T5RUPT -- AUTOPILOT
+		DXCH	ARUPT		# T5RUPT - AUTOPILOT
 		EXTEND
 		DCA	T5ADR
 		DTCB

Luminary099/KALCMANU_STEERING.agc

@@ -37,7 +37,7 @@
 NEWDELHI	TC	BANKCALL	# CHECK FOR AUTO STABILIZATION
 		CADR	ISITAUTO	# ONLY
 		CCS	A
-		TCF	NOGO 	-2
+		TCF	NOGO -2
 NEWANGL		TC	INTPRET
 		AXC,1	AXC,2
 			MIS		# COMPUTE THE NEW MATRIX FROM S/C TO
@@ -45,9 +45,9 @@ NEWANGL		TC	INTPRET
 		CALL
 			MXM3
 		VLOAD	STADR
-		STOVL	MIS 	+12D	# CALCULATE NEW DESIRED CDU ANGLES
+		STOVL	MIS +12D	# CALCULATE NEW DESIRED CDU ANGLES
 		STADR
-		STOVL	MIS 	+6D
+		STOVL	MIS +6D
 		STADR
 		STORE	MIS
 		AXC,1	CALL
@@ -59,7 +59,7 @@ NEWANGL		TC	INTPRET
 		BONCLR	EXIT
 			CALCMAN2
 			MANUSTAT	# TO START MANEUVER
-		CAF	TWO		#	+0 OTHERWISE
+		CAF	TWO		#	   +0 OTHERWISE
 INCRDCDU	TS	SPNDX
 		INDEX	SPNDX
 		CA	BCDU		# INITIAL CDU ANGLES
@@ -67,16 +67,10 @@ INCRDCDU	TS	SPNDX
 		INDEX	SPNDX
 		MSU	NCDU
 		EXTEND
-
-		# The following 2 lines seem to have no purpose at all.
-		# I am removing them because they only serve to confuse
-		# the assembler by getting in between EXTEND and MP.
-		#					--- RSB 2009.
-		#SETLOC	KALCMON1
-		#BANK
-
+		SETLOC	KALCMON1
+		BANK
 		MP	DT/TAU
-		CCS	A		# CONVERT TO 2'S COMPLEMENT
+		CCS	A		# CONVERT TO 2S COMPLEMENT
 		AD	ONE
 		TCF	+2
 		COM
@@ -94,7 +88,7 @@ INCRDCDU	TS	SPNDX
 
 		RELINT
 
-# COMPARE PRESENT TIME WTIH TIME TO TERMINATE MANEUVER
+# COMPARE PRESENT TIME WITH TIME TO TERMINATE MANEUVER
 
 TMANUCHK	TC	TIMECHK
 		TCF	CONTMANU
@@ -117,11 +111,11 @@ TIMECHK		EXTEND
 		TC	Q
 		TCF	+2
 		TCF	2NDRETRN
-		CCS	TTEMP 	+1
+		CCS	TTEMP +1
 		TC	Q
 		TCF	MANUOFF
 		COM
-MANUOFF		AD	ONESEK 	+1
+MANUOFF		AD	ONESEK +1
 		EXTEND
 		BZMF	2NDRETRN
 		INCR	Q
@@ -134,7 +128,7 @@ MANUSTAT	EXIT			# INITIALIZATION ROUTINE
 		EXTEND			# FOR AUTOMATIC MANEUVERS
 		DCA	TIME2
 # Page 367
-		DAS	TM		# TM+TO		MANEUVER COMPLETION TIME
+		DAS	TM		# TM+TO	   MANEUVER COMPLETION TIME
 		EXTEND
 		DCS	ONESEK
 		DAS	TM		# (TM+TO)-1
@@ -157,14 +151,14 @@ RATEBIAS	TS	KSPNDX
 		MP	BRATE
 		EXTEND
 		INDEX	KSPNDX
-		DV	1JACC		# = AJX		$ 90 DEG/SEC-SEC
+		DV	1JACC		# =AJX	$ 90 DEG/SEC-SEC
 		INDEX	KSPNDX
-		TS	DELPEROR	#		$ 180 DEG
+		TS	DELPEROR	#     $ 180 DEG
 		CCS	KSPNDX
 		TCF	RATEBIAS
 
 		CA	TIME1
-		AD	ONESEK 	+1
+		AD	ONESEK +1
 		XCH	NEXTIME
 		TCF	INCRDCDU -1
 
@@ -185,7 +179,7 @@ MANUCALL	INHINT			# CALL FOR NEXT UPDATE VIA WAITLIST
 		EBANK=	TTEMP
 		2CADR	UPDTCALL
 # Page 368
-		CAF	ONESEK 	+1	# INCREMENT TIME FOR NEXT UPDATE
+		CAF	ONESEK +1	# INCREMENT TIME FOR NEXT UPDATE
 		ADS	NEXTIME
 		TCF	ENDOFJOB
 
@@ -213,7 +207,7 @@ MANUSTOP	CAF	ZERO		# ZERO MANEUVER RATES
 ENDROLL		CA	CPHI		# NO FINAL YAW
 		TS	CDUXD
 		CAF	ZERO
-		TS	OMEGAPD		# I.E., MANEUVER DID NOT GO THRU
+		TS	OMEGAPD		# I.E. MANEUVER DID NOT GO THRU
 		TS	DELDCDU		# GIMBAL LOCK ORIGINALLY
 		TS	DELPEROR
 GOODMANU	CA	ATTPRIO		# RESTORE USERS PRIO
@@ -225,5 +219,3 @@ GOODMANU	CA	ATTPRIO		# RESTORE USERS PRIO
 		TC	SPVAC		# RETURN TO USER
 
 		TC	TASKOVER
-
-

Luminary099/KALMAN_FILTER.agc

@@ -68,7 +68,7 @@ LOOPRATE	EXTEND
 		EXTEND
 		BZMF	NEGTORK
 STORTORK	INDEX	Q		# INCREMENT DOWNLIST REGISTER.
-		ADS	DOWNTORK	#	NOTE:  NOT INITIALIZED; OVERFLOWS.
+		ADS	DOWNTORK	#   NOTE: NOT INITIALIZED; OVERFLOWS.
 
 		CCS	DAPTEMP6
 		TCF	RATELOOP +1

Luminary099/KEYRUPT_UPRUPT.agc

@@ -51,7 +51,7 @@ ACCEPTUP	CAF	CHRPRIO		# (NOTE: RUPTREG4 = KEYTEMP1)
 
 		CA	RUPTREG4
 		INDEX	LOCCTR
-		TS	MPAC		# LEAVE 5 BIT KEY CODE IN MPAC FOR CHARIN
+		TS	MPAC		# LEAVE 5 BIT KEY CDE IN MPAC FOR CHARIN
 		TC	RESUME
 
 # Page 1339
@@ -83,9 +83,9 @@ UPRPT1		CAF	LOW5		# TEST FOR TRIPLE CHAR REDUNDANCY
 		COM
 		TC	UPTEST
 
-UPCK		CS	ELRCODE		# CODE IS GOOD.  IF CODE = `ERROR RESET',
-		AD	KEYTEMP1	# CLEAR UPLOCKFL (SET BIT4 OF FLAGWRD7 = 0)
-		EXTEND			# IF CODE DOES NOT = `ERROR RESET', ACCEPT
+UPCK		CS	ELRCODE		# CODE IS GOOD. IF CODE = 'ERROR RESET',
+		AD	KEYTEMP1	# CLEAR UPLOCKFL(SET BIT4 OF FLAGWRD7 = 0)
+		EXTEND			# IF CODE DOES NOT = 'ERROR RESET', ACCEPT
 		BZF	CLUPLOCK	# CODE ONLY IF UPLOCKFL IS CLEAR (=0).
 
 		CAF	UPLOCBIT	# TEST UPLOCKFL FOR 0 OR 1
@@ -94,7 +94,7 @@ UPCK		CS	ELRCODE		# CODE IS GOOD.  IF CODE = `ERROR RESET',
 		TC	RESUME		# UPLOCKFL = 1
 		TC	ACCEPTUP	# UPLOCKFL = 0
 
-CLUPLOCK	CS	UPLOCBIT	# CLEAR UPLOCKFL (I.E., SET BIT 4 OF
+CLUPLOCK	CS	UPLOCBIT	# CLEAR UPLOCKFL (I.E.,SET BIT 4 OF )
 		MASK	FLAGWRD7	# FLAGWRD7 = 0)
 		TS	FLAGWRD7
 		TC	ACCEPTUP
@@ -102,7 +102,7 @@ CLUPLOCK	CS	UPLOCBIT	# CLEAR UPLOCKFL (I.E., SET BIT 4 OF
 					# CODE IS BAD
 TMFAIL2		CS	FLAGWRD7	# LOCK OUT FURTHER UPLINK ACTIVITY
 		MASK	UPLOCBIT	# (BY SETTING UPLOCKFL = 1) UNTIL
-		ADS	FLAGWRD7	# `ERROR RESET' IS SENT VIA UPLINK.
+		ADS	FLAGWRD7	# 'ERROR RESET' IS SENT VIA UPLINK.
 		TC	RESUME
 UPTEST		AD	KEYTEMP1
 # Page 1340
@@ -114,19 +114,17 @@ HI10		OCT	77740
 
 ELRCODE		OCT	22
 
-# `UPLINK ACTIVITY LIGHT' IS TURNED OFF BY .....
-#	1.	VBRELDSP
-#	2.	ERROR RESET
-#	3.	UPDATE PROGRAM (P27) ENTERED BY V70,V71,V72, AND V73.
-#				      _
-# THE RECEPTION OF A BAD CODE (I.E., CCC FAILURE) LOCKS OUT FURTHER UPLINK ACTIVITY BY SETTING BIT4 OF FLAGWRD7 = 1.
-# THIS INDICATION WILL BE TRANSFERRED TO THE GROUND BY THE DOWNLINK WHICH DOWNLINKS ALL FLAGWORDS.
-# WHEN UPLINK ACTIVITY IS LOCKED OUT, IT CAN BE ALLOWED WHEN THE GROUND UPLINKS AND `ERROR RESET' CODE.
-# (IT IS RECOMMENDED THAT THE `ERROR LIGHT RESET' CODE IS PRECEEDED BY 16 BITS THE FIRST OF WHICH IS 1 FOLLOWED
-# BY 15 ZEROS.  THIS WILL ELIMINATE EXTRANEOUS BITS FROM INLINK WHICH MAY HAVE BEEN LEFT OVER FROM THE ORIGINAL
-# FAILURE).
+# 'UPLINK ACTIVITY LIGHT' IS TURNED OFF BY .....
+#	   1.	  VBRELDSP
+#	   2.	  ERROR RESET
+#	   3.	  UPDATE PROGRAM(P27) ENTERED BY V70,V71,V72,AND V73.
 #
-# UPLINK ACTIVITY IS ALSO ALLOWED (UNLOCKED) DURING FRESH START WHEN FRESH START SETS BIT4 OF FLAGWRD7 = 0.
-
+#				    _
+# THE RECEPTION OF A BAD CODE(I.E  CCC FAILURE) LOCKS OUT FURTHER UPLINK ACTIVITY BY SETTING BIT4 OF FLAGWRD7 = 1.
+# THIS INDICATION WILL BE TRANSFERRED TO THE GROUND BY THE DOWNLINK WHICH DOWNLINKS ALL FLAGWORDS.
+# WHEN UPLINK ACTIVITY IS LOCKED OUT ,IT CAN BE ALLOWED WHEN THE GROUND UPLINKS AND 'ERROR RESET' CODE.
+# (IT IS RECOMMENDED THAT THE 'ERROR LIGHT RESET' CODE IS PRECEEDED BY 16 BITS THE FIRST OF WHICH IS 1 FOLLOWED
+# BY 15 ZEROES. THIS WILL ELIMINATE EXTRANEOUS BITS FROM INLINK WHICH MAY HAVE BEEN LEFT OVER FROM THE ORIGINAL
+# FAILURE)
+# UPLINK ACTIVITY IS ALSO ALLOWED(UNLOCKED) DURING FRESH START WHEN FRESH START SETS BIT4 OF FLAGWRD7 = 0.
 		CS	XDSPBIT
-

Luminary099/LANDING_ANALOG_DISPLAYS.agc

@@ -53,10 +53,10 @@ ALTROUT		TC	DISINDAT	# CHECK MODE SELECT SWITCH AND DIDFLG.
 		CAF	BIT2		# RATE COMMAND IS EXECUTED BEFORE RANGE.
 		EXTEND
 		WOR	CHAN14		# ALTRATE (BIT2 = 1), ALTITUDE (BIT2 = 0).
-ARCOMP		CA	RUNIT		# COMPUTE ALTRATE = RUNIT.VVECT M/CS *(-6).
+ARCOMP		CA	RUNIT		# COMPUTE ALTRATE=RUNIT.VVECT M/CS *2(-6).
 		EXTEND
 		MP	VVECT		# MULTIPLY X-COMPONENTS.
-		XCH	RUPTREG1	# SAVE SINGLE PRECISION RESULT M/CS*2(-6)
+		XCH	RUPTREG1	# SAVE SINGLE PRECISION RESULT M/CS*2(-6).
 		CA	RUNIT +1	# MULTIPLY Y-COMPONENTS.
 		EXTEND
 		MP	VVECT +1
@@ -80,10 +80,10 @@ ARCOMP		CA	RUNIT		# COMPUTE ALTRATE = RUNIT.VVECT M/CS *(-6).
 # Page 899
 		EXTEND			# CHECK POLARITY OF ALTITUDE RATE.
 		BZMF	+2
-		TCF	DATAOUT		# NEGATIVE -- SEND POS. PULSES TO ALTM REG.
-		CA	ALTRATE		# POSITIVE OR ZERO -- SET SIGN BIT = 1 AND
-		AD	BIT15		# SEND TO ALTM REGISTER.  *DO NOT SEND +0*
-DATAOUT		TS	ALTM		# ACTIVATE THE LANDING ANALOG DISPLAYS
+		TCF	DATAOUT		# NEGATIVE - SEND POS. PULSES TO ALTM REG.
+		CA	ALTRATE		# POSITIVE OR ZERO - SET SIGN BIT = 1 AND
+		AD	BIT15		# SEND TO ALTM REGISTER. *DO NOT SEND +0*
+DATAOUT		TS	ALTM		# ACTIVATE THE LANDING ANALOG DISPLAYS - -
 		CAF	BIT3
 		EXTEND
 		WOR	CHAN14		# BIT3 DRIVES THE ALT/ALTRATE METER.
@@ -96,13 +96,13 @@ ALTOUT		TC	DISINDAT	# CHECK MODE SELECT SWITCH AND DIDFLG.
 		CS	BIT2
 		EXTEND
 		WAND	CHAN14
-		CCS	ALTBITS		# = -1 IF OLD ALT. DATA TO BE EXTRAPOLATED.
+		CCS	ALTBITS		# =-1 IF OLD ALT. DATA TOBE EXTRAPOLATED.
 		TCF	+4
 		TCF	+3
 		TCF	OLDDATA
 		TS	ALTBITS		# SET ALTBITS FROM -0 TO +0.
 		CS	ONE
-		DXCH	ALTBITS		# SET ALTBITS = -1 FOR SWITCH USE NEXT PASS.
+		DXCH	ALTBITS		# SET ALTBITS=-1 FOR SWITCH USE NEXT PASS.
 		DXCH	ALTSAVE
 		CA	BIT10		# NEW ALTITUDE EXTRAPOLATION WITH ALTRATE.
 		XCH	Q
@@ -150,11 +150,11 @@ DISINDAT	EXTEND
 		RAND	CHAN30		# DISPLAYS?  I.E.,
 		CCS	A		# IS THE MODE SELECT SWITCH IN PGNCS?
 		TCF	DISPRSET	# NO.  ASTRONAUT REQUESTS NO INERTIAL DATA
-		CS	FLAGWRD1	# YES.  CHECK STATUS OF DIDFLAG.
+		CS	FLAGWRD1	# YES. CHECK STATUS OF DIDFLAG.
 		MASK	DIDFLBIT
 		EXTEND
-		BZF	SPEEDRUN	# SET.  PERFORM DATA DISPLAY SEQUENCE.
-		CS	FLAGWRD1	# RESET.  PERFORM INITIALIZATION FUNCTIONS.
+		BZF	SPEEDRUN	# SET. PERFORM DATA DISPLAY SEQUENCE.
+		CS	FLAGWRD1	# RESET. PERFORM INITIALIZATION FUNCTIONS.
 		MASK	DIDFLBIT
 		ADS	FLAGWRD1	# SET DIDFLAG.
 		CS	BIT7
@@ -262,24 +262,24 @@ SPEEDRUN	CS	PIPTIME +1	# UPDATE THE VELOCITY VECTOR
 
 		CA	DELVS		# HI X OF VELOCITY CORRECTION TERM.
 		AD	VVECT		# HI X OF UPDATED VELOCITY VECTOR.
-		TS	ITEMP1		# = VX - DVX M/CS *2(-5).
+		TS	ITEMP1		# = VX - DVX M/CS*2(-5).
 		CA	DELVS +2	#    Y
 		AD	VVECT +1	#    Y
-		TS	ITEMP2		# = VY - DVY M/CS *2(-5)
+		TS	ITEMP2		# = VY - DVY M/CS*2(-5).
 		CA	DELVS +4	#    Z
 		AD	VVECT +2	#    Z
-		TS	ITEMP3		# = VZ - DVZ M/CS *2(-5)
+		TS	ITEMP3		# = VZ - DVZ M/CS*2(-5).
 		CA	ITEMP1		# COMPUTE VHY, VELOCITY DIRECTED ALONG THE
 		EXTEND			# Y-COORDINATE.
-		MP	UHYP		# HI X OF CROSS-RANGE HALF-UNIT VECTOR
+		MP	UHYP		# HI X OF CROSS-RANGE HALF-UNIT VECTOR.
 		XCH	RUPTREG1
 		CA	ITEMP2
 		EXTEND
-		MP	UHYP +2		# Y
+		MP	UHYP +2		#    Y
 		ADS	RUPTREG1	# ACCUMULATE PARTIAL PRODUCTS.
 		CA	ITEMP3
 		EXTEND
-		MP	UHYP +4		# Z
+		MP	UHYP +4		#    Z
 		ADS	RUPTREG1
 # Page 903
 		CA	RUPTREG1
@@ -291,11 +291,11 @@ SPEEDRUN	CS	PIPTIME +1	# UPDATE THE VELOCITY VECTOR
 		XCH	RUPTREG1
 		CA	ITEMP2
 		EXTEND
-		MP	UHZP +2		# Y
+		MP	UHZP +2		#    Y
 		ADS	RUPTREG1	# ACCUMULATE PARTIAL PRODUCTS.
 		CA	ITEMP3
 		EXTEND
-		MP	UHZP +4		# Z
+		MP	UHZP +4		#    Z
 		ADS	RUPTREG1
 		CA	RUPTREG1
 		DOUBLE
@@ -317,7 +317,7 @@ LATFWDV		CA	ITEMP4		# COMPUTE LATERAL AND FORWARD VELOCITIES.
 		CA	ITEMP3
 		EXTEND
 		MP	VHZ
-		ADS	RUPTREG1	# = VHY(COS)AOG+VHZ(SIN)AOG M/CS *2(-5)
+		ADS	RUPTREG1	# =VHY(COS)AOG+VHZ(SIN)AOG M/CS *2(-5)
 		CA	VELCONV		# CONVERT LATERAL VELOCITY TO BIT UNITS.
 		EXTEND
 		MP	RUPTREG1
@@ -344,7 +344,7 @@ LATFWDV		CA	ITEMP4		# COMPUTE LATERAL AND FORWARD VELOCITIES.
 
 		CAF	ONE		# LOOP TWICE.
 VMONITOR	TS	ITEMP5		# FORWARD AND LATERAL VELOCITY LANDING
-		INDEX	ITEMP5		#	ANALOG DISPLAYS MONITOR.
+		INDEX	ITEMP5		#    ANALOG DISPLAYS MONITOR.
 		CCS	LATVEL
 		TCF	+4
 		TCF	LVLIMITS
@@ -427,7 +427,6 @@ LVLIMITS	INDEX	ITEMP5
 		BZMF	+2
 		TCF	NEGLMLV
 		INDEX	ITEMP5
-
 		CS	LATVEL
 		EXTEND
 		BZMF	LVMINLM
@@ -500,11 +499,11 @@ ZEROLSTY	INDEX	ITEMP5
 		EXTEND
 		WOR	CHAN14
 		TC	LADQSAVE	# GO TO ALTROUT +1 OR TO ALTOUT +1
-ZERODATA	CAF	ZERO		# ZERO ALTSAVE AND ALTSAVE +1
-		TS	L		#	NO NEGATIVE ALTITUDES ALLOWED.
+ZERODATA	CAF	ZERO		# ZERO ALTSAVE AND ALTSAVE +1 - - -
+		TS	L		#	 NO NEGATIVE ALTITUDES ALLOWED.
 		TCF	ZDATA2
 
-# ****************************************************************************
+# ************************************************************************
 
 DISPRSET	CS	FLAGWRD0	# ARE WE IN DESCENT TRAJECTORY?
 		MASK	R10FLBIT
@@ -514,7 +513,7 @@ DISPRSET	CS	FLAGWRD0	# ARE WE IN DESCENT TRAJECTORY?
 		MASK	IMODES33	# CHECK IF INERTIAL DATA JUST DISPLAYED.
 		CCS	A
 		CAF	BIT2		# YES. DISABLE RR ERROR COUNTER
-		AD	BIT8		# NO.  REMOVE DISPLAY INERTIAL DATA
+		AD	BIT8		# NO. REMOVE DISPLAY INERTIAL DATA
 		COM
 		EXTEND
 		WAND	CHAN12
@@ -525,12 +524,10 @@ ABORTON		CS	BITS8/7		# RESET INERTIAL DATA, INTERLEAVE FLAGS.
 		MASK	FLAGWRD1
 		TS	FLAGWRD1	# RESET DIDFLAG.
 		TCF	TASKOVER
-
-# ******************************************************************************
-
+# ************************************************************************
 BITS8/7		OCT	00300		# INERTIAL DATA AND INTERLEAVE FLAGS.
+
 BITSET		=	PRIO6
-
-# ******************************************************************************
+# ************************************************************************
 
 

Luminary099/LATITUDE_LONGITUDE_SUBROUTINES.agc

@@ -29,24 +29,24 @@
 # SUBROUTINE TO CONVERT RAD VECTOR AT GIVEN TIME TO LAT,LONG AND ALT
 #
 # CALLING SEQUENCE
-#	L-1	CALL
-#	L		LAT-LONG
 #
+#   L-1	   CALL
+#   L		  LAT-LONG
 # SUBROUTINES USED
-#	R-TO-RP, ARCTAN, SFTGAMMA, SETRE
 #
+#  R-TO-RP,ARCTAN,SETGAMMA,SETRE
 # ERASABLE INIT. REQ.
-#	AXO, -AYO, AZO, TEPHEM (SET AT LAUNCH TIME)
-#	ALPHAV = POSITION VECTOR METERS B-29
-#	MPAC -- TIME (CSECS B-28)
-#	ERADFLAG =1, TO COMPUTE EARTH RADIUS, =0 FOR FIXED EARTH RADIUS
-#	LUNAFLAG=0 FOR EARTH, 1 FOR MOON
 #
+#   AXO,-AYO,AZO,TEPHEM (SET AT LAUNCH TIME)
+# ALPHAV = POSITION VECTOR METERS B-29
+#   MPAC-- TIME  (CSECS B-28)
+#  ERADFLAG =1, TO COMPUTE EARTH RADIUS, =0 FOR FIXED EARTH RADIUS
+#  LUNAFLAG=0 FOR EARTH,1 FOR MOON
 # OUTPUT
-#	LATITUDE IN LAT 	(REVS. B-0)
-#	LONGITUDE IN LONG	(REVS. B-0)
-#	ALTITUDE IN ALT 	METERS B-29
-
+#
+#   LATITUDE IN LAT   (REVS. B-0)
+#   LONGITUDE IN LONG	(REVS. B-0)
+# ALTITUDE IN ALT METERS B-29
 		BANK	30
 		SETLOC	LATLONG
 		BANK
@@ -60,16 +60,16 @@ LAT-LONG	STQ	SETPD
 			ALPHAV
 		PUSH	ABVAL		# 0-5D= R FOR R-TO-RP
 		STODL	ALPHAM		# ABS. VALUE OF R FOR ALT FORMULA BELOW
-			ZEROVEC		# SET MPAC=0 FOR EARTH, NON-ZERO FOR MOON
+			ZEROVEC		# SET MPAC=0 FOR EARTH,NON-ZERO FOR MOON
 		BOFF	COS		# USE COS(0) TO GET NON-ZERO IN MPAC
-			LUNAFLAG	# 0=EARTH, 1=MOON
+			LUNAFLAG	# 0=EARTH,1=MOON
 			CALLRTRP
 CALLRTRP	CALL
 			R-TO-RP		# RP VECTOR CONVERTED FROM R B-29
 		UNIT			# UNIT RP B-1
 		STCALL	ALPHAV		# U2= 1/2 SINL FOR SETRE SUBR BELOW
-			SETGAMMA	#	SET GAMMA=B2/A2 FOR EARTH, =1 FOR MOON
-		CALL			#	SCALED B-1
+			SETGAMMA	#  SET GAMMA=B2/A2 FOR EARTH,=1 FOR MOON
+		CALL			#  SCALED B-1
 			SETRE		# CALC RE METERS B-29
 		DLOAD	DSQ
 			ALPHAV
@@ -96,49 +96,48 @@ CALLRTRP	CALL
 		STCALL	ALT		# EXIT WITH ALT METERS B-29
 			INCORPEX
 # Page 1135
-# SUBROUTINE TO CONVERT LAT,LONG.ALT AT GIVEN TIME TO RADIUS VECTOR
-#
+# SUBROUTINE TO CONVERT LAT,LONG,ALT AT GIVEN TIME TO RADIUS VECTOR
 # CALLING SEQUENCE
-#	L-1	CALL
-#	L		LALOTORV
 #
+#   L-1	   CALL
+#   L		  LALOTORV
 # SUBROUTINES USED
-#	SETGAMMA, SETRE, RP-TO-R
 #
+#  SETGAMMA,SETRE,RP-TO-R
 # ERASABLE INIT. REQ.
-#	AXO, AYO, AZO, TEPHEM SET AT LAUNCH TIME
-#	LAT -- LATITUDE 	(REVS B0)
-#	LONG -- LONGITUDE	(REVS B0)
-#	ALT -- ALTITUDE		(METERS) B-29
-#	MPAC -- TIME		(CSECS B-28)
-#	ERADFLAG =1 TO COMPUTE EARTH RADIUS, =0 FOR FIXED EARTH RADIUS
-#	LUNAFLAG=0 FOR EARTH, 1 FOR MOON
 #
+#   AXO,AYO,AZO,TEPHEM  SET AT LAUNCH TIME
+#   LAT-- LATITUDE  (REVS B0)
+#   LONG-- LONGITUDE  (REVS B0)
+# ALT--ALTITUDE	(METERS) B-29
+#   MPAC-- TIME	 (CSECS B-28)
+#   ERADFLAG =1 TO COMPUTE EARTH RADIUS, =0 FOR FIXED EARTH RADIUS
+#  LUNAFLAG=0 FOR EARTH,1 FOR MOON
 # OUTPUT
-#	R-VECTOR IN ALPHAV 	(METERS B-29)
-
+#
+# R-VECTOR IN ALPHAV (METERS B-29)
 LALOTORV	STQ	SETPD		# LAT,LONG,ALT TO R VECTOR
 			INCORPEX
 			0D
 		STCALL	6D		# 6-7D= TIME FOR RP-TO-R
-			SETGAMMA	# GAMMA=B2/A2 FOR EARTH, 1 FOR MOON B-1
+			SETGAMMA	# GAMMA=B2/A2 FOR EARTH,1 FOR MOON B-1
 		DLOAD	SIN		#           	COS(LONG)COS(LAT) IN MPAC
-			LAT		#     UNIT RP =	SIN(LONG)COS(LAT)    2-3D
+			LAT		#     UNIT RP=	SIN(LONG)COS(LAT)    2-3D
 		DMPR	PDDL		# PD 2      	GAMMA*SIN(LAT)       0-1D
 			GAMRP
-			LAT		#     	 0-1D =	GAMMA*SIN(LAT) B-2
-		COS	PDDL		# PD4 	 2-3D =	COS(LAT) B-1 TEMPORARILY
+			LAT		#     	  0-1D= GAMMA*SIN(LAT) B-2
+		COS	PDDL		# PD4 	   2-3D=COS(LAT) B-1 TEMPORARILY
 			LONG
 		SIN	DMPR		# PD 2
-		PDDL	COS		# PD 4 	 2-3D =	SIN(LONG)COS(LAT) B-2
+		PDDL	COS		# PD 4 	  2-3D=SIN(LONG)COS(LAT) B-2
 			LAT
-		PDDL	COS		# PD 6 	 4-5D =	COS(LAT) B-1 TEMPORARILY
+		PDDL	COS		# PD 6 	   4-5D=COS(LAT) B-1 TEMPORARILY
 			LONG
-		DMPR	VDEF		# PD 4 	 MPAC =	COS(LONG)COS(LAT) B-2
+		DMPR	VDEF		# PD 4 	 MPAC=	COS(LONG)COS(LAT) B-2
 		UNIT	PUSH		# 0-5D= UNIT RP FOR RP-TO-R SUBR.
 		STCALL	ALPHAV		# ALPHAV +4= SINL FOR SETRE SUBR.
 			SETRE		# RE METERS B-29
-		DLOAD	BOFF		# SET MPAC=0 FOR EARTH, NON-ZERO FOR MOON
+		DLOAD	BOFF		# SET MPAC=0 FOR EARTH,NON-ZERO FOR MOON
 			ZEROVEC
 			LUNAFLAG
 			CALLRPRT
@@ -154,14 +153,15 @@ CALLRPRT	CALL
 		VSL1			# R METERS B-29
 		STCALL	ALPHAV		# EXIT WITH R IN METERS B-29
 			INCORPEX
-
 # SUBROUTINE TO COMPUTE EARTH RADIUS
 #
 # INPUT
-#	1/2 SIN LAT IN ALPHAV +4
+#
+#   1/2 SIN LAT IN ALPHAV +4
 #
 # OUTPUT
-#	EARTH RADIUS IN ERADM AND MPAC (METERS B-29)
+#
+#   EARTH RADIUS IN ERADM AND MPAC (METERS B-29)
 
 GETERAD		DLOAD	DSQ
 			ALPHAV +4	# SIN**2(L)
@@ -176,11 +176,10 @@ GETERAD		DLOAD	DSQ
 		STORE	ERADM
 		RVQ
 
-# THE FOLLOWING CONSTANTS WERE COMPUTED WITH A=6378166, B=6356784 METERS
-# B2XSC = B**2 SCALED B-51
-# B2/A2 = B**2/A**2 SCALED B-1
-# EE = (1-B**2/A**2) SCALED B-0
-
+# THE FOLLOWING CONSTANTS WERE COMPUTED WITH A=6378166,B=6356784 METERS
+# B2XSC= B**2 SCALED B-51
+# B2/A2= B**2/A**2 SCALED B-1
+# EE=(1-B**2/A**2) SCALED B-0
 B2XSC		2DEC	.0179450689	# B**2 SCALED B-51
 DP1/2		=	XUNIT
 B2/A2		2DEC	.9933064884 B-1	# GAMMA= B**2/A**2 B-1
@@ -190,12 +189,13 @@ EE		2DEC	6.6935116 E-3	# (1-B**2/A**2) B-0
 # ARCTAN SUBROUTINE
 #
 # CALLING SEQUENCE
-#	SIN THETA IN SINTH B-1
-#	COS THETA IN COSTH B-1
-#	CALL ARCTAN
+#
+#   SIN THETA IN SINTH B-1
+#   COS THETA IN COSTH B-1
+#   CALL ARCTAN
 #
 # OUTPUT
-#	ARCTAN THETA IN MPAC AND THETA B-0 IN RANGE -1/2 TO +1/2
+#   ARCTAN THETA IN MPAC AND THETA B-0 IN RANGE -1/2 TO +1/2
 
 ARCTAN		BOV
 			CLROVFLW
@@ -234,21 +234,21 @@ ATAN=90		DLOAD	SIGN
 2DZERO		=	DPZERO
 
 # Page 1138
-# ***** SETGAMMA SUBROUTINE *****
+# ..... SETGAMMA SUBROUTINE .....
 # SUBROUTINE TO SET GAMMA FOR THE LAT-LONG AND LALOTORV SUBROUTINES
 #
 # GAMMA = B**2/A**2 FOR EARTH (B-1)
 # GAMMA = 1 FOR MOON (B-1)
 #
 # CALLING SEQUENCE
-#	L	CALL
-#	L+1		SETGAMMA
+#  L	   CALL
+#  L+1		  SETGAMMA
 #
 # INPUT
-#	LUNAFLAG=0 FOR EARTH, =1 FOR MOON
+#  LUNAFLAG=0 FOR EARTH,=1 FOR MOON
 #
 # OUTPUT
-#	GAMMA IN GAMRP (B-1)
+#  GAMMA IN GAMRP  (B-1)
 
 SETGAMMA	DLOAD	BOFF		# BRANCH FOR EARTH
 			B2/A2		# EARTH GAMMA
@@ -261,27 +261,27 @@ SETGMEX		STORE	GAMRP
 GAMRP		=	8D
 
 # Page 1139
-# ***** SETRE SUBROUTINE *****
+# .....SETRE SUBROUTINE .....
 # SUBROUTINE TO SET RE (EARTH OR MOON RADIUS)
 #
-#	RE = RM FOR MOON
-#	RE = RREF FOR FIXED EARTH RADIUS OR COMPUTED RF FOR FISCHER ELLIPSOID
+# RE= RM FOR MOON
+#  RE= RREF FOR FIXED EARTH RADIUS OR COMPUTED RF FOR FISCHER ELLIPSOID
 #
 # CALLING SEQUENCE
-#	L	CALL
-#	L+1		SETRE
+#  L	   CALL
+#  L+1		  SETRE
 #
 # SUBROUTINES USED
-#	GETERAD
+#  GETERAD
 #
 # INPUT
-#	ERADFLAG = 0 FOR FIXED RE, 1 FOR COMPUTED RE
-#	ALPHAV +4 = 1/2 SINL IF GETERAD IS CALLED
-#	LUNAFLAG = 0 FOR EARTH, =1 FOR MOON
+#  ERADFLAG=0 FOR FIXED RE, 1 FOR COMPUTED RE
+#  ALPHAV +4= 1/2 SINL IF GETERAD IS CALLED
+#  LUNAFLAG=0 FOR EARTH,=1 FOR MOON
 #
 # OUTPUT
-#	ERADM = 504RM FOR MOON (METERS B-29)
-#	ERADM = ERAD OR COMPUTED RE FOR EARTH (METERS B-29)
+#  ERADM= 504RM FOR MOON (METERS B-29)
+#  ERADM= ERAD OR COMPUTED RE FOR EARTH (METERS B-29)
 
 SETRE		STQ	DLOAD
 			SETREX
@@ -290,19 +290,17 @@ SETRE		STQ	DLOAD
 			LUNAFLAG
 			TSTRLSRM
 			ERAD
-		BOFF	CALL		# ERADFLAG=0 FOR FIXED RE, 1 FOR COMPUTED
+		BOFF	CALL		# ERADFLAG=0 FOR FIXED RE,1 FOR COMPUTED
 			ERADFLAG
 			SETRXX
 			GETERAD
 SETRXX		STCALL	ERADM		# EXIT WITH RE OR RM METERS B-29
 			SETREX
-TSTRLSRM	BON	VLOAD		# ERADFLAG=0, SET R0=RLS
-			ERADFLAG	#         =1      R0=RM
+TSTRLSRM	BON	VLOAD		# ERADFLAG=0,SET R0=RLS
+			ERADFLAG	#         =1     R0=RM
 			SETRXX
 			RLS
 		ABVAL	SR2R		# SCALE FROM B-27 TO B-29
 		GOTO
 			SETRXX
 SETREX		=	S2
-
-

Luminary099/LEM_GEOMETRY.agc

@@ -35,22 +35,22 @@
 		EBANK=	XSM
 
 # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM,CSM BY ADDING
-# THE CONIC R,V AND THE DEVIATIONS R,V.  THE STATE VECTORS ARE CONVERTED TO
+# THE CONIC R,V AND THE DEVIATIONSR,V. THE STATE VECTORS ARE CONVERTED TO
 # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
-# R-OTHER,V-OTHER FOR DOWNLINK.  THE ROUTINES NAMES ARE SWITCHED IN THE
+# R-OTHER , V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
 # OTHER VEHICLES COMPUTER.
 #
 # INPUT
-#	STATE VECTOR IN TEMPORARY STORAGE AREA
-#	IF STATE VECTOR IS SCALED POS B27 AND VEL B5
-#		SET X2 TO +2
-#	IF STATE VECTOR IS SCALED POS B29 AND VEL B7
-#		SET X2 TO 0
+#   STATE VECTOR IN TEMPORARY STORAGE AREA
+#   IF STATE VECTOR IS SCALED POS B27 AND VEL B5
+#      SET X2 TO +2
+#   IF STATE VECTOR IS SCALED POS B29 AND VEL B7
+#      SET X2 TO 0
 #
 # OUTPUT
-#	R(T) IN RN, V(T) IN VN, T IN PIPTIME
+#   R(T) IN RN, V(T) IN VN, T IN PIPTIME
 # OR
-#	R(T) IN R-OTHER, V(T) IN V-OTHER	(T IS DEFINED BY T-OTHER)
+#   R(T) IN R-OTHER, V(T) IN V-OTHER   (T IS DEFINED BY T-OTHER)
 
 		COUNT*	$$/GEOM
 SVDWN2		BOF	RVQ		# SW=1=AVETOMID DOING W-MATRIX INTEG.
@@ -58,14 +58,14 @@ SVDWN2		BOF	RVQ		# SW=1=AVETOMID DOING W-MATRIX INTEG.
 			+1
 		VLOAD	VSL*
 			TDELTAV
-			0 	-7,2
+			0 -7,2
 		VAD	VSL*
 			RCV
 			0,2
 		STOVL	RN
 			TNUV
 		VSL*	VAD
-			0 	-4,2
+			0 -4,2
 			VCV
 		VSL*
 			0,2
@@ -76,14 +76,14 @@ SVDWN2		BOF	RVQ		# SW=1=AVETOMID DOING W-MATRIX INTEG.
 # Page 321
 SVDWN1		VLOAD	VSL*
 			TDELTAV
-			0 	-7,2
+			0 -7,2
 		VAD	VSL*
 			RCV
 			0,2
 		STOVL	R-OTHER
 			TNUV
 		VSL*	VAD
-			0 	-4,2
+			0 -4,2
 			VCV
 		VSL*
 			0,2
@@ -91,32 +91,32 @@ SVDWN1		VLOAD	VSL*
 		RVQ
 
 # Page 322
-# THE FOLLOWING ROUTINE TAKES A HALF UNIT TARGET VECTOR REFERRED TO NAV BASE COORDINATES AND FINDS BOTH
-# GIMBAL ORIENTATIONS AT WHICH THE RR MIGHT SIGHT THE TARGET.  THE GIMBAL ANGLES CORRESPONDING TO THE PRESENT MODE
-# ARE LEFT IN MODEA AND THOSE WHICH WOULD BE USED AFTER A REMODE IN MODEB.  THIS ROUTINE ASSUMES MODE 1 IS TRUNNION
-# ANGLE LESS THAN 90 DEGS IN ABS VALUE WITH ARBITRARY SHAFT, WITH A CORRESPONDING DEFINITION FOR MODE 2.  MODE
+#	   THE FOLLOWING ROUTINE TAKES A HALF UNIT TARGET VECTOR REFERRED TO NAV BASE COORDINATES AND FINDS BOTH
+# GIMBAL ORIENTATIONS AT WHICH THE RR MIGHT SIGHT THE TARGET. THE GIMBAL ANGLES CORRESPONDING TO THE PRESENT MODE
+# ARE LEFT IN MODEA AND THOSE WHICH WOULD BE USED AFTER A REMODE IN MODEB. THIS ROUTINE ASSUMES MODE 1 IS TRUNNION
+# ANGLE LESS THAN 90 DEGS IN ABS VALUE WITH ARBITRARY SHAFT, WITH A CORRESPONDING DEFINITION FOR MODE 2. MODE
 # SELECTION AND LIMIT CHECKING ARE DONE ELSEWHERE.
 #
-# THE MODE 1 CONFIGURATION IS CALCULATED FROM THE VECTOR AND THEN MODE 2 IS FOUND USING THE RELATIONS
+#	   THE MODE 1 CONFIGURATION IS CALCULATED FROM THE VECTOR AND THEN MODE 2 IS FOUND USING THE RELATIONS
 #
-#	S(2) = 180 + S(1)
-#	T(2) = 180 - T(1)
+#	   S(2) = 180 + S(1)
+#	   T(2) = 180 - T(1)
 #
-# THE VECTOR ARRIVES IN MPAC WHERE TRG*SMNG OR *SMNB* WILL HAVE LEFT IT.
+#     THE VECTOR ARRIVES IN MPAC WHERE TRG*SMNB OR *SMNB* WILL HAVE LEFT IT.
 
 RRANGLES	STORE	32D
 		DLOAD	DCOMP		# SINCE WE WILL FIND THE MODE 1 SHAFT
 			34D		# ANGLE LATER, WE CAN FIND THE MODE 1
 		SETPD	ASIN		# TRUNNION BY SIMPLY TAKING THE ARCSIN OF
 			0		# THE Y COMPONENT, THE ASIN GIVIN AN
-		PUSH	BDSU		# ANSWER WHOSE ABS VAL IS LESS THAN 90 DEG.
+		PUSH	BDSU		# ANSWER WHOSE ABS VAL IS LESS THAN 90 DEG
 			LODPHALF
 		STODL	4		# MODE 2 TRUNNION TO 4.
 
 			LO6ZEROS
 		STOVL	34D		# UNIT THE PROJECTION OF THE VECTOR
-			32D		#	IN THE X-Z PLANE
-		UNIT	BOVB		# IF OVERFLOW, TARGET VECTOR IS ALONG Y
+			32D		#   IN THE X-Z PLANE
+		UNIT	BOVB		# IF OVERFLOW,TARGET VECTOR IS ALONG Y
 			LUNDESCH	# CALL FOR MANEUVER UNLESS ON LUNAR SURF
 		STODL	32D		# PROJECTION VECTOR.
 			32D
@@ -154,7 +154,7 @@ RRANGLES	STORE	32D
 		GOTO
 			S2
 # Page 324
-# GIVEN RR TRUNNION AND SHAFT (T,S) IN TANGNB,+1, FIND THE ASSOCIATED
+# GIVEN RR TRUNNION AND SHAFT (T,S) IN TANGNB,+1,FIND THE ASSOCIATED
 # LINE OF SIGHT IN NAV BASE AXES.  THE HALF UNIT VECTOR, .5(SIN(S)COS(T),
 # -SIN(T),COS(S)COS(T)) IS LEFT IN MPAC AND 32D.
 
@@ -190,7 +190,7 @@ RRNB1		PUSH	COS		# SHAFT ANGLE TO 2
 
 RRNBMPAC	STODL	20D		# SAVE SHAFT CDU IN 21.
 			MPAC		# SET MODE TO DP.  (THE PRECEEDING STORE
-					# MAY BE DP, TP OR VECTOR.)
+					# MAY BE DP. TP OR VECTOR.)
 		RTB	SETPD
 			CDULOGIC
 			0
@@ -203,7 +203,4 @@ RRNBMPAC	STODL	20D		# SAVE SHAFT CDU IN 21.
 			CDULOGIC
 		GOTO
 			RRNB1
-# Page 325
-# (This page has nothing on it.)
-
-
+# Page 325 (empty page)

Luminary099/LUNAR_AND_SOLAR_EPHEMERIDES_SUBROUTINES.agc

@@ -25,104 +25,91 @@
 #	16:27 JULY 14, 1969
 
 # Page 984
-# NAME -- LSPOS -- LOCATE SUN AND MOON			DATE -- 25 OCT 67
-# MOD NO. 1
+# NAME - LSPOS  - LOCATE SUN AND MOON			DATE - 25 OCT 67
+# MOD NO.1
 # MOD BY NEVILLE					ASSEMBLY SUNDANCE
 #
 # FUNCTIONAL DESCRIPTION
 #
-# COMPUTES UNIT POSITION VECTOR OF THE SUN AND MOON IN THE BASIC REFERENCE SYSTEM.  THE SUN VECTOR S IS
-# LOCATED VIA TWO ANGLES.  THE FIRST ANGLE (OBLIQUITY) IS THE ANGLE BETWEEN THE EARTH EQUATOR AND THE ECLIPTIC.  THE
-# POSITION VECTOR OF THE SUN IS
-#	_
-#	S = (COS(LOS), COS(OBL)*SIN(LOS), SIN(OBL)*SIN(LOS)), WHERE
+#        COMPUTES UNIT POSITION VECTOR OF THE SUN AND MOON IN THE BASIC REFERENCE SYSTEM. THE SUN VECTOR S IS
+# LOCATED VIA TWO ANGLES. THE FIRST ANGLE(OBLIQUITY) IS THE ANGLE BETWEEN THE EARTH EQUATOR AND THE ECLIPTIC. THE
+# SECOND ANGLE IS THE LONGITUDE OF THE SUN MEASURED IN THE ECLIPTIC.
+# THE POSITION VECTOR OF THE SUN IS
+#	 -
+#	 S=(COS(LOS), COS(OBL)*SIN(LOS), SIN(OBL)*SIN(LOS)), WHERE
 #
-#	LOS = LOS +LOS *T-(C *SIN(2PI*T)/365.24 +C *COS(2PI*T)/365.24)
-#	         0    R     0                     1
-#	LOS  (RAD) IS THE LONGITUDE OF THE SUN FOR MIGNIGHT JUNE 30TH OF THE PARTICULAR YEAR.
-#          0
-#	LOS  (RAD/DAY) IS THE MEAN RATE FOR THE PARTICULAR YEAR.
-#    	   R
-#
-# LOS  AND LOS  ARE STORED AS LOSC AND LOSR IN RATESP.
+#      LOS=LOS +LOS *T-(C *SIN(2PI*T)/365.24 +C *COS(2PI*T)/365.24)
+#	      0    R     0                     1
+#      LOS  (RAD) IS THE LONGITUDE OF THE SUN FOR MIGNIGHT JUNE 30TH OF THE PARTICULAR YEAR.
+#         0
+#      LOS  (RAD/DAY) IS THE MEAN RATE FOR THE PARTICULAR YEAR.
+#    	  R
+# LOS  AND LOS  ARE STORED AS LOSO AND LOSR IN RATESP.
 #    0        R
 # COS(OBL) AND SIN(OBL) ARE STORED IN THE MATRIX KONMAT.
-#
-# T, TIME MEASURED IN DAYS (24 HOURS) IS STORED IN TIMEP.
-#
-# C  AND C  ARE FUDGE FACTORS TO MINIMIZE THE DEVIATION.  THEY ARE STORED AS ONE CONSTANT (CMOD), SINCE
+# T, TIME MEASURED IN DAYS(24 HOURS), IS STORED IN TIMEP.
+# C  AND C  ARE FUDGE FACTORS TO MINIMIZE THE DEVIATION. THEY ARE STORED AS ONE CONSTANT(CMOD), SINCE
 #  0      1                               2  2 1/2
 # C *SIN(X)+C *COS(X) CAN BE WRITTEN AS (C +C )   *SIN(X+PHI), WHERE PHI=ARCTAN(C /C ).
-#                                         0  1                                   1  0
+#  0         1                            0  1                                   1  0
 #
-# THE MOON IS LOCATED VIA FOUR ANGLES, THE FIRST IS THE OBLIQUITY. THE SECOND IS THE MEAN LONGITUDE OF THE MOON,
+# THE MOON IS LOCATED VIA FOUR ANGLES. THE FIRST IS THE OBLIQUITY. THE SECOND IS THE MEAN LONGITUDE OF THE MOON,
 # MEASURED IN THE ECLIPTIC FROM THE MEAN EQUINOX TO THE MEAN ASCENDING NODE OF THE LUNAR ORBIT, AND THEN ALONG THE
-# ORBIT.  THE THIRD ANGLE IS THE ANGLE BETWEEN THE ECLIPTIC AND THE LUNAR ORBIT.  THE FOURTH ANGLE IS THE LONGITUDE
-# OF THE NODE OF THE MOON, MEASURED IN THE LUNAR ORBIT.  LET THESE ANGLES BE OBL,LOM,IM, AND LON RESPECTIVELY.
+# ORBIT. THE THIRD ANGLE IS THE ANGLE BETWEEN THE ECLIPTIC AND THE LUNAR ORBIT. THE FOURTH ANGLE IS THE LONGITUDE
+# OF THE NODE OF THE MOON, MEASURED IN THE LUNAR ORBIT. LET THESE ANGLES BE OBL,LOM,IM, AND LON RESPECTIVELY.
 #
 # THE SIMPLIFIED POSITION VECTOR OF THE MOON IS
-#	_
-#	M=(COS(LOM), COS(OBL)*SIN(LOM)-SIN(OBL)*SIN(IM)*SIN(LOM-LON), SIN(OBL)*SIN(LOM)+COS(OBL)*SIN(IM)*SIN(LOM-LON))
+#   -
+#   M=(COS(LOM), COS(OBL)*SIN(LOM)-SIN(OBL)*SIN(IM)*SIN(LOM-LON), SIN(OBL)*SIN(LOM)+COS(OBL)*SIN(IM)*SIN(LOM-LON))
 #
-# WHERE
-#	LOM=LOM +LOM *T-(A *SIN(2PI*T/27.5545)+A *COS(2PI*T/27.5545)+B *SIN(2PI*T/32)+B *COS(2PI*T/32)), AND
-#	       0    R     0                     1                     0                     1
-#	LON=LON +LON
-#	       0    R
-# A , A , B  AND B  ARE STORE AS AMOD AND BMOD (SEE DESCRIPTION OF CMOD, ABOVE).  COS(OBL), SIN(OBL)*SIN(IM),
+#   WHERE
+#      LOM=LOM +LOM *T-(A *SIN(2PI*T/27.5545)+A *COS(2PI*T/27.5545)+B *SIN(2PI*T/32)+B *COS(2PI*T/32)), AND
+#	      0    R     0                     1                     0                1
+#      LON=LON +LON
+#	      0    R
+# A , A , B  AND B  ARE STORED AS AMOD AND BMOD (SEE DESCRIPTION OF CMOD, ABOVE).  COS(OBL), SIN(OBL)*SIN(IM),
 #  0   1   0      1
-# SIN(OBL), AND COS(OBL)*SIN(IM) ARE STORED IN KONMAT AS K1, K2, K3, AND K4, RESPECTIVELY.  LOM , LOM , LON , LON
-#                                                                                              0     R     0     R
-# ARE STORED AS LOM0, LOMR, LON0, AND LONR IN RATESP.
-#
+# SIN(OBL), AND COS(OBL)*SIN(IM) ARE STORED IN KONMAT AS K1, K2, K3 AND K4, RESPECTIVELY. LOM , LOM , LON , LON
+# ARE STORED AS LOMO, LOMR, LONO, AND LONR IN RATESP.                                        0     R     0     R
 # THE THREE PHIS ARE STORED AS AARG, BARG, AND CARG(SUN).  ALL CONSTANTS ARE UPDATED BY YEAR.
 #
 # CALLING SEQUENCE
 # Page 985
-#	CALL LSPOS.  RETURN IS VIA CPRET.
-#
+#   CALL LSPOS.  RETURN IS VIA QPRET.
 # ALARMS OR ABORTS
-#	NONE
-#
+#   NONE
 # ERASABLE INITIALIZATION REQUIRED
-#	TEPHEM -- TIME FROM MIGNIGHT 1 JULY PRECEDING THE LAUNCH TO THE TIME OF THE LAUNCH (WHEN THE AGC CLOCK WENT
-#	TO ZERO).  TEPHEM IS TP WITH UNITS OF CENTI-SECONDS.
-#
-#	TIME2 AND TIME1 ARE IN MPAC AND MPAC +1 WHEN PROGRAM IS CALLED.
-#
+#   TEPHEM - TIME FROM MIGNIGHT 1 JULY PRECEDING THE LAUNCH TO THE TIME OF THE LAUNCH (WHEN THE AGC CLOCK WENT
+# TO ZERO). TEPHEM IS TP WITH UNITS OF CENTI-SECONDS.
+#   TIME2 AND TIME1 ARE IN MPAC AND MPAC +1 WHEN PROGRAM IS CALLED.
 # OUTPUT
-#	UNIT POSITIONAL VECTOR OF SUN IN VSUN.  (SCALED B-1)
-#	UNIT POSITIONAL VECTOR OF MOON IN VMOON.  (SCALED B-1)
-#
+#   UNIT POSITIONAL VECTOR OF SUN IN VSUN.   (SCALED B-1)
+#   UNIT POSITIONAL VECTOR OF MOON IN VMOON. (SCALED B-1)
 # SUBROUTINES USED
-#	NONE
-#
+#   NONE
 # DEBRIS
-#	CURRENT CORE SET, WORK AREA AND FREEFLAG
-
+#   CURRENT CORE SET,WORK AREA AND FREEFLAG
 		BANK	04
 		SETLOC	EPHEM
 		BANK
-
 		EBANK=	VSUN
 		COUNT*	$$/EPHEM
 LUNPOS		EQUALS	LSPOS
-
 LSPOS		SETPD	SR
 			0
 			14D		# TP
 		TAD	DDV
-# HG comments in [...] are hand written comments in original listing
-			TEPHEM		# TIME OF LAUNCH [IN CENTISEC B 42]
-			CSTODAY		# 24 HOURS -- 8640000 CENTI-SECS/DAY B-33
-		STORE	TIMEP		# T IN DAYS [@ B 9 = 512 DAYS]
-		AXT,1	AXT,2		#	    [GRANULRITY = 0.164 SEC]
+## Comments in [...] are hand-written notations in original listing
+			TEPHEM		# TIME OF LAUNCH [in centisec B 42]
+			CSTODAY		# 24 HOURS-8640000 CENTI-SECS/DAY B-33
+		STORE	TIMEP		# T IN DAYS [@ B 9 = 512 days]
+		AXT,1	AXT,2		#	    [∴ granularity ≈ 0.164 sec]
 			0
 			0
 		CLEAR
 			FREEFLAG	# SWITCH BIT
 POSITA		DLOAD
-			KONMAT +2	# ZEROS
+			KONMAT +2	# ZERO$
 		STORE	GTMP
 POSITB		DLOAD	DMP*
 			TIMEP		# T
@@ -132,11 +119,11 @@ POSITB		DLOAD	DMP*
 			8D
 			VAL67 +2,1	# AARG
 		SIN	DMP*		# SIN(T/27+PHI) OR T/32 OR T/365
-			VAL67,1		# (A0**2+A1**2)**1/2 SIN(X+PHIA)
+			VAL67,1		# (A0**2+A1**2)**1/2SIN(X+PHIA)
 		DAD	INCR,1		# PLUS
-			GTMP		# (B0**2+B1**2)**1/2 SIN(X+PHIB)
+			GTMP		# (B0**2+B1**2)**1/2SIN(X+PHIB)
 		DEC	-6
-		STORE	GTMP		# OR (C0**2+C1**2)**1/2 SIN(X+PHIC)
+		STORE	GTMP		# OR (C0**2+C1**2)**1/2SIN(X+PHIC)
 		BOFSET
 			FREEFLAG
 			POSITB
@@ -145,7 +132,7 @@ POSITD		DLOAD	DMP*
 			RATESP,2	# LOMR,LOSR,LONR
 		SL	DAD*
 			5D
-			RATESP +6,2	# LOM0,LOS0,LON0
+			RATESP +6,2	# LOMO,LOSO,LONO
 		DSU
 			GTMP
 		STORE	STMP,2		# LOM,LOS,LON
@@ -184,7 +171,7 @@ POSITE		DLOAD
 		STORE	GTMP
 		GOTO
 			POSITD
-LUNVEL		RVQ
+LUNVEL		RVQ                     #         TO FOOL INTEGRATION
 		SETLOC	EPHEM1
 		BANK
 

Luminary099/P20-P25.agc

@@ -1100,7 +1100,7 @@ OUTOFLIM	RELINT
 		CAF	OCT501PV
 		TC	BANKCALL	# ISSUE ALARM -- RR ANTENNA NOT WITHIN
 		CADR	PRIOLARM	# LIMITS
-		TC	R23LEM2		# TERMINATE -- EXIT R23 TO R00 (GO TO P00H)
+		TC	R23LEM2		# TERMINATE -- EXIT R23 TO R00 (GO TO POOH)
 		TC	OUTOFLIM +1	# PROCEED ILLEGAL
 		TC	R23LEM3		# RECYCLE -- TO ANOTHER MANEUVER
 		TC	ENDOFJOB

Luminary099/P30_P37.agc

@@ -32,9 +32,8 @@
 # PROGRAM DESCRIPTION P30	DATE 3-6-67
 #
 # MOD.1 BY RAMA AIYAWAR
-#
-# FUNCTIONAL DESCRIPTIONS
-#	ACCEPT ASTRONAUT INPUTS OF TIG,DELV(LV)
+# FUNCTIONAL DESCRIPTION
+#	ACCEPT ASTRONAUT INPUTS OF TIG.DELV(LV)
 #	CALL IMU STATUS CHECK ROUTINE (R02)
 #	DISPLAY TIME TO GO, APOGEE, PERIGEE, DELV(MAG), MGA AT IGN
 #	REQUEST BURN PROGRAM
@@ -43,16 +42,16 @@
 #
 # EXIT VIA V37 CALL OR TO GOTOPOOH (V34E)
 #
-# SUBROUTINE CALLS --	FLAGUP, PHASCHNG, BANKCALL, ENDOFJOB, GOFLASH, GOFLASHR
-#			GOPERF3R, INTPRET, BLANKET, GOTOPOOH, R02BOTH, S30.1,
-#			TIG/N35, MIDGIM, DISPMGA
+# SUBROUTINE CALLS-FLAGUP, PHASCHNG, BANKCALL, ENDOFJOB, GOFLASH, GOFLASHR
+#		   GOPERF3R, INTPRET, BLANKET, GOTOPOOH, R02BOTH, S30.1,
+#		   TIG/N35, MIDGIM, DISPMGA
 #
-# ERASABLE INITIALIZATION -- STATE VECTOR
+# ERASABLE INITIALIZATION- STATE VECTOR
 #
-# OUTPUT -- 	RINIT, VINIT, +MGA, VTIG, RTIG, DELVSIN, DELVSAB, DELVSLV, HAPO,
-#	    	HPER, TTOGO
+# OUTPUT-RINIT, VINIT, +MGA, VTIG, RTIG, DELVSIN, DELVSAB, DELVSLV, HAPO,
+#	 HPER, TTOGO
 #
-# DEBRIS -- A, L, MPAC, PUSHLIST
+# DEBRIS- A,L, MPAC, PUSHLIST
 
 		BANK	32
 		SETLOC	P30S
@@ -65,10 +64,10 @@ P30		TC	UPFLAG		# SET UPDATE FLAG
 		ADRES	TRACKFLG
 
 P30N33		CAF	V06N33		# T OF IGN
-		TC	VNP00H		# RETURN ON PROCEED, P00H ON TERMINATE
+		TC	VNPOOH		# RETURNS ON PROCEED, POOH ON TERMINATE
 
 		CAF	V06N81		# DISPLAY DELTA V (LV)
-		TC	VNP00H		#	REDISPLAY ON RECYCLE
+		TC	VNPOOH		#     REDISPLAY ON RECYCLE
 
 		TC	DOWNFLAG	# RESET UPDATE FLAG
 		ADRES	UPDATFLG
@@ -77,8 +76,8 @@ P30N33		CAF	V06N33		# T OF IGN
 			S30.1
 		SET	EXIT
 			UPDATFLG
-PARAM30		CAF	V06N42		# DISPLAY APOGEE,PERIGEE,DELTA V
-		TC	VNP00H
+PARAM30		CAF	V06N42		# DISPLAY APOGEE,PERIGEE ,DELTA V
+		TC	VNPOOH
 # Page 615
 
 		TC	INTPRET
@@ -93,46 +92,40 @@ V06N42		VN	0642
 # PROGRAM DESCRIPTION S30.1	DATE 9NOV66
 # MOD NO 1			LOG SECTION P30,P37
 # MOD BY RAMA AIYAWAR **
-#
 # FUNCTIONAL DESCRIPTION
-#	BASED ON STORED TARGET PARAMETERS (R OF IGNITION (RTIG), V OF
-#	IGNITION (VTIG), TIME OF IGNITION (TIG)), COMPUTE PERIGEE ALTITUDE
-#	APOGEE ALTITUDE AND DELTAV REQUIRED (DELVSIN).
-#
+#	BASED ON STORED TARGET PARAMETERS(R OF IGNITION(RTIG),V OF
+#	IGNITION(VTIG),TIME OF IGNITION (TIG)),COMPUTE PERIGEE ALTITUDE
+#	APOGEE ALTITUDE AND DELTAV REQUIRED(DELVSIN).
 # CALLING SEQUENCE
 #	L	CALL
 #	L+1		s30.1
-#
 # NORMAL EXIT MODE
 #	AT L+2 OR CALLING SEQUENCE (GOTO L+2)
-#
 # SUBROUTINES CALLED
 #	LEMPREC
 #	PERIAPO
-#
 # ALARM OR ABORT EXIT MODES
 #	NONE
-#
 # ERASABLE INITIALIZATION REQUIRED
 #	TIG		TIME OF IGNITION	DP B28CS
 #	DELVSLV		SPECIFIED DELTA-V IN LOCAL VERT.
 #			COORDS. OF ACTIVE VEHICLE AT
-#			TIME OF IGNITION	VECTOR B+7 METERS/CS
+#			TIME OF IGNITION	VECTOR 	B+7 METERS/CS
 #
 # OUTPUT
-#	RTIG		POSITION AT TIG		VECTOR B+29 METERS
-#	VTIG		VELOCITY AT TIG		VECTOR B+29 METERS/CS
-#	PDL 4D		APOGEE ALTITUDE		DP B+29 M, B+27 METERS.
-#	HAPO		APOGEE ALTITUDE		DP B+29 METERS
-#	PDL 8D		PERIGEE ALTITUDE	DP B+29 M, B+27 METERS.
-#	HPER		PERIGEE ALTITUDE	DP B+29 METERS
+#	RTIG		POSITION AT TIG		VECTOR 	B+29 METERS
+#	VTIG		VELOCITY AT TIG		VECTOR 	B+29 METERS/CS
+#	PDL 4D		APOGEE ALTITUDE		DP 	B+29 M ,  B+27 METERS.
+#	HAPO		APOGEE ALTITUDE		DP 	B+29 METERS
+#	PDL 8D		PERIGEE ALTITUDE	DP 	B+29 M ,  B+27 METERS.
+#	HPER		PERIGEE ALTITUDE	DP 	B+29 METERS
 #	DELVSIN		SPECIFIED DELTA-V IN INTERTIAL
 #			COORD. OF ACTIVE VEHICLE AT
-#			TIME OF IGNITION	VECTOR B+7 METERS/CS
-#	DELVSAB		MAG. OF DELVSIN		VECTOR B+7 METERS/CS
+#			TIME OF IGNITION	VECTOR 	B+7 METERS/CS
+#	DELVSAB		MAG. OF DELVSIN		VECTOR 	B+7 METERS/CS
 #
-# DEBRIS	QTEMP	TEMP.ERASABLE
-#		QPRET, MPAC
+# DEBRIS	QTEMP	TEMP. ERASABLE
+#		QPRET,MPAC
 #		PUSHLIST
 
 		SETLOC	P30S1
@@ -160,7 +153,7 @@ S30.1		STQ	DLOAD
 		SETPD	SXA,1
 			0
 			RTX1
-		PUSH	VXV		# YRF/LV PDL 0 SCALED AT 2
+		PUSH	VXV		# YRF/LV PDL 0  SCALED AT 2
 			DELVSIN
 		VSL1	PDVL
 		PDVL	PDVL		# YRF/LV PDL 6 SCALED AT 2
@@ -181,13 +174,12 @@ S30.1		STQ	DLOAD
 			SHIFTR1		# RESCALE IF NEEDED
 		CALL			# LIMIT DISPLAY TO 9999.9 N. MI.
 			MAXCHK
-		STODL	HPER		# PERIGEE ALT 2(29) METERS FOR DISPLAY
+		STODL	HPER		# PERIGEE ALT 2(29) METERS, FOR DISPLAY
 			4D
 		CALL
 			SHIFTR1		# RESCALE IF NEEDED
 		CALL			# LIMIT DISPLAY TO 9999.9 N. MI.
 			MAXCHK
-		STCALL	HAPO		# APOGEE ALT 2(29) METERS FOR DISPLAY
+		STCALL	HAPO		# APOGEE  ALT 2(29) METERS, FOR DISPLAY
 			QTEMP
 
-

Luminary099/P32-P35_P72-P75.agc

@@ -182,7 +182,7 @@
 #	GOFLASH
 #	GOTOPOOH
 # Page 621
-#	VNP00H
+#	VNPOOH
 #	GOFLASHR
 #	BLANKET
 #	ENDOFJOB
@@ -226,7 +226,7 @@ P32/P72A	TC	P20FLGON
 		TS	TCSI
 		TS	TCSI 	+1
 VN0611		CAF	V06N11		# TCSI
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		DLOAD	DCOMP
 			TCSI
@@ -261,7 +261,7 @@ VN0655		EXIT
 		TC	+2
 		TC	-5
 		CAF	V06N37		# TTPI
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		DLOAD
 			TCSI
@@ -303,7 +303,7 @@ P32/P72F	STORE	T2TOT3
 			P32/P72F
 		EXIT
 		CAF	V06N75
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		VLOAD	CALL
 			DELVEET1
@@ -462,7 +462,7 @@ P32/P72F	STORE	T2TOT3
 #	AVFLAGA
 #	AVFLAGP
 #	P20FLGON
-#	VNP00H
+#	VNPOOH
 #	SELECTMU
 #	ADVANCE
 #	CDHMVR
@@ -484,7 +484,7 @@ P33		TC	AVFLAGA
 P73		TC	AVFLAGP
 P33/P73A	TC	P20FLGON
 		CAF	V06N13		# TCDH
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		DLOAD
 			TTPIO
@@ -560,7 +560,7 @@ P33/P73F	ABS	DSU
 		STORE	T2TOT3
 		EXIT
 		CAF	V06N75
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		VLOAD	CALL
 			DELVEET2
@@ -602,7 +602,7 @@ P20FLGON	EXTEND
 # SUBROUTINES USED
 #
 #	S32/33.X
-#	VNP00H
+#	VNPOOH
 
 DISDVLVC	STORE	DELVLVC
 		STQ	CALL
@@ -616,7 +616,7 @@ DISDVLVC	STORE	DELVLVC
 		STORE	DELVLVC
 		EXIT
 		CA	VERBNOUN
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		GOTO
 			NORMEX

Luminary099/P34-35_P74-75.agc

@@ -184,7 +184,7 @@
 #	AVFLAGA
 # Page 661
 #	AVFLAGP
-#	VNP00H
+#	VNPOOH
 #	DISPLAYE
 #	SELECTMU
 #	PRECSET
@@ -209,7 +209,7 @@ P34		TC	AVFLAGA
 P74		TC	AVFLAGP
 P34/P74A	TC	P20FLGON	# SET UPDATFLG, TRACKFLG
 		CAF	V06N37		# TTPI
-		TC	VNP00H
+		TC	VNPOOH
 		EXTEND
 		DCA	130DEG
 		DXCH	CENTANG
@@ -265,7 +265,7 @@ SWCHCLR		BONCLR	BON
 		TC	P34/P74E
 P34/P74D	EXIT
 		CAF	V06N37		# TTPI
-		TC	VNP00H
+		TC	VNPOOH
 P34/P74E	TC	INTPRET
 		SETPD	DLOAD
 			0D
@@ -312,7 +312,7 @@ P34/P74E	TC	INTPRET
 		STORE	TIG
 		EXIT
 		CAF	V06N58
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		CALL
 			S34/35.5
@@ -856,7 +856,7 @@ ALLSET		STOVL	TET
 #	GOTOPOOH
 #	S34/35.3
 #	S34.35.4
-#	VNP00H
+#	VNPOOH
 
 S34/35.5	STQ	BON
 			SUBEXIT
@@ -909,7 +909,7 @@ FLAGOFF		CALL
 			S34/35.4
 		EXIT
 		CAF	V06N59
-		TC	VNP00H
+		TC	VNPOOH
 		TC	INTPRET
 		GOTO
 			SUBEXIT
@@ -1012,14 +1012,14 @@ P3XORP7X	CAF	HIGH9
 		INCR	Q
 		RETURN
 
-# ***** VNP00H *****
+# ***** VNPOOH *****
 #
 # SUBROUTINES USED
 #	BANKCALL
 #	GOFLASH
 #	GOTOPOOH
 
-VNP00H		EXTEND
+VNPOOH		EXTEND
 		QXCH	RTRN
 		TS	VERBNOUN
 		CA	VERBNOUN

Luminary099/P70-P71.agc

@@ -52,7 +52,7 @@ R10,R11A	CS	IMODES33	# IF LAMP TEST, DO NOT CHANGE LR LITES.
 		EXTEND
 		BZF	10,11
 
-FLASHH?		MASK	FLGWRD11	# C(A) = 1 - HFLASH BIT
+FLASHH?		MASK	FLGWRD11	# C(A) = 1 = HFLASH BIT
 		EXTEND
 		BZF	FLASHV?		# H FLASH OFF, SO LEAVE ALONE
 
@@ -72,7 +72,7 @@ FLASHV?		CA	VFLSHBIT	# VLASHBIT MUST BE BIT 2.
 10,11		CA	FLAGWRD9	# IS THE LETABORT FLAG SET ?
 		MASK	LETABBIT
 		EXTEND
-		BZF	LANDISP		# NO. PROCEED TO R10.
+		BZF	LANDISP		# NO.  PROCEED TO R10.
 
 P71NOW?		CS	MODREG		# YES.  ARE WE IN P71 NOW?
 # Page 830
@@ -80,7 +80,7 @@ P71NOW?		CS	MODREG		# YES.  ARE WE IN P71 NOW?
 		EXTEND
 		BZF	LANDISP		# YES.  PROCEED TO R10.
 
-		EXTEND			# NO. IS AN ABORT STAGE COMMANDED?
+		EXTEND			# NO.  IS AN ABORT STAGE COMMANDED?
 		READ	CHAN30
 		COM
 		TS	L
@@ -88,7 +88,7 @@ P71NOW?		CS	MODREG		# YES.  ARE WE IN P71 NOW?
 		CCS	A
 		TCF	P71A		# YES.
 
-P70NOW?		CS	MODREG		# NO. ARE WE IN P70 NOW?
+P70NOW?		CS	MODREG		# NO.  ARE WE IN P70 NOW?
 		AD	1DEC70
 		EXTEND
 		BZF	LANDISP		# YES.  PROCEED TO R10.
@@ -146,7 +146,7 @@ ABRTJASK	CAF	OCTAL27
 		MASK	APSFLBIT
 		ADS	FLGWRD10
 		CS	DAPBITS		# DAPBITS = OCT 640 = BITS 6, 8, 9
-		MASK	DAPBOOLS	# (TURN OFF ULLAGE, DRIFT, AND XOVINHIB
+		MASK	DAPBOOLS	# (TURN OFF: ULLAGE, DRIFT, AND XOVINHIB )
 		TS	DAPBOOLS
 
 		CS	FLAGWRD5	# SET ENGONFLG.
@@ -167,6 +167,7 @@ ABRTJASK	CAF	OCTAL27
 		MASK	R10FLBIT	# CROSS-POINTER DISPLAY.
 		ADS	FLAGWRD0	# THE FOLLOWING ENEMA WILL REMOVE THE
 					# DISPLAY INERTIAL DATA OUTBIT.
+
 		TC	CLRADMOD	# INSURE RADMODES PROPERLY SET FOR R29.
 
 		EXTEND			# LOAD TEVENT FOR THE DOWNLINK.
@@ -195,7 +196,6 @@ ABRTJASK	CAF	OCTAL27
 		COM
 		DXCH	-PHASE4
 
-# the 3 in OCT37774 could be something else, garbled
 		CAF	OCT37774	# SET T5RUPT TO CALL DAPIDLER IN
 		TS	TIME5		# 40 MILLISECONDS.
 
@@ -272,20 +272,20 @@ P70INIT		TC	INTPRET
 		SET	CALL
 			FLAP
 			COMMINIT
-		AXC,1	GOTO		# RETURN HERE IN P70, SET X1 FOR DPS COEFF.
+		AXC,1	GOTO		# RETURN HERE IN P70, SE X1 FOR DPS COEFF.
 			0D
 			BOTHPOLY
-INJTARG		AXC,1			# RETURN HERE IN P71, SET X1 FOR APS COEFF.
+INJTARG		AXC,1			# RETURN HERE IN P71, SET X1 FOR APS COEFF
 			8D
 BOTHPOLY	DLOAD*	DMP		# TGO D
 			ABTCOF,1
 			TGO
 # Page 834
 		DAD*	DMP
-			ABTCOF +2,1	#	TGO(C+TGO )
+			ABTCOF +2,1	# TGO(C+TGO D)
 			TGO
 		DAD*	DMP
-			ABTCOF +4,1	# TGO(B+TGO d))
+			ABTCOF +4,1	# TGO(B+TGO(C+TGO D))
 			TGO
 		DAD*
 			ABTCOF +6,1	# A+TGO(B+TGO(C+TGO D))
@@ -295,7 +295,7 @@ BOTHPOLY	DLOAD*	DMP		# TGO D
 			UPRATE		# IF BIG ENOUGH, LEAVE ZDOTD AS IS .
 		DLOAD
 			VMIN
-		STORE	ZDOTD		# IF TOO SMALL, REPLCAE WITH MINIMUM.
+		STORE	ZDOTD		# IF TOO SMALL, REPLACE WITH MINIMUM.
 UPRATE		DLOAD
 			ABTRDOT
 		STCALL	RDOTD		# INITIALZE RDOTD.
@@ -303,7 +303,7 @@ UPRATE		DLOAD
 		ABS	DSU
 			YLIM		# /Y/-DYMAX
 		BMN	SIGN		# IF <0, XR<.5DEG, LEAVE YCO AT 0
-			YOK		# IF >0, FIX SIGN OF DEFICIT.  THIS IS YCO.
+			YOK		# IF >0, FIX SIGN OF DEFICIT, THIS IS YCO.
 			Y
 		STORE	YCO
 YOK		DLOAD	DSU
@@ -323,7 +323,7 @@ UPTHROT		SET	EXIT
 		TC	PHASCHNG
 		OCT	04024
 
--3		TC	BANKCALL	# VERIFY THAT THE PANEL SWITCHES
+ -3		TC	BANKCALL	# VERIFY THAT THE PANEL SWITCHES
 		CADR	P40AUTO		# ARE PROPERLY SET.
 
 		TC	THROTUP
@@ -371,6 +371,7 @@ TGO1		=	VGBODY
 		BANK	21
 		SETLOC	R11
 		BANK
+
 		COUNT*	$$/P70
 
 LEGAL?		CS	MMNUMBER	# IS THE DESIRED PGM ALREADY IN PROGRESS?
@@ -387,7 +388,7 @@ LEGAL?		CS	MMNUMBER	# IS THE DESIRED PGM ALREADY IN PROGRESS?
 		CA	FLAGWRD7	# IS SERVICER ON THE AIR?
 		MASK	AVEGFBIT
 		CCS	A
-		TC	Q		# YES. ALL IS WELL.
+		TC	Q		# YES.  ALL IS WELL.
 ABORTALM	TC	FALTON
 		TC	RELDSP
 		TC	POSTJUMP
@@ -399,7 +400,7 @@ ABORTALM	TC	FALTON
 
 		COUNT*	$$/P70
 
-# **********************************************************************
+# ************************************************************************
 
 TGOCOMP		RTB	DSU
 			LOADTIME
@@ -421,14 +422,18 @@ THROTUP		CAF	BIT13
 # ************************************************************************
 
 10SECS		2DEC	1000
+
 HINJECT		2DEC	18288 B-24	# 60,000 FEET EXPRESSED IN METERS.
+
 (TGO)A		2DEC	37000 B-17
+
 K(AT)		2DEC	.02		# SCALING CONSTANT
+
 WHICHADR	REMADR	ABRTABLE
 
 # ************************************************************************
 # Page 837
 		EBANK=	DVCNTR
 ATMAGAD		2CADR	ATMAG
-ORBMANAD	ADRES	ORBMANUV
 
+ORBMANAD	ADRES	ORBMANUV

Luminary099/PLANETARY_INERTIAL_ORIENTATION.agc

@@ -25,32 +25,31 @@
 #    16:27 JULY 14, 1969
 
 # Page 1140
-# ***** RP-TO-R SUBROUTINE *****
-# SUBROUTINE TO CONVERT RP (VECTOR IN PLANETARY COORDINATE SYSTEM, EITHER
-# EARTH-FIXED OR MOON-FIXED) TO R (SAME VECTOR IN THE BASIC REF. SYSTEM)
+# ..... RP-TO-R SUBROUTINE .....
+# SUBROUTINE TO CONVERT RP (VECTOR IN PLANETARY COORDINATE SYSTEM,EITHER
+#  EARTH-FIXED OR MOON-FIXED) TO R (SAME VECTOR IN THE BASIC REF. SYSTEM)
 #
-#	R = MT(T) * (RP + LP X RP)	MT = M MATRIX TRANSPOSE
+#  R=MT(T)*(RP+LPXRP)	 MT= M MATRIX TRANSPOSE
 #
 # CALLING SEQUENCE
-#	L 	CALL
-#	L+1		RP-TO-R
+#  L	   CALL
+#  L+1		  RP-TO-R
 #
 # SUBROUTINES USED
-#	EARTHMX, MOONMX, EARTHL
-#
-# 	ITEMS AVAILABLE FROM LAUNCH DATA
-#		504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
-#			IN THE MOON-FIXED COORD. SYSTEM		RADIANS B0
+#  EARTHMX,MOONMX,EARTHL
 #
+#    ITEMS AVAILABLE FROM LAUNCH DATA
+#     504LM= THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL,EXPRESSED
+#     IN THE MOON-FIXED COORD. SYSTEM	RADIANS	 B0
 #	ITEMS NECESSARY FOR SUBR. USED (SEE DESCRIPTION OF SUBR.)
 #
 # INPUT
-#	MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
-#	0-5D = RP VECTOR
-#	6-7D = TIME
+#  MPAC= 0 FOR EARTH,NON-ZERO FOR MOON
+#  0-5D= RP VECTOR
+#  6-7D= TIME
 #
 # OUTPUT
-#	MPAC = R VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
+#  MPAC= R VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
 
 		SETLOC	PLANTIN1
 		BANK
@@ -84,32 +83,31 @@ RPTORA		CALL			# EARTH COMPUTATIONS
 		COUNT*	$$/LUROT
 
 # Page 1142
-# ***** R-TO-RP SUBROUTINE *****
+# ..... R-TO-RP SUBROUTINE .....
 # SUBROUTINE TO CONVERT R (VECTOR IN REFERENCE COORD. SYSTEM) TO RP
-# (VECTOR IN PLANETARY COORD SYSTEM) EITHER EARTH-FIXED OR MOON-FIXED
+#  (VECTOR IN PLANETARY COORD SYSTEM) EITHER EARTH-FIXED OR MOON-FIXED
 #
-#	RP = M(T) * (R - L X R)
+#  RP=M(T)*(R-LXR)
 #
 # CALLING SEQUENCE
-#	L	CALL
-#	L+1		R-TO-RP
+#  L	   CALL
+#  L+1		  R-TO-RP
 #
 # SUBROUTINES USED
-#	EARTHMX, MOONMX, EARTHL
+#  EARTHMX,MOONMX,EARTHL
 #
 # INPUT
-#	MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
-#	0-5D = R VECTOR
-#	6-7D = TIME
-#
-#	ITEMS AVAILABLE FROM LAUNCH DATA
-#		504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
-#			IN THE MOON-FIXED COORD. SYSTEM	  RADIANS B0
+#  MPAC= 0 FOR EARTH, NON-ZERO FOR MOON
+#  0-5D= R VECTOR
+#  6-7D= TIME
 #
+#    ITEMS AVAILABLE FROM LAUNCH DATA
+#     504LM= THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL,EXPRESSED
+#     IN THE MOON-FIXED COORD. SYSTEM	RADIANS B0
 #	ITEMS NECESSARY FOR SUBROUTINES USED (SEE DESCRIPTION OF SUBR.)
 #
 # OUTPUT
-#	MPAC = RP VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
+#  MPAC=RP VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
 
 R-TO-RP		STQ	BHIZ
 			RPREXIT
@@ -119,11 +117,11 @@ R-TO-RP		STQ	BHIZ
 		VLOAD	VXM
 			504LM		# LP=LM
 			MMATRIX
-		VSL1			# L = MT(T)*LP 		RADIANS B0
+		VSL1			#  L=MT(T)*LP  RADIANS B0
 RTORPB		VXV	BVSU
 			504RPR
 			504RPR
-		MXV			# M(T)*(R-LXR)		B-2
+		MXV			# M(T)*(R-LXR) B-2
 			MMATRIX
 RPRPXXXX	VSL1	SETPD
 			0D
@@ -133,74 +131,73 @@ RTORPA		CALL			# EARTH COMPUTATIONS
 			EARTHMX
 		CALL
 			EARTHL
-		GOTO			# MPAC=L=(-AX,-AY,0) 	RAD B-0
+		GOTO			# MPAC=L=(-AX,-AY,0) RAD B-0
 			RTORPB
 
 # Page 1143
-# ***** MOONMX SUBROUTINE *****
+# ..... MOONMX SUBROUTINE .....
 # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE MOON
 #
 # CALLING SEQUENCE
-#	L	CALL
-#	L+1		MOONMX
+#  L	   CALL
+#  L+1		  MOONMX
 #
 # SUBROUTINES USED
-#	NEWANGLE
+#  NEWANGLE
 #
 # INPUT
-#	6-7D = TIME
-#
-#	ITEMS AVAILABLE FROM LAUNCH DATA
-#		BSUBO, BDOT
-#		TIMSUBO, NODIO, NODDOT, FSUBO, FDOT
-#		COSI = COS(I)	B-1
-#		SINI = SIN(I)	B-1
-#		  I IS THE ANGLE BETWEEN THE MEAN LUNAR EQUATORIAL PLANE AND THE
-#		  PLANE OF THE ECLIPTIC (1 DEGREE 32.1 MINUTES)
+#  6-7D= TIME
+#    ITEMS AVAILABLE FROM LAUNCH DATA
+#     BSUBO,BDOT
+#     TIMSUBO,NODIO,NODDOT,FSUBO,FDOT
+#     COSI= COS(I) B-1
+#     SINI= SIN(I) B-1
+#	I  IS THE ANGLE BETWEEN THE MEAN LUNAR EQUATORIAL PLANE AND THE
+#	PLANE OF THE ECLIPTIC  (1 DEGREE  32.1 MINUTES)
 #
 # OUTPUT
-#	MMATRIX = 3X3 M MATRIX B-1	(STORED IN VAC AREA)
+#  MMATRIX= 3X3 M MATRIX B-1   (STORED IN VAC AREA)
 
 MOONMX		STQ	SETPD
 			EARTHMXX
 			8D
 		AXT,1			# B REQUIRES SL 0, SL 5 IN NEWANGLE
 			5
-		DLOAD	PDDL		# PD 10D	8-9D=BSUBO
-			BSUBO		#		10-11D=BDOT
+		DLOAD	PDDL		# PD 10D	    8-9D=BSUBO
+			BSUBO		#		    10-11D= BDOT
 			BDOT
 		PUSH	CALL		# PD 12D
-			NEWANGLE	# EXIT WITH PD 8D AND MPAC= B	REVS B0
+			NEWANGLE	# EXIT WITH PD 8D AND MPAC= B  REVS B0
 		PUSH	COS		# PD 10D
-		STODL	COB		# PD 8D		COS(B) B-1
-		SIN			#		SIN(B) B-1
-		STODL	SOB		# SETUP INPUT FOR NEWANGLE
-			FSUBO		# 			8-9D=FSUBO
-		PDDL	PUSH		# PD 10D THEN 12D	10-11D=FDOT
+		STODL	COB		# PD 8D	   COS(B) B-1
+		SIN			#	   SIN(B) B-1
+		STODL	SOB		#           SETUP INPUT FOR NEWANGLE
+			FSUBO		# 		      8-9D=FSUBO
+		PDDL	PUSH		# PD 10D THEN 12D   10-11D=FDOT
 			FDOT
-		AXT,1	CALL		# F REQUIRES SL 1, SL 6 IN NEWANGLE.
+		AXT,1	CALL		# F REQUIRES SL 1, SL 6 IN NEWANGLE
 			4
 			NEWANGLE	# EXIT WITH PD 8D AND MPAC= F REVS B0
 		STODL	AVECTR +2	# SAVE F TEMP
 			NODIO		#			8-9D=NODIO
-		PDDL	PUSH		# PD 10D THEN 12D	10-11D=NODDOT
+		PDDL	PUSH		# PD 10D THEN 12D     10-11D=NODDOT
 			NODDOT		#			MPAC=T
 		AXT,1	CALL		# NODE REQUIRES SL 0, SL 5 IN NEWANGLE
 			5
 			NEWANGLE	# EXIT WITH PD 8D AND MPAC= NODI REVS B0
 # Page 1144
-		PUSH	COS		# PD 10D	8-9D= NODI REVS B0
-		PUSH			# PD 12D	10-11D= COS(NODI) B-1
+		PUSH	COS		# PD 10D   8-9D= NODI  REVS  B0
+		PUSH			# PD 12D 10-11D= COS(NODI)  B-1
 		STORE	AVECTR
 		DMP	SL1R
-			COB		#			 COS(NODI) B-1
-		STODL	BVECTR +2	# PD 10D  20-25D=AVECTR= COB*SIN(NODI)
-		DMP	SL1R		#			 SOB*SIN(NODI)
+			COB		#			  COS(NODI)    B-1
+		STODL	BVECTR +2	# PD 10D   20-25D=AVECTR= COB*SIN(NODI)
+		DMP	SL1R		#			  SOB*SIN(NODI)
 			SOB
 		STODL	BVECTR +4	# PD 8D
-		SIN	PUSH		# PD 10D		-SIN(NODI) B-1
-		DCOMP			#         26-31D=BVECTR= COB*COS(NODI)
-		STODL	BVECTR		# PD 8D			 SOB*COS(NODI)
+		SIN	PUSH		# PD 10D		 -SIN(NODI)   B-1
+		DCOMP			#          26-31D=BVECTR= COB*COS(NODI)
+		STODL	BVECTR		# PD 8D			  SOB*COS(NODI)
 			AVECTR +2	# MOVE F FROM TEMP LOC. TO 504F
 		STODL	504F
 		DMP	SL1R
@@ -214,30 +211,30 @@ MOONMX		STQ	SETPD
 		COUNT*	$$/LUROT
 
 MOONMXA		STODL	AVECTR +2
-			SINNODI		# 8-9D=SIN(NODI) B-1
+			SINNODI		# 8-9D=SIN(NODI)  B-1
 		DMP	SL1R
 			SOB
-		STODL	AVECTR +4	#			 0
-			HI6ZEROS	#	8-13D= CVECTR= -SOB  B-1
-		PDDL	DCOMP		# PD 10D		COB
+		STODL	AVECTR +4	#			   0
+			HI6ZEROS	#	  8-13D= CVECTR= -SOB  B-1
+		PDDL	DCOMP		# PD 10D		  COB
 			SOB
 		PDDL	PDVL		# PD 12D THEN PD 14D
 			COB
 			BVECTR
-		VXSC	PDVL		# PD 20D	BVECTR*SINI  B-2
+		VXSC	PDVL		# PD 20D	 BVECTR*SINI  B-2
 			SINI
 			CVECTR
-		VXSC	VAD		# PD 14D	CVECTR*COSI  B-2
+		VXSC	VAD		# PD 14D	 CVECTR*COSI  B-2
 			COSI
 		VSL1
 		STOVL	MMATRIX +12D	# PD 8D  M2=BVECTR*SINI+CVECTR*COSI  B-1
 		VXSC	PDVL		# PD 14D
-			SINI		#		CVECTR*SINI  B-2
+			SINI		#		 CVECTR*SINI  B-2
 			BVECTR
-		VXSC	VSU		# PD 8D		BVECTR*COSI  B-2
+		VXSC	VSU		# PD 8D		 BVECTR*COSI  B-2
 			COSI
 		VSL1	PDDL		# PD 14D
-			504F		# 8-13D=DVECTR=BVECTR*COSI-CVECTR*SINI  B-1
+			504F		# 8-13D=DVECTR=BVECTR*COSI-CVECTR*SINI B-1
 		COS	VXSC
 # Page 1145
 			DVECTR
@@ -256,13 +253,12 @@ MOONMXA		STODL	AVECTR +2
 		VSL1	VCOMP
 		STCALL	MMATRIX		# M0= -(AVECTR*COSF+DVECTR*SINF)  B-1
 			EARTHMXX
-
 # COMPUTE X=X0+(XDOT)(T+T0)
-# 8-9D= X0 (REVS B-0), PUSHLOC SET AT 12D
+# 8-9D= X0 (REVS B-0),PUSHLOC SET AT 12D
 # 10-11D=XDOT (REVS/CSEC) SCALED B+23 FOR WEARTH,B+28 FOR NODDOT AND BDOT
-#			AND B+27 FOR FDOT
-# X1=DIFFERENCE IN 23 AND SCALING OF XDOT, =0 FOR WEARTH, 5 FOR NDDOT AND
-#					BDOT AND 4 FOR FDOT
+#			  AND B+27 FOR FDOT
+#  X1=DIFFERENCE IN 23 AND SCALING OF XDOT,=0 FOR WEARTH,5 FOR NODDOT AND
+#					   BDOT AND 4 FOR FDOT
 # 6-7D=T (CSEC B-28), TIMSUBO= (CSEC B-42 TRIPLE PREC.)
 
 NEWANGLE	DLOAD	SR		# ENTER PD 12D
@@ -273,58 +269,58 @@ NEWANGLE	DLOAD	SR		# ENTER PD 12D
 			MPAC
 		STODL	TIMSUBM		# T+T0 CSEC B-42
 			TIMSUBM +1
-		DMP			# PD 10D	MULT BY XDOT IN 10-11D
-		SL*	DAD		# PD 8D		ADD X0 IN 8-9D AFTER SHIFTING
-			5,1		#		SUCH THAT SCALING IS B-0
-		PUSH	SLOAD		# PD 10D  SAVE PARTIAL (X0+XDOT*T) IN 8-9D
+		DMP			# PD 10D  MULT BY XDOT IN 10-11D
+		SL*	DAD		# PD 8D	  ADD X0 IN 8-9D AFTER SHIFTING
+			5,1		#	  SUCH THAT SCALING IS B-0
+		PUSH	SLOAD		# PD 10D SAVE PARTIAL (X0+XDOT*T) IN 8-9D
 			TIMSUBM
 		SL	DMP
 			9D
 			10D		# XDOT
-		SL*	DAD		# PD 8D		SHIFT SUCH THAT THIS PART OF X
-			10D,1		#		IS SCALED REVS/CSEC B-0
+		SL*	DAD		# PD 8D	  SHIFT SUCH THAT THIS PART OF X
+			10D,1		#	  IS SCALED REVS/CSEC B-0
 		BOV			# TURN OFF OVERFLOW IF SET BY SHIFT
-			+1		# INSTRUCTION BEFORE EXITING.
+			+1		# INSTRUCTION BEFORE EXITING
 		RVQ			# MPAC=X= X0+(XDOT)(T+T0)  REVS B0
 
 # Page 1146
-# ***** EARTHMX SUBROUTINE *****
+# ..... EARTHMX SUBROUTINE .....
 # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE EARTH
 #
 # CALLING SEQUENCE
-#	L	CALL
-#	L+1		EARTHMX
+#  L	   CALL
+#  L+1		  EARTHMX
 #
 # SUBROUTINE USED
-#	NEWANGLE
+#  NEWANGLE
 #
 # INPUT
-#	INPUT AVAILABLE FROM LAUNCH DATA	AZO  REVS B-0
-#						TEPHEM  CSEC B-42
-#	6-7D= TIME CSEC B-28
+#    INPUT AVAILABLE FROM LAUNCH DATA	  AZO  REVS B-0
+#					  TEPHEM  CSEC B-42
+#  6-7D= TIME CSEC B-28
 #
 # OUTPUT
-#	MMATRIX= 3X3 M MATRIX B-1	(STORED IN VAC AREA)
+#  MMATRIX= 3X3 M MATRIX B-1   (STORED IN VAC AREA)
 
 		BANK	26
 		SETLOC	PLANTIN1
 		BANK
 		COUNT*	$$/LUROT
 
-EARTHMX		STQ	SETPD		# SET 8-9D=AZO
+EARTHMX		STQ	SETPD		# SET	8-9D=AZO
 			EARTHMXX
 			8D		# 10-11D=WEARTH
-		AXT,1			# FOR SL 5, AND SL 10 IN NEWANGLE
+		AXT,1			# FOR SL 5, AND SL 10  IN NEWANGLE
 			0
-		DLOAD	PDDL		# LEAVING PD SET AT 12D FOR NEWANGLE
+		DLOAD	PDDL		#   LEAVING PD SET AT 12D FOR NEWANGLE
 			AZO
 			WEARTH
 		PUSH	CALL
 			NEWANGLE
 		SETPD	PUSH		# 18-19D=504AZ
-			18D		#			 COS(AZ)   SIN(AZ)     0
-		COS	PDDL		# 20-37D=  MMATRIX=	-SIN(AZ)   COS(AZ)     0    B-1
-			504AZ		#			    0         0        1
+			18D		#		     COS(AZ) SIN(AZ) 0
+		COS	PDDL		# 20-37D=  MMATRIX= -SIN(AZ) COS(AZ) 0 B-1
+			504AZ		#		      0       0      1
 		SIN	PDDL
 			HI6ZEROS
 		PDDL	SIN
@@ -339,20 +335,20 @@ EARTHMX		STQ	SETPD		# SET 8-9D=AZO
 			EARTHMXX
 
 # Page 1147
-# ***** EARTHL SUBROUTINE *****
+# ..... EARTHL SUBROUTINE .....
 # SUBROUTINE TO COMPUTE L VECTOR FOR EARTH
 #
 # CALLING SEQUENCE
-#	L	CALL
-#	L+1		EARTHL
+#  L	   CALL
+#  L+1		  EARTHL
 #
 # INPUT
-#	AXO,AYO SET AT LAUNCH TIME WITH AYO IMMEDIATELY FOLLOWING AXO IN CORE
+#  AXO,AYO SET AT LAUNCH TIME WITH AYO IMMEDIATELY FOLLOWING AXO IN CORE
 #
 # OUTPUT
-#		-AX
-#	MPAC=	-AY	RADIANS B-0
-#		  0
+#	    -AX
+#   MPAC=   -AY    RADIANS B-0
+#	      0
 
 		BANK	06
 		SETLOC	EARTHLOC
@@ -371,21 +367,19 @@ EARTHL		DLOAD	DCOMP
 
 # Page 1148
 # CONSTANTS AND ERASABLE ASSIGNMENTS
-
 1B1		=	DP1/2		# 1  SCALED B-1
 RPREXIT		=	S1		# R-TO-RP AND RP-TO-R SUBR EXIT
-EARTHMXX	=	S2		# EARTHMX, MOONMX SUBR. EXITS
-504RPR		=	0D		# 6 REGS	R OR RP VECTOR
-SINNODI		=	8D		# 2		SIN(NODI)
-DVECTR		=	8D		# 6		D VECTOR MOON
-CVECTR		=	8D		# 6		C VECTR MOON
-504AZ		=	18D		# 2		AZ
-TIMSUBM		=	14D		# 3		TIME SUB M (MOON) T+T0 IN GETAZ
-504LPL		=	14D		# 6		L OR LP VECTOR
-AVECTR		=	20D		# 6		A VECTOR (MOON)
-BVECTR		=	26D		# 6		B VECTOR (MOON)
-MMATRIX		=	20D		# 18		M MATRIX
-COB		=	32D		# 2		COS(B) B-1
-SOB		=	34D		# 2		SIN(B) B-1
-504F		=	6D		# 2		F(MOON)
-
+EARTHMXX	=	S2		# EARTHMX,MOONMX SUBR. EXITS
+504RPR		=	0D		# 6 REGS  R OR RP VECTOR
+SINNODI		=	8D		# 2	  SIN(NODI)
+DVECTR		=	8D		# 6	  D VECTOR MOON
+CVECTR		=	8D		# 6	  C VECTR MOON
+504AZ		=	18D		# 2	 AZ
+TIMSUBM		=	14D		# 3	  TIME SUB M (MOON) T+T0 IN GETAZ
+504LPL		=	14D		# 6	  L OR LP VECTOR
+AVECTR		=	20D		# 6	  A VECTOR (MOON)
+BVECTR		=	26D		# 6	  B VECTOR (MOON)
+MMATRIX		=	20D		# 18	  M MATRIX
+COB		=	32D		# 2	  COS(B) B-1
+SOB		=	34D		# 2	  SIN(B) B-1
+504F		=	6D		# 2	  F (MOON)

Luminary099/R30.agc

@@ -40,51 +40,51 @@
 # USED THROUGHOUT.		CALCULATE AND DISPLAY ORBITAL PARAMETERS
 #
 # 1.	IF AVERAGE G IS OFF:
-#		FLASH DISPLAY V04N06.  R2 INDICATES WHICH SHIP'S STATE VECTOR IS
-#			TO BE UPDATED.  INITIAL CHOICE IS THIS SHIP (R2=1).  ASTRONAUT
-#			CAN CHANGE TO OTHER SHIP BY V22E XE. WHERE X IS NOT EQ 1.
+#		FLASH DISPLAY V04N06. R2 INDICATES WHICH SHIP'S STATE VECTOR IS
+#		 TO BE UPDATED. INITIAL CHOICE IS THIS SHIP (R2=1). ASTRONAUT
+#		 CAN CHANGE TO OTHER SHIP BY V22EXE, WHERE X NOT EQ 1.
 #		SELECTED STATE VECTOR UPDATED BY THISPREC (OTHPREC).
 #		CALLS SR30.1 (WHICH CALLS TFFCONMU + TFFRP/RA) TO CALCULATE
-#			RPER (PERIGEE RADIUS), RAPO (APOGEE RADIUS), HPER (PERIGEE
-#			HEIGHT ABOVE LAUNCH PAD OR LUNAR LANDING SITE), HARD (APOGEE
-#			HEIGHT AS ABOVE), TPER (TIME TO PERIGEE), TFF (TIME TO
-#			INTERSECT 300 KFT ABOVE PAD OR 35KFT ABOVE LANDING SITE).
-#		FLASH MONITOR V16N44 (HAPO, HPER, TFF).  TFF IS -59M59S IF IT WAS
-#			NOT COMPUTABLE, OTHERWISE IT INCREMENTS ONCE PER SECOND.
-#			ASTRONAUT HAS OPTION TO MONITOR TPER BY KEYING IN N 32 E.
-#			DISPLAY IS IN HMS, IS NEGATIVE (AS WAS TFF), AND INCREMENTS
-#			ONCE PER SECOND ONLY IF TFF DISPLAY WAS -59M59S.
-#	2.	IF AVERAGE G IS ON:
-#			CALLS SR30.1 APPROX EVERY TWO SECS.  STATE VECTOR IS ALWAYS
-#				FOR THIS VEHICLE.  V82 DOES NOT DISTURB STATE VECTOR.  RESULTS
-#				OF SR30.1 ARE RAPO, RPER, HAPO, HPER, TPER, TFF.
-#			FLASH MONITOR V16N44 (HAPO, HPER, TFF).
-#	ADDENDUM:  HAPO AND HPER SHOULD BE CHANGED TO READ HAPOX AND HPERX IN THE
-#		ABOVE REMARKS.
+#		 RPER (PERIGEE RADIUS), RAPO (APOGEE RADIUS), HPER (PERIGEE
+#		 HEIGHT ABOVE LAUNCH PAD OR LUNAR LANDING SITE), HARD (APOGEE
+#		 HEIGHT AS ABOVE), TPER (TIME TO PERIGEE), TFF (TIME TO
+#		 INTERSECT 300 KFT ABOVE PAD OR 35KFT ABOVE LANDING SITE).
+#		FLASH MONITOR V16N44 (HAPO, HPER, TFF).TFF IS -59M59S IF IT WAS
+#		 NOT COMPUTABLE, OTHERWISE IT INCREMENTS ONCE PER SECOND.
+#		 ASTRONAUT HAS OPTION TO MONITOR TPER BY KEYING IN N 32 E.
+#		 DISPLAY IS IN HMS, IS NEGATIVE (AS WAS TFF), AND INCREMENTS
+#		 ONCE PER SECOND ONLY IF TFF DISPLAY WAS -59M59S.
 #
-# CALLING SEQUENCE: VERB 82 ENTER.
+# 2.	IF AVERAGE G IS ON:
+#		CALLS SR30.1 APPROX EVERY TWO SECS.  STATE VECTOR IS ALWAYS
+#		 FOR THIS VEHICLE. V82 DOES NOT DISTURB STATE VECTOR.  RESULTS
+#		 OF SR30.1 ARE RAPO, RPER, HAPO, HPER, TPER, TFF.
+#		FLASH MONITOR V16N44 (HAPO, HPER, TFF).
+# ADDENDUM: HAPO AND HPER SHOULD BE CHANGED TO READ HAPOX AND HPERX IN THE
+#		 ABOVE REMARKS.
 #
-# SUBROUTINES CALLED:	SR30.1, GOXDSPF
-#			MAYBE -- THISPREC, OTHPREC, LOADTIME, DELRSPL
+# CALLING SEQUENCE:  VERB 82 ENTER.
 #
+# SUBROUTINES CALLED:  SR30.1, GOXDSPF
+#			MAYBE - THISPREC , OTHPREC, LOADTIME, DELRSPL
 # NORMAL EXIT MODES:  TC ENDEXT
 #
 # ALARMS:  NONE
 #
-# OUTPUT:	HAPOX	(-29) M
-#		HPERX	(-29) M
-#		RAPO	(-29) M EARTH
+# OUTPUT:  HAPOX	(-29) M
+#	   HPERX	(-29) M
+#	   RAPO		(-29) M EARTH
 #			(-27) M MOON
-#		RPER	(-29) M EARTH
+#	   RPER		(-29) M EARTH
 #			(-27) M MOON
-#		TFF	(-28) CS	CONTAINS NEGATIVE QUANTITY
-#		-TPER	(-28) CS	CONTAINS NEGATIVE QUANTITY
-#
+#	   TFF		(-28) CS	CONTAINS NEGATIVE QUANTITY
+#	   -TPER	(-28) CS	CONTAINS NEGATIVE QUANTITY
 # Page 713
-# ERASABLE INITIALIZATION REQUIRED:  STATE VECTOR.
 #
-# DEBRIS:	QPRET, RONE, VONE, TFF/RTMU, HPERMIN, RPADTEM, V82EMFLG.
-#		MAYBE:  TSTART82, V82FLAGS, TDEC1.
+# ERASABLE INITIALIZATION REQUIRED: STATE VECTOR.
+#
+# DEBRIS:	QPRET, RONE, VONE,TFF/RTMU, HPERMIN, RPADTEM, V82EMFLG.
+#		MAYBE: TSTART82, V82FLAGS, TDEC1.
 
 		EBANK=	HAPOX
 		BANK	31
@@ -108,8 +108,8 @@ V82GOFF		EXIT			# ALLOW ASTRONAUT TO SELECT VEHICLE
 		CADR	GOXDSPF
 		TC	ENDEXT		# TERMINATE
 		TC	+2		# PROCEED
-		TC	-5		# DATA IN.  OPTION1+1 = 1 FOR THIS VEHICLE
-					#		UNEQ 1 FOR OTHER VEHICLE
+		TC	-5		# DATA IN. OPTION1+1 = 1 FOR THIS VEHICLE.
+					#		UNEQ 1 FOR OTHER VEHICLE.
 		CAF	BIT4		# 80 MS
 		TC	WAITLIST
 		EBANK=	TFF
@@ -140,9 +140,9 @@ V82STALL	CAF	THREE		# STALL IN THIS LOOP AND WITHOLD V 16 N 44
 FLAGGON		CAF	V16N44		# MONITOR HAPO,HPER,TFF.
 		TC	BANKCALL
 		CADR	GOXDSPF
-		TC	B5OFF		# TERM. THIS TELLS TICKTEST TO KILL ITSELF
-		TC	B5OFF		# PROCEED.  DITTO
-		TC	V82GOFLP	# RECYCLE.  RECOMPUTE STATE VECT + DISPLAY
+		TC	B5OFF		# TERM  THIS TELLS TICKTEST TO KILL ITSELF
+		TC	B5OFF		# PROCEED  DITTO
+		TC	V82GOFLP	# RECYCLE  RECOMPUTE STATE VECT + DISPLAY
 
 OPTIONVN	VN	412
 V16N44		VN	1644
@@ -162,16 +162,16 @@ OTHSHIP		TC	INTPRET
 		CALL			# CALL STATE VECTOR UPDATE FOR OTHER SHIP.
 			OTHPREC
 BOTHSHIP	VLOAD			# MOVE RESULTS INTO TFFCONIC STORAGE AREAS
-			RATT		# TO BE CALLED BY SR30.1.
-		STOVL	RONE		# RATT AT (-29)M FOR EARTH OR MOON.
+			RATT		#  TO BE CALLED BY SR30.1.
+		STOVL	RONE		# RATT AT (-29)M FOR EARTH OR MOON
 			VATT
-		STORE	VONE		# VATT AT (-7)M/CS FOR EARTH OR MOON
+		STORE	VONE		#  VATT AT (-7)M/CS FOR EARTH OR MOON
 		DLOAD*
-			1/RTMUE,2	# X2 IS 0 FOR EARTH CENTERED STATE VEC
-		STORE	TFF/RTMU	# X2 IS 2 FOR MOON
+			1/RTMUE,2	#  X2 IS 0 FOR EARTH CENTERED STATE VEC
+		STORE	TFF/RTMU	#  X2 IS 2 FOR MOON
 		DLOAD*			# AS LEFT BY THISPREC OR OTHPREC.
 			MINPERE,2
-		STORE	HPERMIN		# TFFRTMU, HPERMIN, AND RPADTEM ARE ALL
+		STORE	HPERMIN		#   TFFRTMU, HPERMIN AND RPADTEM ARE ALL
 		SLOAD	BHIZ		# EARTH/MOON PARAMETERS AS SET HERE.
 			X2
 			EARTHPAD
@@ -184,41 +184,41 @@ THISSHIP	TC	INTPRET
 		GOTO
 			BOTHSHIP
 
-# THE FOLLOWING CONSTANTS ARE PAIRWISE INDEXED.  DO NOT SEPARATE PAIRS.
+# THE FOLLOWING CONSTANTS ARE PAIRWISE INDEXED. DO NOT SEPARATE PAIRS.
 
 MINPERM		2DEC	10668 B-27	# 35 KFT MIN PERIGEE HEIGHT FOR MOON(-27)M
 
 MINPERE		2DEC	91440 B-29	# 300 KFT (-29)M FOR EARTH
 
-EARTHPAD	DLOAD	CLRGO		# PAD 37-B RADIUS.  SCALED AT (-29)M
+EARTHPAD	DLOAD	CLRGO		#  PAD 37-B RADIUS.  SCALED AT (-29)M.
 			RPAD
-			V82EMFLG	# INDICATE EARTH SCALING FOR SR30.1
+			V82EMFLG	#  INDICATE EARTH SCALING FOR SR30.1
 			BOTHPAD
 
 MOONPAD		VLOAD	ABVAL		# COMPUTE MOON PAD RADIUS FROM RLS VECTOR.
-			RLS		# SCALED AT (-27)M
+			RLS		#  SCALED AT (-27)M.
 		SET
-			V82EMFLG	# INDICATE MOON SCALILNG FOR SR30.1
+			V82EMFLG	#  INDICATE MOON SCALING FOR SR30.1
 BOTHPAD		STCALL	RPADTEM
 			SR30.1		# CALCULATE ORBITAL PARAMETERS
 		RTB	DSU
 			LOADTIME
-			TSTART82	# PRESENT TIME -- TIME V82GOFF1 BEGAN
-		STORE	TSTART82	#                 SAVE IT
+			TSTART82	# PRESENT TIME - TIME V82GOFF1 BEGAN
+		STORE	TSTART82	#                SAVE IT
 		DLOAD	BZE		# SR30.1 SETS -TPER=0 IF HPER L/
-			-TPER		# HPERMIN (300 OR 35) KFT.
+			-TPER		#  HPERMIN (300 OR 35) KFT.
 			TICKTIFF	# (-TPER = 0)
-TICKTPER	DLOAD	DAD		# (-TPER NON ZERO) TFF WAS NOT COMPUTED.
-			-TPER		# BUT WAS SET TO 59M59S.  DON'T DICK TFF, DO
-			TSTART82	# TICK -TPER.  DISPLAY BOTH.
+TICKTPER	DLOAD	DAD		# (-TPER NON ZERO)  TFF WAS NOT COMPUTED.
+			-TPER		# BUT WAS SET TO 59M59S.DONT TICK TFF, DO
+			TSTART82	# TICK -TPER. DISPLAY BOTH.
 		STORE	-TPER		# -TPER CORRECTED FOR TIME SINCE V82GOFF1
-		EXIT			# BEGAN
+		EXIT			# BEGAN.
 		CAF	BIT1
 		TS	V82FLAGS	# INFORMS TICKTEST TO INCREMENT ONLY -TPER
 		TC	ENDOFJOB
 
-TICKTIFF	DLOAD	DAD		# (-TPER=0) TFF WAS COMPUTED.  TICK TFF.
-			TFF		# DO NOT TICK -TPER.  DISPLAY TFF, BUT NOT
+TICKTIFF	DLOAD	DAD		# (-TPER=0)  TFF WAS COMPUTED.TICK TFF.
+			TFF		# DO NOT TICK -TPER.DISPLAY TFF, BUT NOT
 			TSTART82	# -TPER.
 		STORE	TFF		# TFF CORRECTED FOR TIME SINCE V82GOFF1
 		EXIT			# BEGAN.
@@ -232,7 +232,7 @@ TICKTEST	CAF	BIT5		# THIS WAITLIST PROGRAM PERPETUATES ITSELF
 		CCS	A
 		TC	DOTICK
 		CAF	PRIO25
-		TC	NOVAC		# TERMINATE V 82.  CAN'T CALL ENDEXT IN RUPT.
+		TC	NOVAC		# TERMINATE V 82.CANT CALL ENDEXT IN RUPT.
 		EBANK=	EXTVBACT
 		2CADR	ENDEXT
 
@@ -246,10 +246,10 @@ DOTICK		CAF	1SEC		# RE-REQUEST TICKTEST.
 		MASK	V82FLAGS
 		INDEX	A
 		TC	+1
-		TC	TASKOVER	# IF NO FLAGBITS SET DONT' CHANGE TFF OR
+		TC	TASKOVER	# IF NO FLAGBITS SET DONT CHANGE TFF OR
 					# -TPER, BUT CONTINUE LOOP.
-		TC	TPERTICK	# ONLY BIT 1 SET.  INCR -TPER BY 1 SEC.
-TFFTICK		CAF	1SEC		# ONLY BIT 2 SET.  INCR TFF BY 1 SEC.
+		TC	TPERTICK	# ONLY BIT 1 SET. INCR -TPER BY 1 SEC.
+TFFTICK		CAF	1SEC		# ONLY BIT 2 SET. INCR TFF BY 1 SEC.
 		TS	L
 		CAF	ZERO
 		DAS	TFF
@@ -261,7 +261,7 @@ TPERTICK	CAF	1SEC
 		TC	TASKOVER
 
 # Page 717
-V82GON		EXIT			# AVERAGE G ON.  USE CURRENT STATE VECTOR
+V82GON		EXIT			#  AVERAGE G ON. USE CURRENT STATE VECTOR
 					# FOR ORBITAL PARAMETER CALCULATIONS.
 		CAF	PRIO7		# LESS THAN LAMBERT
 		TC	FINDVAC		# V82GON1 WILL PERFORM ORBIT CALCULATIONS
@@ -270,7 +270,7 @@ V82GON		EXIT			# AVERAGE G ON.  USE CURRENT STATE VECTOR
 
 		RELINT
 		CCS	NEWJOB		# WITHOLD V16 N44 UNTIL FIRST ORBIT CALC
-		TC	CHANG1		# IS DONE.  NOTE:  V82GON1 (PRIO7, FINDVAC
+		TC	CHANG1		# IS DONE. NOTE: V82GON1 (PRIO7, FINDVAC
 					# JOB) IS COMPLETED BEFORE V82GON (PRIO7,
 					# NOVAC JOB).
 V82REDSP	CAF	V16N44		# MONITOR HAPO, HPER, TFF
@@ -283,23 +283,23 @@ V82REDSP	CAF	V16N44		# MONITOR HAPO, HPER, TFF
 V82GON1		TC	INTPRET		# THIS EXEC PROGRAM PERPETUATES ITSELF
 					# ONCE A SEC UNTIL BIT 5 OF EXTVBACT =0.
 		VLOAD	GOTO		# HOLDS OFF CCS NEWJOB BETWEEN RN AND
-			RN		# VN FETCH SO RN, VN ARE FROM SAME
-			NEXTLINE	# STATE VECTOR UPDATE.
-NEXTLINE	STOVL	RONE		# RN AT (-29)M FOR EARTH OR MOON
+			RN		#   VN FETCH SO RN , VN ARE FROM SAME
+			NEXTLINE	#   STATE VECTOR UPDATE.
+NEXTLINE	STOVL	RONE		#  RN AT (-29)M FOR EARTH OR MOON
 			VN
 		STORE	VONE		# VN AT (-7)M/CS FOR EARTH OR MOON
 		BON	GOTO
 			MOONTHIS	# FLAG INDICATES BODY ABOUT WHICH ORBITAL
-			MOONGON		# CALCULATIONS ARE TO BE PERFORMED.
-			EARTHGON	# IF SET -- MOON, IF RESET --EARTH.
+			MOONGON		#    CALCULATIONS ARE TO BE PERFORMED.
+			EARTHGON	#   IF SET - MOON , IF RESET - EARTH.
 
 MOONGON		SET	DLOAD
-			V82EMFLG	# FLAG MOON SCALING FOR SR30.1
+			V82EMFLG	# INDICATE MOON SCALING FOR SR30.1
 			1/RTMUM		# LUNAR PARAMETERS LOADED HERE FOR SR30.1
 		STODL	TFF/RTMU
 			MINPERM
 		STOVL	HPERMIN
-			RLS		# SCALED AT (-27)M
+			RLS		#  SCALED AT (-27)M.
 		ABVAL	GOTO
 			V82GON2
 EARTHGON	CLEAR	DLOAD
@@ -319,7 +319,7 @@ V82GON3		CAF	BIT5
 		BZF	ENDEXT		# YES, TERMINATE VB 82 LOOP
 		CAF	1SEC
 		TC	BANKCALL	# WAIT ONE SECOND BEFORE REPEATING
-		CADR	DELAYJOB	# ORBITAL PARAMETER COMPUTATION.
+		CADR	DELAYJOB	#   ORBITAL PARAMETER COMPUTATION.
 		TC	V82GON1
 
 SPLRET		=	V82GON3
@@ -433,9 +433,9 @@ STORHAPO	STODL	HAPOX
 STORHPER	STODL	HPERX		# STORE (RPER - RPADTEM) INTO HPERX.
 			MPAC 	+4
 		DSU	BPL		# HPERMIN AT (-29)M FOR EARTH, (-27)M MOON
-			HPERMIN		# IF HPER L/ HPERMIN (300 OR 35) KFT,
-			DOTPER		# THEN ZERO INTO -TPER.
-		DLOAD	GOTO		# OTHERWISE CALCULATE TPER.
+			HPERMIN		# IF HPER L/   HPERMIN (300 OR 35)KFT,
+			DOTPER		#  THEN ZERO INTO -TPER.
+		DLOAD	GOTO		#   OTHERWISE CALCULATE TPER.
 			HI6ZEROS
 			SKIPTPER
 DOTPER		DLOAD	CALL
@@ -447,19 +447,18 @@ SKIPTPER	STODL	-TPER
 		DAD	CALL
 			RPADTEM		# RPADTEM AT (-29)M FOR EARTH, (-27)M MOON
 			CALCTFF		# GIVES 59M59S FOR TFF IF HPER G/
-		DCOMP			# HPERMIN + RPADTEM.  (TPER WAS NON ZERO)
+		DCOMP			#   HPERMIN + RPADTEM. (TPER WAS NON ZERO)
 		STCALL	TFF		# OTHERWISE COMPUTES TFF.	(GOTO)
 			S2
 
 MAXCHK		DSU	BPL		# IF C(MPAC) > 9999.9 NM. MPAC = 9999.9 NM.
 			MAXNM
-			+3		# OTHERWISE C(MPAC) - B(MPAC).
+			+3		# OTHERWISE C(MPAC) = B(MPAC).
 		DAD	RVQ
 			MAXNM
- +3		DLOAD	RVQ		# (USED BY P30 -- P37 ALSO)
+ +3		DLOAD	RVQ		# (USED BY P30 - P37 ALSO)
 			MAXNM
 
 MAXNM		2OCT	0106505603
 
 # Page 722 (empty page)
-

Luminary099/R31.agc

@@ -67,12 +67,12 @@ DISPN5X		CAF	V16N54
 V83CALL		CS	FLAGWRD7	# TEST AVERAGE G FLAG
 		MASK	AVEGFBIT
 		EXTEND
-		BZF	MUNG?		# ON.  TEST MUNFLAG
+		BZF	MUNG?		# ON - TEST MUNFLAG
 
 		CS	FLAGWRD8
 		MASK	SURFFBIT
 		EXTEND
-		BZF	ONEBASE		# ON SURFACE -- BYPASS LEMPREC
+		BZF	ONEBASE		# ON SURFACE - BYPASS LEMPREC
 
 		TC	INTPRET		# EXTRAPOLATE BOTH STATE VECTORS
 		RTB
@@ -104,7 +104,7 @@ REV83		CS	FLAGWRD7
 		CS	FLAGWRD8
 		MASK	SURFFBIT
 		EXTEND
-		BZF	R31SURF		# IF ON SURFACE, USE LEMAREC
+		BZF	R31SURF		# IF ON SURFACE,USE LEMAREC
 
 		TC	INTPRET		# DO CONIC EXTRAPOLATION FOR BOTH VEHICLES
 		RTB
@@ -125,13 +125,13 @@ REV83		CS	FLAGWRD7
 		SET
 			INTYPFLG	# CONIC EXTRAP.
 		STCALL	TET
-			INTEGRVS	# INTEGRATION --- AT LAST ---
+			INTEGRVS	# INTEGRATION --- AT LAST---
 OTHCONIC	VLOAD
 # Page 705
 			RATT
 		STOVL	RONE
 			VATT
-		STCALL	VONE		# GET SET FOR CONIC EXTRAP., OTHER.
+		STCALL	VONE		# GET SET FOR CONIC EXTRAP.,OTHER.
 			INTSTALL
 		SET	DLOAD
 			INTYPFLG
@@ -160,7 +160,7 @@ COMPDISP	VLOAD	VSU
 			0,1
 		STOVL	RANGE		# SCALED 2(29)M
 			VATT
-		VSU	DOT		# (VCM-VLM).UNIT(LOS), PD=0
+		VSU	DOT		# (VCM- VLM).UNIT(LOS). PD=0
 			VONE
 		SL1			# SCALED 2(7)M/CS
 		STOVL	RRATE
@@ -169,9 +169,9 @@ COMPDISP	VLOAD	VSU
 			UNITZ
 		CALL
 			CDU*NBSM
-		VXM	PUSH		# UNIT(Z)/4 TO PD 6-11
+		VXM	PUSH		# UNIT (Z)/4 TO PD 6-11
 			REFSMMAT
-		VPROJ	VSL2		# UNIT(P)=UNIT(UZ-(UZ)PROJ(UR))
+		VPROJ	VSL2		# UNIT(P)=UNIT(UZ -(UZ)PROJ(UR))
 			0D
 		BVSU	UNIT
 			6D
@@ -179,10 +179,10 @@ COMPDISP	VLOAD	VSU
 			0D		# UNIT(RL)
 			VONE
 # Page 706
-		VXV	DOT		# (UR * VL) * UR . U(P)
+		VXV	DOT		# (UR * VL)*UR . U(P)
 			0D
 			12D
-		PDVL			# SIGN TO 12-13, LOAD U(P)
+		PDVL			# SIGN TO 12-13 , LOAD U(P)
 		DOT	SIGN
 			6D
 			12D
@@ -190,7 +190,7 @@ COMPDISP	VLOAD	VSU
 		STOVL	RTHETA
 			0D
 		DOT	BPL		# IF UR.UZ NEG,
-			6D		#	RTHETA = 1 - RTHETA
+			6D		#   RTHETA = 1 - RTHETA
 			+5
 		DLOAD	DSU
 			DPPOSMAX
@@ -201,7 +201,7 @@ COMPDISP	VLOAD	VSU
 		CA	BIT5
 		MASK	EXTVBACT
 		EXTEND			# IF ANSWERED,
-		BZF	ENDEXT		#	TERMINATE
+		BZF	ENDEXT		#	 TERMINATE
 
 		CS	EXTVBACT
 		MASK	BIT12
@@ -212,12 +212,12 @@ GETRVN		CA	PRIO22		# INHIBIT SERVICER
 		TC	PRIOCHNG
 		TC	INTPRET
 		VLOAD	SETPD
-			RN		# LM STATE VECTOR IN RN,VN.
+			RN		# LM STATE VECTOR IN RN,VN
 			0
 		STOVL	RONE
 			VN
 		STOVL	VONE		# LOAD R(CSM),V(CSM) IN CASE MUNFLAG SET
-			V(CSM)		# (TO INSURE TIME COMPATIBILITY)
+			V(CSM)		# (TO INSURE TIME COMPATABILITY)
 		PDVL	PDDL
 			R(CSM)
 			PIPTIME
@@ -246,7 +246,7 @@ GETRVN2		CALL
 			OTHINT
 R31SURF		TC	INTPRET
 		RTB			# LM IS ON SURFACE, SO PRECISION
-			LOADTIME	# INTEGRATION USED PLANETARY INERTIAL
+			LOADTIME	# INTEGRATION USES PLANETARY INERTIAL
 		STCALL	TDEC1		# ORIENTATION SUBROUTINE
 			LEMPREC
 		GOTO			# DO CSM CONIC
@@ -264,4 +264,3 @@ ONEBASE		TC	INTPRET		# GET CSM BASE VECTOR
 V16N54		VN	1654
 
 # Page 708 (empty page)
-

Luminary099/R60_62.agc

@@ -27,8 +27,8 @@
 #	16:27 JULY 14, 1969
 
 # Page 472
-# MOD NO: 0				DATE: 1 MAY 1968
-# MOD BY: DIGITAL DEVEL GROUP		LOG SECTION R60,R62
+# MOD NO: 0			DATE: 1 MAY 1968
+# MOD BY: DIGITAL DEVEL GROUP	LOG SECTION R60,R62
 #
 # FUNCTIONAL DESCRIPTION:
 #
@@ -42,21 +42,21 @@
 #
 # 3. REQUEST FLASHING DISPLAY V50 N18 PLEASE PERFORM AUTO MANEUVER.
 #
-# 4. IF PRIORITY DISPLAY FLAG IS SET DO A PHASECHANGE.  THEN AWAIT
+# 4. IF PRIORITY DISPLAY FLAG IS SET DO A PHASECHANGE. THEN AWAIT
 # ASTRONAUT RESPONSE.
 #
-# 5. DISPLAY RESPONSE RETURNS.
+# 5. DISPLAY RESPONSE RETURNS:
 #
-#	A. 	ENTER -- RESET 3-AXIS FLAG AND RETURN TO CLIENT.
+#     A. ENTER - RESET 3-AXIS FLAG AND RETURN TO CLIENT.
 #
-#	B.	TERMINATE -- IF IN P00 GO TO STEP 5A.  OTHERWISE CHECK IF R61 IS
-#		THE CALLING PROGRAM.  IF IN R61 AN EXIT IS MADE TO GOTOV56.  IF
-#		NOT IN R61 AN EXIT IS DONE VIA GOTOPOOH.
+#     B. TERMINATE - IF IN P00 GO TO STEP 5A. OTHERWISE CHECK IF R61 IS
+#	 THE CALLING PROGRAM. IF IN R61 AN EXIT IS MADE TO GOTOV56. IF
+#	 NOT IN R61 AN EXIT IS DONE VIA GOTOPOOH.
 #
-#	C.	PROCEED -- CONTINUE WITH PROGRAM AT STEP 6.
+#     C. PROCEED - CONTINUE WITH PROGRAM AT STEP 6.
 #
 # 6. IF THE 3-AXISFLAG IS NOT SET, THE FINAL CDU ANGLES ARE CALCULATED
-# (VECPOINT).
+#    (VECPOINT).
 #
 # 7. THE FDAI BALL ANGLES (NOUN 18) ARE CALCULATED (BALLANGS).
 #
@@ -64,32 +64,32 @@
 #
 # 9. IF THE AUTO SWITCH IS NOT SET GO BACK TO STEP 3.
 #
-# 10. NON-FLASHING DISPLAY V06N18 (FDAI ANGLES).
+# 10. NONFLASHING DISPLAY V06N18 (FDAI ANGLES).
 #
-# 11. DO A PHASE-CHANGE.
+# 11. DO A PHASECHANGE.
 #
 # 12. DO A MANEUVER CALCULATION AND ICDU DRIVE ROUTINE TO ACHIEVE FINAL
-# GIMBAL ANGLES (GOMANUR).
 #
-# 13. AT END OF MANEUVER TO TO STEP 3.
+#     GIMBAL ANGLES (GOMANUR).
+# 13. AT END OF MANEUVER GO TO STEP 3.
 #
-#	IF SATISFACTORY MANEUVER STEP 5A EXITS R60.
-#	FOR FURTHER ADJUSTMENT OF THE VEHICLE ATTITUDE ABOUT THE
-#	DESIRED VECTOR, THE ROUTINE MAY BE PERFORMED AGAIN STARTING AT
+#	   IF SATISFACTORY MANEUVER STEP 5A EXITS R60.
+#	   FOR FURTHER ADJUSTMENT OF THE VEHICLE ATTITUDE ABOUT THE
+#	   DESIRED VECTOR, THE ROUTINE MAY BE PERFORMED AGAIN STARTING AT
 # Page 473
-#	STEP 5C.
+#	   STEP 5C.
 #
-# CALLING SEQUENCE:	TC	BANKCALL
-#			CADR	R60LEM
+# CALLING SEQUENCE:  TC BANKCALL
+#		     CADR R60LEM
 #
-# ERASABLE INITIALIZATION REQUIRED:	SCAXIS, POINTVSM (FOR VECPOINT)
-#					3AXISFLG.
+# ERASABLE INITIALIZATION REQUIRED : SCAXIS, POINTVSM (FOR VECPOINT)
+#				     3AXISFLG.
 #
-# SUBROUTINES CALLED:	VECPOINT, BALLANGS, GOPERF24, LINUS, GODSPER,
-#			GOMANUR, DOWNFLAG, PHASCHNG, UPFLAG
+# SUBROUTINES CALLED: VECPOINT, BALLANGS, GOPERF2R, LINUS, GODSPER,
+#		     GOMANUR, DOWNFLAG, PHASCHNG, UPFLAG
 #
-# NORMAL EXIT MODES:	CAE	TEMPR60		(CALLER'S RETURN ADDRESS)
-#			TC	BANKJUMP
+# NORMAL EXIT MODES: CAE TEMPR60   (CALLERS RETURN ADDRESS)
+#		     TC  BANKJUMP
 #
 # ALARMS: NONE
 #
@@ -114,7 +114,7 @@ REDOMANN	CAF	3AXISBIT
 		TC	INTPRET
 		CALL
 			VECPOINT	# TO COMPUTE FINAL ANGLES
-		STORE	CPHI		# STORE FINAL ANGLES -- CPHI, CTHETA, CPSI
+		STORE	CPHI		# STORE FINAL ANGLES - CPHI,CTHETA,CPSI
 		EXIT
 
 TOBALL		TC	BANKCALL
@@ -124,7 +124,7 @@ TOBALLA		CAF	V06N18
 		CADR	GOPERF2R	# DISPLAY PLEASE PERFORM AUTO MANEUVER
 		TC	R61TEST
 		TC	REDOMANC	# PROCEED
-		TC	ENDMANU1	# ENTER I.E., FINISHED WITH R60
+		TC	ENDMANU1	# ENTER I.E. FINISHED WITH R60
 # Page 474
 		TC	CHKLINUS	# TO CHECK FOR PRIORITY DISPLAYS
 		TC	ENDOFJOB
@@ -162,11 +162,11 @@ ENDMANU1	TC	DOWNFLAG	# RESET 3-AXIS FLAG
 CHKLINUS	CS	FLAGWRD4
 		MASK	PDSPFBIT	# IS PRIORITY DISPLAY FLAG SET?
 		CCS	A
-		TC	Q		# NO -- EXIT
+		TC	Q		# NO - EXIT
 		CA	Q
 		TS	MPAC +2		# SAVE RETURN
 		CS	THREE		# OBTAIN LOCATION FOR RESTART
-		AD	BUF2		# HOLD Q OF LAST DISPLAY
+		AD	BUF2		# HOLDS Q OF LAST DISPLAY
 		TS	TBASE2
 
 		TC	PHASCHNG
@@ -208,7 +208,7 @@ R61TEST		CA	MODREG		# IF WE ARE IN P00 IT MUST BE V49 OR V89
 		EXTEND
 		BZF	ENDMANU1	# THUS WE GO TO ENDEXT VIA USER
 
-		CA	FLAGWRD4	# ARE WE IN R61 (P20 OR P25)
+		CA	FLAGWRD4	# ARE WE IN R61  (P20 OR P25)
 		MASK	PDSPFBIT
 		EXTEND
 		BZF	GOTOPOOH	# NO
@@ -218,69 +218,62 @@ BIT14+7		OCT	20100
 OCT203		OCT	203
 V06N18		VN	0618
 
-# SUBROUTINE TO CHECK FOR G+N CONTROL, AUTO STABILIZATION
+# SUBROUTINE TO CHECK FOR G+N CONTROL. AUTO STABILIZATION
 #
-# RETURNS WITH C(A) = + 	IF NOT SET FOR G+N, AUTO
-# RETURNS WITH C(A) = +0	IF SWITCHES ARE SET
+# RETURNS WITH C(A) = +  IF NOT SET FOR G+N, AUTO
+# RETURNS WITH C(A) = +0 IF SWITCHES ARE SET
 
 G+N,AUTO	EXTEND
 		READ	CHAN30
 		MASK	BIT10
 		CCS	A
-		TC	Q		# NOT IN G+N	C(A) = +
+		TC	Q		# NOT IN G+N  C(A) = +
 # Page 476
 ISITAUTO	EXTEND			# CHECK FOR AUTO MODE
 		READ	CHAN31
 		MASK	BIT14
-		TC	Q		# (+) = NOT IN AUTO, (+0) = AOK
+		TC	Q		# (+) = NOT IN AUTO,  (+0) = AOK
 
 # Page 477
 # PROGRAM DESCRIPTION BALLANGS
-# MOD NO.				LOG SECTION R60,R62
-#
-# WRITTEN BY RAMA M. AIYAWAR
+# MOD NO.	  LOG SECTION  R60,R62
 #
+# WRITTEN BY RAMA M.AIYAWAR
 # FUNCTIONAL DESCRIPTION
 #
-# 	COMPUTES LM FDAI BALL DISPLAY ANGLES
-#
+# COMPUTES LM FDAI BALL DISPLAY ANGLES
 # CALLING SEQUENCE
 #
-#	TC	BALLANGS
-#
+#		TC	BALLANGS
 # NORMAL EXIT MODE
 #
-#	TC	BALLEXIT	# (SAVED Q)
-#
-# ALARM OR EXIT MODE:	NIL
+#		TC	BALLEXIT	# (SAVED Q)
 #
+# ALARM OR EXIT MODE  NIL
 # SUBROUTINES CALLED
-#
-#	CD*TR*G
-#	ARCTAN
+#		CD*TR*G
+#		ARCTAN
 #
 # INPUT
 #
-#	CPHI,CTHETA,CPSI ARE THE ANGLES CORRESPONDING TO AOG, AIG, AMG.  THEY ARE
-#	SP,2'S COMPLEMENT SCALED TO HALF REVOLUTION.
-#
+# CPHI,CTHETA,CPSI  ARE  THE ANGLES CORRESPONDING TO AOG,AIG,AMG. THEY ARE
+# SP,2S COMPLIMENT SCALED TO HALF REVOLUTION.
 # OUTPUT
 #
-#	FDAIX, FDAIY, FDAIZ ARE THE REQUIRED BALL ANGLES SCALED TO HALF REVOLUTION
-#	SP,2'S COMPEMENT.
-#
-#	THESE ANGLES WILL BE DISPLAYED AS DEGREES AND HUNDREDTHS, IN THE ORDER ROLL, PITCH, YAW, USING NOUNS 18 & 19.
+# FDAIX,FDAIY,FDAIZ ARE THE REQUIRED BALL ANGLES SCALED TO HALF REVOLUTION
+# SP,2S COMPLIMENT.
+# THESE ANGLES WILL BE DISPLAYED AS DEGREES AND HUNDREDTHS. IN THE ORDER  ROLL, PITCH, YAW, USING NOUNS 18 & 19.
 #
 # ERASABLE INITIALIZATION REQUIRED
 #
-#	CPHI, CTHETA, CPSI 	EACH AN SP REGISTER
-#
+# CPHI,CTHETA,CPSI EACH A SP REGISTER
 # DEBRIS
 #
-#	A,L,Q,MPAC,SINCDU,COSCDU,PUSHLIST,BALLEXIT
+# A,L,Q,MPAC,SINCDU,COSCDU,PUSHLIS,BALLEXIT
 #
-# NOMENCLATURE:	CPHI, CTHETA, & CPSI REPRESENT THE OUTER, INNER, AND MIDDLE GIMBAL ANGLES, RESPECTIVELY; OR
-# 		EQUIVALENTLY, CDUX, CDUY, AND CDUZ.
+#
+# NOMENCLATURE:	 CPHI, CTHETA, & CPSI REPRESENT THE OUTER, INNER, & MIDDLE GIMBAL ANGLES, RESPECTIVELY; OR
+# EQUIVALENTLY, CDUX, CDUY, & CDUZ.
 #
 # NOTE:  ARCTAN CHECKS FOR OVERFLOW AND SHOULD BE ABLE TO HANDLE ANY SINGULARITIES.
 
@@ -314,7 +307,7 @@ BALLANGS	TC	MAKECADR
 			COSCDUZ
 		DMP	SL1		# RESCALE
 			COSCDUX
-		STCALL	COSTH		# (COSTH = 16D IN PD)
+		STCALL	COSTH		# (COSTH= 16D IN PD)
 			ARCTAN
 		PDDL	DMP		# ROLL = ARCTAN(SZ/CZCX) INTO 2 PD
 			SINCDUZ
@@ -327,15 +320,15 @@ BALLANGS	TC	MAKECADR
 			COSCDUX
 		DMP	SL1		# CXCY
 			COSCDUY
-		DSU	STADR		# PULL UP FORM 6 PD
+		DSU	STADR		# PULL UP FROM 6 PD
 		STODL	COSTH		# COSTH = CXCY - SXSZSY
 			SINCDUY
 		DMP	SL1
 			COSCDUX		# CXSY
-		DAD	STADR		# PULL UP FORM 4 PD
+		DAD	STADR		# PULL UP FROM 4 PD
 		STCALL	SINTH		# SINTH = CXSY + SXSZCY
 			ARCTAN		# RETURNS WITH D(MPAC) = PITCH
-		PDDL	VDEF		# PITCH INTO 2 PD, ROLL INTO MPAC FROM 2 PD
+		PDDL	VDEF		# PITCH INTO 2 PD, ROLL INTO MPAC FROM 2PD
 		RTB			# VDEF MAKES V(MPAC) = ROLL, PITCH, YAW
 			V1STO2S
 		STORE	FDAIX		# MODE IS TP
@@ -347,53 +340,51 @@ ENDBALL		CA	BALLEXIT
 		TC	BANKJUMP
 
 # Page 480
-# PROGRAM DESCRIPTION -- VECPOINT
+# PROGRAM DESCRIPTION - VECPOINT
 #
-# THIS INTERPRETIVE SUBROUTINE MAY BE USED TO POINT A SPACECRAFT AXIS IN A DESIRED DIRECTION.  THE AXIS
+#
+#	   THIS INTERPRETIVE SUBROUTINE MAY BE USED TO POINT A SPACECRAFT AXIS IN A DESIRED DIRECTION.  THE AXIS
 # TO BE POINTED MUST APPEAR AS A HALF UNIT DOUBLE PRECISION VECTOR IN SUCCESSIVE LOCATIONS OF ERASABLE MEMORY
 # BEGINNING WITH THE LOCATION CALLED SCAXIS.  THE COMPONENTS OF THIS VECTOR ARE GIVEN IN SPACECRAFT COORDINATES.
 # THE DIRECTION IN WHICH THIS AXIS IS TO BE POINTED MUST APPEAR AS A HALF UNIT DOUBLE PRECISION VECTOR IN
 # SUCCESSIVE LOCATIONS OF ERASABLE MEMORY BEGINNING WITH THE ADDRESS CALLED POINTVSM.  THE COMPONENTS OF THIS
-# VECTOR ARE GIVEN IN STABLE MEMBER COORDINATES.  WITH THIS INFORMTION VECPOINT COMPUTES A SET OF THREE GIMBAL
-# ANGLES (2'S COMPLEMENT) CORRESPONDING TO THE CROSS-PRODUCT ROTATION BETWEEN SCAXIS AND POINTVSM AND STORES THEM
+# VECTOR ARE GIVEN IN STABLE MEMBER COORDINATES.  WITH THIS INFORMATION VECPOINT COMPUTES A SET OF THREE GIMBAL
+# ANGLES (2S COMPLEMENT) CORESPONDING TO THE CROSS-PRODUCT ROTATION BETWE EN SCAXIS AND POINTVSM AND STORES THEM
 # IN T(MPAC) BEFORE RETURNING TO THE CALLER.
-#
-# THIS ROTATION, HOWEVER, MAY BRING THE S/C INTO GIMBAL LOCK.  WHEN POINTING A VECTOR IN THE Y-Z PLANE,
+#	   THIS ROTATION, HOWEVER, MAY BRING THE S/C INTO GIMBAL LOCK.  WHEN POINTING A VECTOR IN THE Y-Z PLANE,
 # THE TRANSPONDER AXIS, OR THE AOT FOR THE LEM, THE PROGRAM WILL CORRECT THIS PROBLEM BY ROTATING THE CROSS-
 # PRODUCT ATTITUDE ABOUT POINTVSM BY A FIXED AMOUNT SUFFICIENT TO ROTATE THE DESIRED S/C ATTITUDE OUT OF GIMBAL
-# LOCK.  IF THE AXIS TO BE POINTED IS MORE THAN 40.6 DEGREES BUT LESS THAN 60.5 DEG FROM THE +X (OR -X) AXIS,
-# THE ADDITIONAL ROTATION TO AVOID GIMBAL LOCK IS 35 DEGREES.  IF THE AXIS IS MORE THAN 60.5 DEGREES FROM +X (OR -X)
+# LOCK.  IF THE AXIS TO BE POINTED IS MORE THAN 40.6 DEGREES BUT LESS THAN 60.5 DEG FROM THE +X (OR-X) AXIS,
+# THE ADDITIONAL ROTATION TO AVOID GIMAL LOCK IS 35 DEGREES.  IF THE AXIS IS MORE THAN 60.5 DEGEES FROM +X (OR -X)
 # THE ADDITIONAL ROTATION IS 35 DEGREES.  THE GIMBAL ANGLES CORRESPONDING TO THIS ATTITUDE ARE THEN COMPUTED AND
-# STORED AS 2'S COMPLEMENT ANGLES IN T(MPAC) BEFORE RETURNING TO THE CALLER.
-#
-# WHEN POINTING THE X-AXIS, OR THE THRUST VECTOR, OR ANY VECTOR WITHIN 40.6 DEG OF THE X-AXIS, VECPOINT
+# STORED AS 2S COMPLIMENT ANGLES IN T(MPAC) BEFORE RETURNING TO THE CALLER.
+#	   WHEN POINTING THE X-AXIS, OR THE THRUST VECTOR, OR ANY VECTOR WITHIN 40.6 DEG OF THE X-AXIS, VECPOINT
 # CANNOT CORRECT FOR A CROSS-PRODUCT ROTATION INTO GIMBAL LOCK.  IN THIS CASE A PLATFORM REALIGNMENT WOULD BE
 # REQUIRED TO POINT THE VECTOR IN THE DESIRED DIRECTION.  AT PRESENT NO INDICATION IS GIVEN FOR THIS SITUATION
 # EXCEPT THAT THE FINAL MIDDLE GIMBAL ANGLE IN MPAC +2 IS GREATER THAN 59 DEGREES.
 #
-# CALLING SEQUENCE
+#	   CALLING SEQUENCE -
+#	       1) LOAD SCAXIS, POINTVSM
+#	       2) CALL
+#		       VECPOINT
 #
-#	1)	LOAD SCAXIS, POINTVSM
-#	2)	CALL
-#			VECPOINT
+#	   RETURNS WITH
 #
-# RETURNS WITH
+#	       1) DESIRED OUTER  GIMBAL ANGLE IN MPAC
+#	       2) DESIRED INNER  GIMBAL ANGLE IN MPAC +1
+#	       3) DESIRED MIDDLE GIMBAL ANGLE IN MPAC +2
 #
-#	1)	DESIRED OUTER GIMBAL ANGLE IN MPAC
-#	2)	DESIRED INNER GIMBAL ANGLE IN MPAC +1
-#	3)	DESIRED MIDDLE GIMBAL ANGLE IN MPAC +2
+#	   ERASABLES USED -
 #
-# ERASABLES USED --
+#	       1) SCAXIS	   6
+#	       2) POINTVSM	   6
+#	       3) MIS		  18
+#	       4) DEL		  18
+#	       5) COF		   6
+#	       6) VECQTEMP	   1
+#	       7) ALL OF VAC AREA 43
 #
-#	1)	SCAXIS		6
-#	2)	POINTVSM	6
-#	3)	MIS		18
-#	4)	DEL		18
-#	5)	COF		6
-#	6)	VECQTEMP	1
-#	7)	ALL OF VAC AREA	43
-#
-#			TOTAL	99
+#			TOTAL	  99
 
 		SETLOC	VECPT
 		BANK
@@ -403,7 +394,7 @@ ENDBALL		CA	BALLEXIT
 		EBANK=	BCDU
 
 VECPNT1		STQ	BOV		# THIS ENTRY USES DESIRED CDUS
-			VECQTEMP	# NOT PRESENT -- ENTER WITH CDUD'S IN MPAC
+			VECQTEMP	# NOT PRESENT-ENTER WITH CDUD'S IN MPAC
 			VECPNT2
 VECPNT2		AXC,2	GOTO
 			MIS
@@ -418,7 +409,7 @@ STORANG		STCALL	25D
 			CDUTODCM	# S/C AXES TO STABLE MEMBER AXES (MIS)
 		VLOAD	VXM
 			POINTVSM	# RESOLVE THE POINTING DIRECTION VF INTO
-			MIS		# INITIAL S/C AXES (VF = POINTVSM)
+			MIS		# INITIAL S/C AXES ( VF = POINTVSM)
 		UNIT
 		STORE	28D
 					# PD 28 29 30 31 32 33
@@ -431,12 +422,12 @@ STORANG		STCALL	25D
 		DSU	BMN		# VECTOR, IF LESS
 			DPB-14		# THAN B-14 ASSUME
 			PICKAXIS	# UNIT OPERATION
-		VLOAD	DOT		# INVALID.
+		VLOAD	DOT		#	   INVALID.
 			SCAXIS
 			28D
 		SL1	ARCCOS
 COMPMATX	CALL			# NOW COMPUTE THE TRANSFORMATION FROM
-			DELCOMP		# FINAL S/C AXES TO INITIAL S/C AXES MFI
+			DELCOMP		# FINAL S/C AXES TO INITIAL S/C AXES  MFI
 		AXC,1	AXC,2
 			MIS		# COMPUTE THE TRANSFORMATION FROM FINAL
 			KEL		# S/C AXES TO STABLE MEMBER AXES
@@ -444,34 +435,34 @@ COMPMATX	CALL			# NOW COMPUTE THE TRANSFORMATION FROM
 			MXM3		# (IN PD LIST)
 
 		DLOAD	ABS
-			6		# MFS6 = SIN(CPSI)			$2
+			6		# MFS6 = SIN(CPSI)		       $2
 		DSU	BMN
-			SINGIMLC	# = SIN(59 DEGS)			$2
-			FINDGIMB	# /CPSI/ LESS THAN 59 DEGS.
+			SINGIMLC	# = SIN(59 DEGS)		       $2
+			FINDGIMB	# /CPSI/ LESS THAN 59 DEGS
 # Page 482
-					# I.E., DESIRED ATTITUDE NOT IN GIMBAL LOCK
+					# I.E. DESIRED ATTITUDE NOT IN GIMBAL LOCK
 
 		DLOAD	ABS		# CHECK TO SEE IF WE ARE POINTING
 			SCAXIS		# THE THRUST AXIS
 		DSU	BPL
-			SINVEC1		# SIN 49.4 DEGS				$2
+			SINVEC1		# SIN 49.4 DEGS			       $2
 			FINDGIMB	# IF SO, WE ARE TRYING TO POINT IT INTO
 		VLOAD			# GIMBAL LOCK, ABORT COULD GO HERE
 		STADR
-		STOVL	MIS 	+12D
+		STOVL	MIS +12D
 		STADR			# STORE MFS (IN PD LIST) IN MIS
-		STOVL	MIS 	+6
+		STOVL	MIS +6
 		STADR
 		STOVL	MIS
-			MIS 	+6	# INNER GIMBAL AXIS IN FINAL S/C AXES
+			MIS +6		# INNER GIMBAL AXIS IN FINAL S/C AXES
 		BPL	VCOMP		# LOCATE THE IG AXIS DIRECTION CLOSEST TO
 			IGSAMEX		# FINAL X S/C AXIS
 
 IGSAMEX		VXV	BMN		# FIND THE SHORTEST WAY OF ROTATING THE
 			SCAXIS		# S/C OUT OF GIMBAL LOCK BY A ROTATION
-			U=SCAXIS	# ABOUT +- SCAXIS, I.E., IF  (IG (SGN MFS3)
+			U=SCAXIS	# ABOUT +- SCAXIS, I.E. IF (IG (SGN MFS3)
 					# X SCAXIS . XF) LESS THAN 0, U = SCAXIS
-					# OTHERWISE U = -SCAXIS.
+					# OTHERWISE U = -SCAXIS
 
 		VLOAD	VCOMP
 			SCAXIS
@@ -483,14 +474,14 @@ U=SCAXIS	VLOAD
 CHEKAXIS	DLOAD	ABS
 			SCAXIS		# SEE IF WE ARE POINTING THE AOT
 		DSU	BPL
-			SINVEC2		# SIN 29.5 DEGS				$2
+			SINVEC2		# SIN 29.5 DEGS			       $2
 			PICKANG1	# IF SO, ROTATE 50 DEGS ABOUT +- SCAXIS
 		DLOAD	GOTO		# IF NOT, MUST BE POINTING THE TRANSPONDER
 			VECANG2		# OR SOME VECTOR IN THE Y, OR Z PLANE
 			COMPMFSN	# IN THIS CASE ROTATE 35 DEGS TO GET OUT
 					# OF GIMBAL LOCK (VECANG2  $360)
 PICKANG1	DLOAD
-			VECANG1		# = 50 DEGS.				$360
+			VECANG1		# = 50 DEGS			     $ 360
 COMPMFSN	CALL
 			DELCOMP		# COMPUTE THE ROTATION ABOUT SCAXIS TO
 		AXC,1	AXC,2		# BRING MFS OUT OF GIMBAL LOCK
@@ -505,12 +496,12 @@ FINDGIMB	AXC,1	CALL
 			0		# EXTRACT THE COMMANDED CDU ANGLES FROM
 			DCMTOCDU	# THIS MATRIX
 		RTB	SETPD
-			V1STO2S		# CONVERT TO 2'S COMPLEMENT
+			V1STO2S		# CONVERT TO 2:S COMPLEMENT
 			0
 		GOTO
 			VECQTEMP	# RETURN TO CALLER
 
-PICKAXIS	VLOAD	DOT		# IF VF X VI = 0, FIND VF, VI
+PICKAXIS	VLOAD	DOT		# IF VF X VI = 0,  FIND VF . VI
 			28D
 			SCAXIS
 		BMN	TLOAD
@@ -523,11 +514,11 @@ PICKAXIS	VLOAD	DOT		# IF VF X VI = 0, FIND VF, VI
 		SETLOC	MANUVER1
 		BANK
 ROT180		VLOAD	VXV		# IF VF, VI ANTIPARALLEL, 180 DEG ROTATION
-			MIS 	+6	# IS REQUIRED.  Y STABLE MEMBER AXIS IN
+			MIS 	+6	# IS REQUIRED. Y STABLE MEMBER AXIS IN
 			HIDPHALF	# INITIAL S/C AXES.
 		UNIT	VXV		# FIND Y(SM) X X(I)
 			SCAXIS		# FIND UNIT(VI X UNIT(Y(SM) X X(I)))
-		UNIT	BOV		# I.E., PICK A VECTOR IN THE PLANE OF X(I),
+		UNIT	BOV		# I.E. PICK A VECTOR IN THE PLANE OF X(I),
 			PICKX		# Y(SM) PERPENDICULAR TO VI
 		STODL	COF
 			36D		# CHECK MAGNITUDE
@@ -543,17 +534,17 @@ XROT		STODL	COF
 PICKX		VLOAD	GOTO		# PICK THE XAXIS IN THIS CASE
 			HIDPHALF
 			XROT
-SINGIMLC	2DEC	.4285836003	# = SIN(59)				$2
+SINGIMLC	2DEC	.4285836003	# =SIN(59)		  $2
 
-SINVEC1		2DEC	.3796356537	# = SIN(49.4)				$2
+SINVEC1		2DEC	.3796356537	# =SIN(49.4)		  $2
 
-SINVEC2		2DEC	.2462117800	# = SIN(29.5)				$2
+SINVEC2		2DEC	.2462117800	# =SIN(29.5)		  $2
 
-VECANG1		2DEC	.1388888889	# = 50 DEGREES				$360
+VECANG1		2DEC	.1388888889	# = 50 DEGREES			      $360
 # Page 484
-VECANG2		2DEC	.09722222222	# = 35 DEGREES				$360
+VECANG2		2DEC	.09722222222	# = 35 DEGREES			      $360
 
-1BITDP		OCT	0		# KEEP THIS BEFORE DPB(-14)	************
+1BITDP		OCT	0		# KEEP THIS BEFORE DPB(-14)	 *********
 DPB-14		OCT	00001
 		OCT	00000
 
@@ -577,11 +568,10 @@ R62FLASH	CAF	V06N22		# FLASH V06N22 AND
 		TCF	R62FLASH	# ENTER
 
 					# ASTRONAUT MAY LOAD NEW ICDUS AT THIS
-					# POINT.
+					# POINT
 GOMOVE		TC	UPFLAG		# SET FOR 3-AXIS MANEUVER
 		ADRES	3AXISFLG
 
 		TC	BANKCALL
 		CADR	R60LEM
 		TCF	ENDEXT		# END R62
-

Luminary099/RADAR_LEADIN_ROUTINES.agc

@@ -83,12 +83,12 @@ DORSAMP2	INHINT
 		CA	RTSTLOC
 		AD	TWO		# STORAGE IS DP
 		TS	RTSTLOC
-		TCF	ENDOFJOB	# CONTINUOUS SAMPLING AND 2N TRIES -- GONE.
+		TCF	ENDOFJOB	# CONTINUOUS SAMPLING AND 2N TRIES - GONE.
 
 # VARIABLE RADAR DATA CALLER FOR ONE MEASUREMENT ONLY.
 
 VARADAR		CAF	ONE		# WILL BE SENT TO RADAR ROUTINE IN A BY
-		TS	BUF2		# SWCALL
+		TS	BUF2		# SWCALL.
 		INDEX	RTSTDEX
 		CAF	RDRLOCS
 		TCF	SWCALL		# NOT TOUCHING Q.

Luminary099/RCS_FAILURE_MONITOR.agc

@@ -25,25 +25,25 @@
 #	16:27 JULY 14, 1969
 
 # Page 190
-# PROGRAM DESCRIPTION:
+# PROGRAM DESCRIPTION
 #
-# AUTHOR: J. S. MILLER
+# AUTHOR:  J S MILLER
 #
-# MODIFIED 6 MARCH 1968 BY P. S. WEISSMAN TO SET UP JOB FOR 1/ACCS WHEN THE MASKS ARE CHANGED.
+# MODIFIED 6 MARCH 1968 BY P S WEISSMAN TO SET UP JOB FOR 1/ACCS WHEN THE MASKS ARE CHANGED.
 #
-# THIS ROUTINE IS ATTACHED TO T4RUPT, AND IS ENTERED EVERY 480 MS.  ITS FUNCTION IS TO EXAMINE THE LOW 8 BITS
+#      THIS ROUTINE IS ATTACHED TO T4RUPT, AND IS ENTERED EVERY 480 MS.  ITS FUNCTION IS TO EXAMINE THE LOW 8 BITS
 # OF CHANNEL 32 TO SEE IF ANY ISOLATION-VALVE CLOSURE BITS HAVE APPEARED OR DISAPPEARED (THE CREW IS WARNED OF JET
 # FAILURES BY LAMPS LIT BY THE GRUMMAN FAILURE-DETECTION CIRCUITRY; THEY MAY RESPOND BY OPERATING SWITCHES WHICH
 # ISOLATE PAIRS OF JETS FROM THE PROPELLANT TANKS AND SET BITS IN CHANNEL 32).  IN THE EVENT THAT CHANNEL 32 BITS
-# DIFFER FROM `PVALVEST', THE RECORD OF ACTIONS TAKEN BY THIS ROUTINE, THE APPROPRIATE BITS IN `CH5MASK' &
-# `CH6MASK', USED BY THE DAP JET-SELECTION LOGIC, ARE UPDATED, AS IS `PVALVEST'.  TO SPEED UP & SHORTEN THE
+# DIFFER FROM 'PVALVEST', THE RECORD OF ACTIONS TAKEN BY THIS ROUTINE, THE APPROPRIATE BITS IN 'CH5MASK' &
+# 'CH6MASK', USED BY THE DAP JET-SELECTION LOGIC, ARE UPDATED, AS IS 'PVALVEST'.  TO SPEED UP & SHORTEN THE
 # ROUTINE, NO MORE THAN ONE CHANGE IS ACCEPTED PER ENTRY.  THE HIGHEST-NUMBERED BIT IN CHANNEL 32 WHICH REQUIRES
 # ACTION IS THE ONE PROCESSED.
 #
-# THE CODING IN THE FAILURE MONITOR HAS BEEN WRITTEN SO AS TO HAVE ALMOST COMPLETE RESTART PROTECTION.  FOR
-# EXAMPLE, NO ASSUMPTION IS MADE WHEN SETTING A `CH5MASK' BIT TO 1 THAT THE PREVIOUS STATE IS 0, ALTHOUGH IT OF
+#      THE CODING IN THE FAILURE MONITOR HAS BEEN WRITTEN SO AS TO HAVE ALMOST COMPLETE RESTART PROTECTION.  FOR
+# EXAMPLE, NO ASSUMPTION IS MADE WHEN SETTING A 'CH5MASK' BIT TO 1 THAT THE PREVIOUS STATE IS 0, ALTHOUGH IT OF
 # COURSE SHOULD BE.  ONE CASE WHICH MAY BE SEEN TO EVADE PROTECTION IS THE OCCURRENCE OF A RESTART AFTER UPDATING
-# ONE OR BOTH DAP MASK-WORDS BUT BEFORE UPDATING `PVALVEST', COUPLED WITH A CHANGE IN THE VALVE-BIT BACK TO ITS
+# ONE OR BOTH DAP MASK-WORDS BUT BEFORE UPDATING 'PVALVEST', COUPLED WITH A CHANGE IN THE VALVE-BIT BACK TO ITS
 # FORMER STATE.  THE CONSEQUENCE OF THIS IS THAT THE NEXT ENTRY WOULD NOT SEE THE CHANGE INCOMPLETELY INCORP-
 # ORATED BY THE LAST PASS (BECAUSE IT WENT AWAY AT JUST THE RIGHT TIME), BUT THE DAP MASK-WORDS WILL BE INCORRECT.
 # THIS COMBINATION OF EVENTS SEEMS QUITE REMOTE, BUT NOT IMPOSSIBLE UNLESS THE CREW OPERATES THE SWITCHES AT HALF-
@@ -52,22 +52,21 @@
 #
 # CALLING SEQUENCE:
 #
-#	TCF	RCSMONIT		# (IN INTERRUPT MODE, EVERY 480 MS.)
+#		TCF	RCSMONIT	(IN INTERRUPT MODE, EVERY 480 MS.)
 #
-# EXIT: TCF RCSMONEX (ALL PATHS EXIT VIA SUCH AN INSTRUCTION)
-
+# EXIT:  TCF  RCSMONEX  (ALL PATHS EXIT VIA SUCH AN INSTRUCTION)
 RCSMONEX	EQUALS	RESUME
 
 # ERASABLE INITIALIZATION REQUIRED:
 #
-# 	VIA FRESH START:	PVALVEST	=	+0	(ALL JETS ENABLED)
-#				CH5MASK,CH6MASK	=	+0	(ALL JETS OK)
+#	   VIA FRESH START:  PVALVEST	       = +0  (ALL JETS ENABLED)
+#			     CH5MASK, CH6MASK  = +0  (ALL JETS OK)
 #
-# OUTPUT:	CH5MASK & CH6MASK UPDATED (1'S WHERE JETS NOT TO BE USED, IN CHANNEL 5 & 6 FORMAT)
-#		PVALTEST UPDATED (1'S WHEN VALVE CLOSURES HAVE BEEN TRANSLATED INTO CH5MASK & CH6MASK; CHAN 32 FORMAT)
-#		JOB TO DO 1/ACCS.
+# OUTPUT:  CH5MASK & CH6MASK UPDATED  (1'S WHERE JETS NOT TO BE USED, IN CHANNEL 5 & 6 FORMAT)
+#	   PVALTEST UPDATED  (1.5 WHEN VALVE CLOSURES HAVE BEEN TRANSLATED INTO CH5MASK & CH6MASK; CHAN 32 FORMAT)
+#	   JOB TO DO 1/ACCS.
 #
-# DEBRIS:  A, L, AND Q AND DEBRIS OF NOVAC.
+# DEBRIS:  A, L, Q AND DEBRIS OF NOVAC.
 #
 # SUBROUTINE CALLED:  NOVAC.
 
@@ -83,91 +82,92 @@ RCSMONIT	EQUALS	RCSMON
 
 RCSMON		CS	ZERO
 		EXTEND
-		RXOR	CHAN32			# PICK UP + INVERT INVERTED CHANNEL 32.
-		MASK	LOW8			# KEEP JET-FAIL BITS ONLY.
+		RXOR	CHAN32		# PICK UP + INVERT INVERTED CHANNEL 32.
+		MASK	LOW8		# KEEP JET-FAIL BITS ONLY.
 		TS	Q
 
-		CS	PVALVEST		#       _   _
-		MASK	Q			# FORM PC + PC.
-		TS	L			# 	(P = PREVIOUS ISOLATION VALVE STATE,
-		CS	Q			#	 C = CURRENT VALVE STATE (CH32)).
+		CS	PVALVEST	#       -   -
+		MASK	Q		# FORM PC + PC.
+		TS	L		#   (P = PREVIOUS ISOLATION VALVE STATE,
+		CS	Q		#    C = CURRENT VALVE STATE (CH 32)).
 		MASK	PVALVEST
-		ADS	L			# RESULT NZ INDICATES ACTION REQUIRED.
+		ADS	L		# RESULT NZ INDICATES ACTION REQUIRED.
 
 		EXTEND
-		BZF	RCSMONEX		# QUIT IF NO ACTION REQUIRED.
+		BZF	RCSMONEX	# QUIT IF NO ACTION REQUIRED.
 
 		EXTEND
-		MP	BIT7			# MOVE BITS 8-1 OF A TO 14-7 OF L.
-		XCH	L			# ZERO TO L IN THE PROCESS.
+		MP	BIT7		# MOVE BITS 8 - 1 OF A TO 14 - 7 OF L.
+		XCH	L		# ZERO TO L IN THE PROCESS.
 
  -3		INCR	L
- 		DOUBLE				# BOUND TO GET OVERFLOW IN THIS LOOP,
-		OVSK				# SINCE WE ASSURED INITIAL NZ IN A.
+		DOUBLE			# BOUND TO GET OVERFLOW IN THIS LOOP.
+		OVSK			# SINCE WE ASSURED INITIAL NZ IN A.
 		TCF	-3
 
 		INDEX	L
-		CA	BIT8 -1			# SAVE THE RELEVANT BIT (8-1).
+		CA	BIT8 -1		# SAVE THE RELEVANT BIT (8 - 1).
 		TS	Q
-		MASK	PVALVEST		# LOOK AT PREVIOUS VALVE STATE BIT.
+		MASK	PVALVEST	# LOOK AT PREVIOUS VALVE STATE BIT.
 		CCS	A
-		TCF	VOPENED			# THE VALVE HAS JUST BEEN OPENED.
+		TCF	VOPENED		# THE VALVE HAS JUST BEEN OPENED.
 
-		CS	CH5MASK			# THE VALVE HAS JUST BEEN CLOSED.
+		CS	CH5MASK		# THE VALVE HAS JUST BEEN CLOSED.
 		INDEX	L
 		MASK	5FAILTAB
-		ADS	CH5MASK			# SET INHIBIT BIT FOR CHANNEL 5 JET.
+		ADS	CH5MASK		# SET INHIBIT BIT FOR CHANNEL 5 JET.
 
 		CS	CH6MASK
 		INDEX	L
 		MASK	6FAILTAB
-		ADS	CH6MASK			# SET INGIBIT BIT FOR CHANNEL 6 JET
+		ADS	CH6MASK		# SET INGIBIT BIT FOR CHANNEL 6 JET.
 
 		CA	Q
-		ADS	PVALVEST		# RECORD ACTION TAKEN.
+		ADS	PVALVEST	# RECORD ACTION TAKEN.
 
-		TCF	1/ACCFIX		# SET UP 1/ACCJOB AND EXIT.
+		TCF	1/ACCFIX	# SET UP 1/ACCJOB AND EXIT.
 
 # Page 192
-VOPENED		INDEX	L			# A VALVE HAS JUST BEEN OPENED.
+VOPENED		INDEX	L		# A VALVE HAS JUST BEEN OPENED.
 		CS	5FAILTAB
 		MASK	CH5MASK
-		TS	CH5MASK			# REMOVE INHIBIT BIT FOR CHANNEL 5 JET.
+		TS	CH5MASK		# REMOVE INHIBIT BIT FOR CHANNEL 5 JET.
 
 		INDEX	L
 		CS	6FAILTAB
 		MASK	CH6MASK
-		TS	CH6MASK			# REMOVE INHIBIT BIT FOR CHANNEL 6 JET.
+		TS	CH6MASK		# REMOVE INHIBIT BIT FOR CHANNEL 6 JET.
 
 		CS	Q
 		MASK	PVALVEST
-		TS	PVALVEST		# RECORD ACTION TAKEN.
+		TS	PVALVEST	# RECORD ACTION TAKEN.
 
-1/ACCFIX	CAF	PRIO27			# SET UP 1/ACCS SO THAT THE SWITCH CURVES
-		TC	NOVAC			#	FOR TJETLAW CAN BE MODIFIED IF CH5MASK
-		EBANK=	AOSQ			#	HAS BEEN ALTERED.
+1/ACCFIX	CAF	PRIO27		# SET UP 1/ACCS SO THAT THE SWITCH CURVES
+		TC	NOVAC		#   FOR TJETLAW CAN BE MODIFIED IF CH5MASK
+		EBANK=	AOSQ		#   HAS BEEN ALTERED.
 		2CADR	1/ACCJOB
 
-		TCF	RCSMONEX		# EXIT.
-
-5FAILTAB	EQUALS	-1			# CH 5 JET BIT CORRESPONDING TO CH 32 BIT:
-		OCT	00040			# 8
-		OCT	00020			# 7
-		OCT	00100			# 6
-		OCT	00200			# 5
-		OCT	00010			# 4
-		OCT	00001			# 3
-		OCT	00004			# 2
-		OCT	00002			# 1
-
-6FAILTAB	EQUALS	-1			# CH 6 JET BIT CORRESPONDING TO CH 32 BIT:
-		OCT	00010			# 8
-		OCT	00020			# 7
-		OCT	00004			# 6
-		OCT	00200			# 5
-		OCT	00001			# 4
-		OCT	00002			# 3
-		OCT	00040			# 2
-		OCT	00100			# 1
+		TCF	RCSMONEX	# EXIT.
+
+
+5FAILTAB	EQUALS	-1		# CH 5 JET BIT CORRESPONDING TO CH 32 BIT:
+		OCT	00040		# 8
+		OCT	00020		# 7
+		OCT	00100		# 6
+		OCT	00200		# 5
+		OCT	00010		# 4
+		OCT	00001		# 3
+		OCT	00004		# 2
+		OCT	00002		# 1
+
+6FAILTAB	EQUALS	-1		# CH 6 JET BIT CORRESPONDING TO CH 32 BIT:
+		OCT	00010		# 8
+		OCT	00020		# 7
+		OCT	00004		# 6
+		OCT	00200		# 5
+		OCT	00001		# 4
+		OCT	00002		# 3
+		OCT	00040		# 2
+		OCT	00100		# 1
 
 

Luminary099/README.md

@@ -67,7 +67,7 @@ What follows is simply a bunch of file-includes for the individual code chunks.
 | [P20-P25.agc]                                 | 492-614     |
 | [P30_P37.agc]                                 | 615-617     |
 | [P32-P35_P72-P75.agc]                         | 618-650     |
-| [LAMBERT_AIMPOINT_GUIDANCE.agc]               | 651-653     |
+| [GENERAL_LAMBERT_AIMPOINT_GUIDANCE.agc]       | 651-653     |
 | [GROUND_TRACKING_DETERMINATION_PROGRAM.agc]   | 654-657     |
 | [P34-35_P74-75.agc]                           | 658-702     |
 | [R31.agc]                                     | 703-708     |
@@ -164,7 +164,7 @@ What follows is simply a bunch of file-includes for the individual code chunks.
 [P20-P25.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/P20-P25.agc
 [P30_P37.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/P30_P37.agc
 [P32-P35_P72-P75.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/P32-P35_P72-P75.agc
-[LAMBERT_AIMPOINT_GUIDANCE.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/LAMBERT_AIMPOINT_GUIDANCE.agc
+[GENERAL_LAMBERT_AIMPOINT_GUIDANCE.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/GENERAL_LAMBERT_AIMPOINT_GUIDANCE.agc
 [GROUND_TRACKING_DETERMINATION_PROGRAM.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/GROUND_TRACKING_DETERMINATION_PROGRAM.agc
 [P34-35_P74-75.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/P34-35_P74-75.agc
 [R31.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Luminary099/R31.agc

Luminary099/RESTART_TABLES.agc

@@ -28,56 +28,57 @@
 
 # Page 238
 # RESTART TABLES
-# --------------
+# ------------------
 #
 # THERE ARE TWO FORMS OF RESTART TABLES FOR EACH GROUP.  THEY ARE KNOWN AS THE EVEN RESTART TABLES AND THE ODD
 # RESTART TABLES.  THE ODD TABLES HAVE ONLY ONE ENTRY OF THREE LOCATIONS WHILE THE EVEN TABLES HAVE TWO ENTRIES
-# EACH USING THREE LOCATIONS.  THE INFORMATION AS TO WHETHER IT IS A JOB, WAITLIST, OR A LONGCALL IS GIVEN BY THE
-# WAY THINGS ARE PUT IN TO THE TABLES.
-#
-# A JOB HAS ITS PRIORITY STORED IN A PRDTTAB OF THE CORRECT PHASE SPOT -- A POSITIVE PRIORITY INDICATES A
+# EACH USING THREE LOCATIONS. THE INFORMATION AS TO WHETHER IT IS A JOB, WAITLIST, OR A LONGCALL IS GIVEN BY THE
+# WAY THINGS ARE PUT INTO THE TABLES.
+#      A JOB HAS ITS PRIORITY STORED IN PRDTTAB OF THE CORRECT PHASE SPOT - A POSITIVE PRIORITY INDICATES A
 # FINDVAC JOB, A NEGATIVE PRIORITY A NOVAC.  THE 2CADR OF THE JOB IS STORED IN THE CADRTAB.
 # FOR EXAMPLE,
 #
-#		5.7SPOT		OCT	23000
-#				2CADR	SOMEJOB
+# 5.7SPOT	OCT	23000
+#		2CADR	SOMEJOB
 #
 # A RESTART OF GROUP 5 WITH PHASE SEVEN WOULD THEN CAUSE SOMEJOB TO BE RESTARTED AS A FINDVAC WITH PRIORITY 23.
 #
-#		5.5SPOT		OCT	-23000
-#				2CADR	ANYJOB
+# 5.5SPOT	OCT	-23000
+#		2CADR	ANYJOB
 #
 # HERE A RESTART OF GROUP 5 WITH PHASE 7 WOULD CAUSE ANYJOB TO BE RESTARTED AS A NOVAC WITH PRIORITY 23.
 # A LONGCALL HAS ITS GENADR OF ITS 2CADR STORED NEGATIVELY AND ITS BBCON STORED POSITIVELY.  IN ITS PRDTTAB IS
 # PLACED THE LOCATION OF A DP REGISTER THAT CONTAINS THE DELTA TIME THAT LONGCALL HAD BEEN ORIGINALLY STARTED
 # WITH.  EXAMPLE,
 #
-#		3.6SPOT		GENADR	DELTAT
-#				-GENADR	LONGTASK
-#				BBCON	LONGTASK
-#				OCT	31000
-#				2CADR	JOBAGAIN
+# 3.6SPOT	GENADR	DELTAT
+#	       -GENADR	LONGTASK
+#		BBCON	LONGTASK
 #
-# THIS WOULD START UP LONGTASK AT THE APPROPRIATE TIME, OR IMMEDIATELY IF THE TIME HAD ALREADY PASSED.  IT SHOULD
-# BE NOTED THAT IF DELTAT IS IN A SWITCHED E BANK, THIS INFORMATION SHOULD BE IN THE BBCON OF THE 2CADR OF THE
-# TASK.  FROM ABOVE, WE SEE THAT THE SECOND PART O THIS PHASE WOULD BE STARTED AS A JOB WITH A PRIORITY OF 31.
+#		OCT	31000
+#		2CADR	JOBAGAIN
 #
-# WAITLIST CALLS ARE IDENTIFIED BY THE FCT THAT THEIR 2CADR IS STORED NEGATIVELY.  IF PRDTTAB OF THE PHASE SPOT
+# THIS WOULD START UP LONGTASK AT THE APPROPRIATE TIME, OR IMMEDIATELY IF THE TIME HAD ALREADY PASSED. IT SHOULD
+# BE NOTED THAT IF DELTAT IS IN A SWITCHED E BANK, THIS INFORMATOIN SHOULD BE IN THE BBCON OFTHE 2CADR OF THE
+# TASK.  FROM ABOVE, WE SEE THAT THE SECOND PART OF THIS PHASE WOULD BE STARTED AS A JOB WITH A PRIORITY OF 31.
+#
+# WAITLIST CALLS ARE IDENTIFIED BY THE FACT THAT THEIR 2CADR IS STORED NEGATIVELY. IF PRDTTAB OF THE PHASE SPOT
 # IS POSITIVE, THEN IT CONTAINS THE DELTA TIME, IF PRDTTAB IS NEGATIVE THEN IT IS THE -GENADR OF AN ERASABLE
+# LOCATION CONTAINING THE DELTA TIME, THAT IS, THE TIME IS STORED INDIRECTLY.  IT SHOULD BE NOTED AS ABOVE, THAT
 # IF THE TIME IS STORED INDIRECTLY, THE BBCON MUST CONTAIN THE NECESSARY E BANK INFORMATION IF APPLICABLE.  WITH
 # WAITLIST WE HAVE ONE FURTHER OPTION, IF -0 IS STORED IN PRDTTAB, IT WILL CAUSE AN IMMEDIATE RESTART OF THE
 # TASK.  EXAMPLES,
 #
-#				OCT	77777		# THIS WILL CAUSE AN IMMEDIATE RESTART
-#				-2CADR	ATASK		# OF THE TASK :ATASK:
+#		OCT	77777		# THIS WILL CAUSE AN IMMEDIATE RESTART
+#	       -2CADR	ATASK		# OF THE TASK :ATASK:
 #
-#				DEC	200		# IF THE TIME OF THE 2 SECONDS SINCE DUMMY
-#				-2CADR	DUMMY		# WAS PUT ON THE WAITLIST IS UP, IT WILL BEGIN
-#							# IN 10 MS, OTHERWISE IT WILL BEGIN WHEN
-#							# IT NORMALLY WOULD HAVE BEGUN.
+#		DEC	200		# IF THE TIME OF THE 2 SECONDS SINCE DUMMY
+#	       -2CADR	DUMMY		# WAS PUT ON THE WAITLIST IS UP, IT WILL BEGIN
+#					# IN 10 MS, OTHERWISE IT WILL BEGIN WHEN
+#					# IT NORMALLY WOULD HAVE BEGUN.
 # Page 239
-#				-GENADR	DTIME		# WHERE DTIME CONTAINS THE DELTA TIME
-#				-2CADR	TASKTASK	# OTHERWISE THIS IS AS ABOVE
+#	       -GENADR	DTIME		# WHERE DTIME CONTAINS THE DELTA TIME
+#	       -2CADR	TASKTASK	# OTHERWISE THIS IS AS ABOVE
 #
 # ***** NOW THE TABLES THEMSELVES *****
 
@@ -85,11 +86,11 @@
 		SETLOC	RESTART
 		BANK
 
-PRDTTAB		EQUALS	12000			# USED TO FIND THE PRIORITY OR DELTATIME
-CADRTAB		EQUALS	12001			# THIS AND THE NEXT RELATIVE LOC CONTAIN
-						# RESTART 2CADR
+PRDTTAB		EQUALS	12000		# USED TO FIND THE PRIORITY OR DELTATIME
+CADRTAB		EQUALS	12001		# THIS AND THE NEXT RELATIVE LOC CONTAIN
+					# RESTART 2CADR
 
-		COUNT*	$$/RSTAB		# TABLES IN BANK 1.
+		COUNT*	$$/RSTAB	# TABLES IN BANK 1.
 SIZETAB		TC	1.2SPOT -12006
 		TC	1.3SPOT -12004
 		TC	2.2SPOT -12006
@@ -102,29 +103,27 @@ SIZETAB		TC	1.2SPOT -12006
 		TC	5.3SPOT -12004
 		TC	6.2SPOT -12006
 		TC	6.3SPOT -12004
-1.2SPOT		OCT	21000			# A DUMMY EXAMPLE TO BE REPLACED AS SOON
+1.2SPOT		OCT	21000		# A DUMMY EXAMPLE TO BE REPLACED AS SOON
 		EBANK=	STATE
-		2CADR	ENDOFJOB		# AS THERE IS A LEGITIMATE 1.2SPOT
+		2CADR	ENDOFJOB	# AS THERE IS A LEGITIMATE 1.2SPOT
 
 		DEC	100
 		EBANK=	STATE
 		2CADR	TASKOVER
 
-# ANY MORE GROUP 1.EVEN RESTART VALUES SHOULD GO HERE.
+# ANY MORE GROUP 1.EVEN RESTART VALUES SHOULD GO HERE
 
-1.3SPOT		-GENADR	SAVET-30
+1.3SPOT	       -GENADR	SAVET-30
 		EBANK=	DVCNTR
-		-2CADR	ULLGTASK
+	       -2CADR	ULLGTASK
 
-# ANY MORE GROUP 1.ODD RESTART VALUES SHOULD GO HERE.
+# ANY MORE GROUP 1.ODD RESTART VALUES SHOULD GO HERE
 
 2.2SPOT		EQUALS	1.2SPOT
-
 # ANY MORE GROUP 2.EVEN RESTART VALUES SHOULD GO HERE
 
 2.3SPOT		GENADR	600SECS
-
-		-GENADR	STATEINT
+	       -GENADR	STATEINT
 		EBANK=	RRECTCSM
 		BBCON	STATEINT
 
@@ -135,7 +134,7 @@ SIZETAB		TC	1.2SPOT -12006
 
 2.7SPOT		DEC	1500
 		EBANK=	LOSCOUNT
-		-2CADR	P20LEMC1
+	       -2CADR	P20LEMC1
 
 2.11SPOT	OCT	14000
 		EBANK=	P21TIME
@@ -151,21 +150,20 @@ SIZETAB		TC	1.2SPOT -12006
 
 2.17SPOT	OCT	77777
 		EBANK=	VGPREV
-		-2CADR	REDO2.17
+	       -2CADR	REDO2.17
 
 2.21SPOT	DEC	25
 		EBANK=	DVCNTR
-		-2CADR	R10,R11
+	       -2CADR	R10,R11
 
 # ANY MORE GROUP 2.ODD RESTART VALUES SHOULD GO HERE.
 
 3.2SPOT		EQUALS	1.2SPOT
-
 # ANY MORE GROUP 3.EVEN RESTART VALUES SHOULD GO HERE
 
-3.3SPOT		-GENADR	ZOOMTIME
+3.3SPOT	       -GENADR	ZOOMTIME
 		EBANK=	DVCNTR
-		-2CADR	ZOOM
+	       -2CADR	ZOOM
 
 3.5SPOT		OCT	20000
 		EBANK=	TTOGO
@@ -175,13 +173,12 @@ SIZETAB		TC	1.2SPOT -12006
 
 4.2SPOT		DEC	2500
 		EBANK=	TTOGO
-
-		-2CADR	TIG-5
+	       -2CADR	TIG-5
 
 		OCT	77777
 		EBANK=	TTOGO
 # Page 241
-		-2CADR	REDO4.2
+	       -2CADR	REDO4.2
 
 # ANY MORE GROUP 4.EVEN RESTART VALUES SHOULD GO HERE
 
@@ -191,15 +188,15 @@ SIZETAB		TC	1.2SPOT -12006
 
 4.5SPOT		DEC	50
 		EBANK=	TTOGO
-		-2CADR	ULLAGOFF
+	       -2CADR	ULLAGOFF
 
 4.7SPOT		DEC	500
 		EBANK=	DVCNTR
-		-2CADR	TIG-0
+	       -2CADR	TIG-0
 
-4.11SPOT	-GENADR	TGO +1
+4.11SPOT       -GENADR	TGO +1
 		EBANK=	DVCNTR
-		-2CADR	ENGOFTSK
+	       -2CADR	ENGOFTSK
 
 4.13SPOT	OCT	12000
 		EBANK=	TRKMKCNT
@@ -207,11 +204,11 @@ SIZETAB		TC	1.2SPOT -12006
 
 4.15SPOT	DEC	500
 		EBANK=	TTOGO
-		-2CADR	TIG-30
+	       -2CADR	TIG-30
 
 4.17SPOT	OCT	77777
 		EBANK=	DVCNTR
-		-2CADR	TIG-5
+	       -2CADR	TIG-5
 
 4.21SPOT	OCT	13000
 		EBANK=	STAR
@@ -219,17 +216,17 @@ SIZETAB		TC	1.2SPOT -12006
 
 4.23SPOT	OCT	77777
 		EBANK=	DVCNTR
-		-2CADR	IGNITION
+	       -2CADR	IGNITION
 
 4.25SPOT	GENADR	SAVET-30
-		-GENADR	TIG-35
+	       -GENADR	TIG-35
 		EBANK=	SAVET-30
 		BBCON	TIG-35
 
-
 4.27SPOT	OCT	52777
 		EBANK=	DVCNTR
 		2CADR	P70A
+
 # Page 242
 4.31SPOT	OCT	52777
 		EBANK=	DVCNTR
@@ -248,17 +245,18 @@ SIZETAB		TC	1.2SPOT -12006
 		2CADR	COMFAIL
 
 # ANY MORE 4.ODD RESTART VALUES SHOULD GO HERE.
+
 5.2SPOT		OCT	22000
 		EBANK=	DVCNTR
 		2CADR	NORMLIZE
 
 		DEC	200
 		EBANK=	DVCNTR
-		-2CADR	REREADAC
+	       -2CADR	REREADAC
 
 5.4SPOT		DEC	200
 		EBANK=	DVCNTR
-		-2CADR	REREADAC
+	       -2CADR	REREADAC
 
 		OCT	20000
 		EBANK=	DVCNTR
@@ -268,30 +266,28 @@ SIZETAB		TC	1.2SPOT -12006
 
 5.3SPOT		DEC	200
 		EBANK=	DVCNTR
-		-2CADR	REREADAC
+	       -2CADR	REREADAC
 
 5.5SPOT		OCT	77777
 		EBANK=	DVCNTR
-		-2CADR	REDO5.5
+	       -2CADR	REDO5.5
 
 5.7SPOT		OCT	77777
 		EBANK=	DVCNTR
 # Page 243
-		-2CADR	BIBIBIAS
+	       -2CADR	BIBIBIAS
 
 # ANY MORE GROUP 5.ODD RESTART VALUES SHOULD GO HERE
 
 6.2SPOT		EQUALS	1.2SPOT
 6.3SPOT		DEC	100
 		EBANK=	TIG
-		-2CADR	CLOKTASK
+	       -2CADR	CLOKTASK
 
-6.5SPOT		OCT	30000			# PROTECT INCREMENTING OF TIME2,TIME1 BY
-		EBANK=	TEPHEM			# P27(UPDATE PROGRAM) VIA V70 OR V73.
+6.5SPOT		OCT	30000		# PROTECT INCREMENTING OF TIME2,TIME1 BY
+		EBANK=	TEPHEM		# P27(UPDATE PROGRAM) VIA V70 OR V73.
 		2CADR	TIMEDIDR
 
 6.7SPOT		OCT	17000
 		EBANK=	VGPREV
 		2CADR	REDO6.7
-
-

Luminary099/TRIM_GIMBAL_CONTROL_SYSTEM.agc

@@ -43,8 +43,8 @@
 # GTS IS THE ENTRY TO THE GIMBAL TRIM SYSTEM FOR CONTROLLING ATTITUDE ERRORS AND RATES AS WELL AS ACCELERATIONS.
 
 GTS		CAF	NEGONE		# MAKE THE NEXT PASS THROUGH THE DAP BE
-		TS	COTROLER	# 	THROUGH RCS CONTROL,
-		CAF	FOUR		#	AND ENSURE THAT IT IS NOT A SKIP.
+		TS	COTROLER	#   THROUGH RCS CONTROL,
+		CAF	FOUR		#   AND ENSURE THAT IT IS NOT A SKIP.
 		TS	SKIPU
 		TS	SKIPV
 
@@ -55,27 +55,27 @@ GTS		CAF	NEGONE		# MAKE THE NEXT PASS THROUGH THE DAP BE
 
 # THE DRIVE SETTING ALGORITHM
 #
-#	DEL = SGN(OMEGA + ALPHA*ABS(ALPHA)/(2*K))
-#						    2               1/2                  2       3/2
-#	NEGUSUM = ERROR*K + ALPHA*(DEL*OMEGA + ALPHA /(3*K)) + DEL*K   (DEL*OMEGA + ALPHA /(2*K))
+# DEL = SGN(OMEGA + ALPHA*ABS(ALPHA)/(2*K))
+#					      2               1/2                  2       3/2
+# NEGUSUM = ERROR*K + ALPHA*(DEL*OMEGA + ALPHA /(3*K)) + DEL*K   (DEL*OMEGA + ALPHA /(2*K))
 #
-#	DRIVE = -SGN(NEGUSUM)
+# DRIVE = -SGN(NEGUSUM)
 
 		CA	SR		# SAVE THE SR.  SHIFT IT LEFT TO CORRECT
 		AD	A		# FOR THE RIGHT SHIFT DUE TO EDITING.
 		TS	SAVESR
 
-GTSGO+DN	CAF	TWO		# SET INDEXER FOR R-AXIS CALCULATIONS.
+GTSGO+ON	CAF	TWO		# SET INDEXER FOR R-AXIS CALCULATIONS.
 		TCF	GOQTRIMG +1
 
 GOQTRIMG	CAF	ZERO		# SET INDEXER FOR Q-AXIS CALCULATIONS
 		TS	QRCNTR
 # Page 1473
-# RSB 2009 ---------------------------------------------------------------------
+# RSB 2009 -----------------------------------------------------------------------
 # Everything between this line and the similar line below was simply filled-in
 # as-is from Luminary 131, and then verified to assemble to the proper binary
-# values.  This area is blank on the Luminary 099 print-out, as if the
-# printer ribbon had run out.
+# values.  This area is blank on the Luminary 099 print-out, as if the printer
+# ribbon had run out.
 		INDEX	QRCNTR		# AOS SCALED AT PI/2
 		CA	AOSQ
 		EXTEND
@@ -124,7 +124,7 @@ ALGORTHM	EXTEND			# Q(R)DIFF IS THETA (ERROR) SCALED AT PI.
 		EXTEND
 		DCS	A		# ALPHA(2)/2 - K
 		AD	KCENTRAL
-# RSB 2009 ---------------------------------------------------------------------
+# RSB 2009 -----------------------------------------------------------------------
 		EXTEND
 		DV	KCENTRAL	# HIGH ORDER OF QUOTIENT.
 		XCH	A2CNTRAL
@@ -133,7 +133,7 @@ ALGORTHM	EXTEND			# Q(R)DIFF IS THETA (ERROR) SCALED AT PI.
 		EXTEND
 # Page 1474
 		DV	KCENTRAL
-		XCH	A2CNTRAL +1	# QUOTIENT STORED AT 16*PI, D.P.
+		XCH	A2CNTRAL +1	# QUOTIENT STORED AT 16*PI , D.P.
 		TCF	HAVEQUOT
 
 HUGEQUOT	CA	POSMAX
@@ -191,7 +191,7 @@ NEGFNCT2	EXTEND
 
 FUNCT2		EXTEND
 		DCA	A2CNTRAL
-		DAS	K2CNTRAL	# DEL*OMEGA + ALPHA(2)/(2*K) AT 16*PI, D.P.
+		DAS	K2CNTRAL	# DEL*OMEGA + ALPHA(2)/(2*K) AT 16*PI,D.P.
 
 FUNCT3		CA	A2CNTRAL
 		EXTEND
@@ -202,7 +202,7 @@ FUNCT3		CA	A2CNTRAL
 		MP	NEG1/3
 		ADS	A2CNTRAL +1
 		TS	L
-		TCF	+2		# A2CNTRAL NOW CONTAINS -ALPHA(2)/(6*K),
+		TCF	+2		# A2CNTRAL NOW CONTAINS  -ALPHA(2)/(6*K),
 		ADS	A2CNTRAL	# SCALED AT 16*PI, IN D.P.
 
 		EXTEND
@@ -300,38 +300,38 @@ ACDT+C12	CS	NEGUQ
 #
 # TIMEGMBL COMPUTES THE DRIVE TIME NEEDED FOR THE TRIM GIMBAL TO POSITION THE DESCENT ENGINE NOZZLE SO AS TO NULL
 # THE OFFSET ANGULAR ACCELERATION ABOUT THE Q (OR R) AXIS.  INSTEAD OF USING AOSQ(R), TIMEGMBL USES .4*AOSQ(R),
-# SCALED AT PI/8.  FOR EACH AXIS, THE DRIVE TIME IS COMPUTED AS ABS(ALPHA/ACCDOT).  A ZERO
+# SCALED AT PI/8.                         FOR EACH AXIS, THE DRIVE TIME IS COMPUTED AS ABS(ALPHA/ACCDOT).  A ZERO
 # ALPHA OR ACCDOT OR A ZERO QUOTIENT TURNS OFF THE GIMBAL DRIVE IMMEDIATELY.  OTHERWISE, THE GIMBAL IS TURNED ON
-# DRIVING IN THE CORRECT DIRECTION.  THE Q(R)GIMTIMR IS SET TO TERMINATE THE DRIVE AND Q(R)ACCDOT
+# DRIVING IN THE CORRECT DIRECTION. THE Q(R)GIMTIMR IS SET TO TERMINATE THE DRIVE AND Q(R)ACCDOT
 # IS STORED TO REFLECT THE NEW ACCELERATION DERIVATIVE.  NEGUQ(R) WILL CONTAIN +1,+0,-1 FOR A Q(R)ACCDOT VALUE
 # WHICH IS NEGATIVE, ZERO, OR POSITIVE.
 #
-# INPUTS:	AOSQ,AOSR, SCALED AT P1/2, AND ACCDOTQ, ACCDOTR AT PI/2(7).	PI/2(7).
+# INPUTS:  AOSQ,AOSR, SCALED AT P1/2, AND ACCDOTQ, ACCDOTR AT PI/2(7).    PI/2(7).
 #
-# OUTPUTS:	NEW GIMBAL DRIVE BITS IN CHANNEL 12, NEGUQ, NEGUR, QACCDOT, AND RACCDOT, THE LAST SCALED AT PI/2(7).
-#		Q(R)GIMTIMR WILL BE SET TO TIME AND TERMINATE GIMBAL DRIVE(S).
+# OUTPUTS:   NEW GIMBAL DRIVE BITS IN CHANNEL 12,NEGUQ,NEGUR,QACCDOT AND RACCDOT, THE LAST SCALED AT PI/2(7).
+#	     Q(R)GIMTIMR WILL BE SET TO TIME AND TERMINATE GIMBAL DRIVE(S)
 #
-# DEBRIS:	A, L, Q, ITEMPS 2, 3, 6, AND RUPTREG2 AND ACDT+C12 DEBRIS.
+# DEBRIS:  A,L,Q, ITEMPS 2,3,6, RUPTREG2 AND ACDT+C12 DEBRIS.
 #
-# EXITS:	VIA TC Q.
+# EXITS:  VIA TC Q.
 #
-# ALARMS, ABORTS:  NONE.
+# ALARMS, ABORTS, :  NONE
 #
-# SUBROUTINES:	ACDT+C12, IBNKCALL
+# SUBROUTINES:  ACDT+C12, IBNKCALL
 #
-# WARNING:	THIS SUBROUTINE WRITES INTO CHANNEL 12 AND USES THE ITEMPS.  THEREFORE IT MAY ONLY BE CALLED WITH
-# 		INTERRUPT INHIBITED.
+# WARNING:  THIS SUBROUTINE WRITES INTO CHANNEL 12 AND USES THE ITEMPS.  THEREFORE IT MAY ONLY BE CALLED WITH
+# INTERRUPT INHIBITED.
 #
 # ERASABLE STORAGE CONFIGURATION (NEEDED BY THE INDEXING METHODS):
-#	NEGUQ		ERASE	+2		# NEGATIVE OF Q-AXIS GIMBAL DRIVE
-#	(SPWORD)	EQUALS	NEGUQ +1	# ANY S.P. ERASABLE NUMBER, NOW THRSTCMD
-#	NEGUR		EQUALS	NEGUQ +2	# NEGATIVE OF R-AXIS GIMBAL DRIVE
-#	ACCDOTQ		ERASE	+2		# Q-JERK TERM SCALED AT PI/2(7) RAD/SEC(3)
-#	(SPWORD)	EQUALS 	ACCDOTQ +1	# ANY S.P. ERASABLE NUMBER NOW QACCDOT
-#	ACCDOTR		EQUALS	ACCDOTQ +2	# R-JERK TERM SCALED AT PI/2(7) RAD/SEC(3)
-#						# ACCDOTQ, ACCDOTR ARE MAGNITUDES.
-#	AOSQ		ERASE	+4		# Q-AXIS ACC., D.P. AT PI/2 R/SEC(2)
-#	AOSR		EQUALS	AOSQ +2		# R-AXIS ACCELERATION SCALED AT PI/2 R/S2
+# NEGUQ		ERASE	+2			# NEGATIVE OF Q-AXIS GIMBAL DRIVE
+# (SPWORD)	EQUALS	NEGUQ +1		# ANY S.P. ERASABLE NUMBER, NOW THRSTCMD
+# NEGUR		EQUALS	NEGUQ +2		# NEGATIVE OF R-AXIS GIMBAL DRIVE
+# ACCDOTQ	ERASE	+2			# Q-JERK TERM SCALED AT PI/2(7) RAD/SEC(3)
+# (SPWORD)	EQUALS	ACCDOTQ +1		# ANY S.P. ERASABLE NUMBER NOW QACCDOT
+# ACCDOTR	EQUALS	ACCDOTQ +2		# R-JERK TERM SCALED AT PI/2(7) RAD/SEC(3)
+#						# ACCDOTQ,ACCDOTR ARE MAGNITUDES.
+# AOSQ		ERASE   +4			# Q-AXIS ACC., D.P. AT PI/2 R/SEC(2)
+# AOSR		EQUALS  AOSQ +2			# R-AXIS ACCELERATION SCALED AT PI/2 R/S2
 
 QRNDXER		EQUALS	ITEMP6
 OCT23146	OCTAL	23146			# DECIMAL .6
@@ -358,14 +358,14 @@ ALPHATRY	INDEX	QRNDXER
 		EXTEND
 		BZF	TGOFFNOW		# IS ALPHA ZERO?
 
-		TS	Q			# SAVE A COPY OF -AOS.
+		TS	Q			# SAVE A COPY OF  -AOS.
 		EXTEND				# NO.  RESCALE FOR TIMEGMBL USE.
 		MP	OCT23146		# OCTAL 23146 IS DECIMAL .6
-		AD	Q			# -1.6*AOS AT PI/2 = -.4*AOS AT PI/8
+		AD	Q			# -1.6*AOS AT PI/2 = -.4*AOS AT PI/8.
 		TS	L			# WAS THERE OVERFLOW?
 		TCF	SETNEGU			# NO.  COMPUTE DRIVE TIME.
 
-		CS	A			# RECOVER -SGN(AOS) IN THE A REGISTER.
+		CS	A			# RECOVER  -SGN(AOS) IN THE A REGISTER.
 		INDEX	QRNDXER			# YES.  START DRIVE WITHOUT WAITLIST.
 		XCH	NEGUQ
 		TCF	NOTALLOW		# KNOCK DOWN THE ALLOWGTS FLAG.
@@ -374,10 +374,10 @@ SETNEGU		EXTEND
 		BZMF	POSALPH
 
 		COM
-		TS	ITEMP2			# STORE -ABS(.4*AOS) SCALED AT PI/8.
+		TS	ITEMP2			# STORE  -ABS(.4*AOS) SCALED AT PI/8.
 		CS	BIT1
 		TCF	POSALPH +2
-POSALPH		TS	ITEMP2			# STORE -ABS(.4*AOS) SCALED AT PI/8.
+POSALPH		TS	ITEMP2			# STORE  -ABS(.4*AOS) SCALED AT PI/8.
 		CA	BIT1
 	+2	INDEX	QRNDXER			# SGN(AOS) INTO NEGU
 		TS	NEGUQ			# STORE SGN(ALPHA) AS NEGU
@@ -433,15 +433,15 @@ DONEYET		CCS	QRNDXER
 OCT00240	OCTAL	00240			# DECIMAL 10/1024
 
 # Page 1481
-# THE FOLLOWING SECTION IS A CONTINUATION OF THE TRIM GIMBAL CONTROL FROM THE LAST GTS ENTRY.  THE QUANTITY NEGUSUM
+# THE FOLLOWING SECTION IS A CONTINUATION OF THE TRIM GIMBAL CONTROL FROM THE LAST GTS ENTRY. THE QUANTITY NEGUSUM
 # IS COMPUTED FOR EACH AXIS (Q,R), .707*DEL*FUNCTION(3/2) + K2THETA = NEGUSUM.  NEW DRIVES ARE ENTERED TO CH 12.
 #
 # THE SUBROUTINE GTSQRT ACCEPTS A DOUBLE PRECISION VALUE IN FUNCTION, FUNCTION +1 AND RETURNS A SINGLE-PRECISION
 # SQUARE ROOT OF THE FOURTEEN MOST SIGNIFICANT BITS OF THE ARGUMENT.  ALSO, THE CELL SHFTFLAG CONTAINS A BINARY
 # EXPONENT S, SUCH THAT THE SQUARE ROOT (RETURNED IN THE A REGISTER) MUST BE SHIFTED RIGHT (MULTIPLIED BY 2 TO THE
 # POWER (-S)) IN ORDER TO BE THE TRUE SQUARE ROOT OF THE FOURTEEN MOST SIGNIFICANT BITS OF FUNCTION, FUNCTION +1.
-# SQUARE ROOT ERROR IS NOT MORE THAN 2 IN THE 14TH SIGNIFICANT BIT.  CELLS CLOBBERED ARE A, L, SHFTFLAG, ININDEX,
-# HALFARG, SCRATCH, SR, FUNCTION, FUNCTION +1.  GTSQRT IS CALLED BY TC GTSQRT AND RETURNS VIA TC Q OR TC FUNCTION +1.
+# SQUARE ROOT ERROR IS NOT MORE THAN 2 IN THE 14TH SIGNIFICANT BIT.  CELLS CLOBBERED ARE A,L,SHFTFLAG,ININDEX,
+# HALFARG,SCRATCH,SR,FUNCTION, FUNCTION +1.  GTSQRT IS CALLED BY TC GTSQRT AND RETURNS VIA TC Q OR TC FUNCTION +1.
 # ZERO OR NEGATIVE ARGUMENTS YIELD ZERO FOR SQUARE ROOTS.
 
 GTSQRT		CCS	FUNCTION
@@ -506,20 +506,19 @@ SCALDONE	EXTEND
 		TC	ROOTCYCL
 		TC	ROOTCYCL
 		TC	FUNCTION +1
-
-# ***************************************************************************
+# ****************************************************************************************************************
 
 RSTOFGTS	TC	GTSQRT
 PRODUCT		XCH	K2CNTRAL
 		EXTEND
 		MP	K2CNTRAL
 		DXCH	K2CNTRAL
-		EXTEND			#		THE PRODUCT OF
+		EXTEND			#	      THE PRODUCT OF
 		MP	L		#  1/2                   2       1/2
 		ADS	K2CNTRAL +1	# K   *(DEL*OMEGA + ALPHA /(2*K))
-		TS	L		#		      AND
-		TCF	+2		#                       2
-		ADS	K2CNTRAL	# DEL*(DEL*OMEGA + ALPHA /(2*K)) NOW IN
+		TS	L		#		  AND
+		TCF	+2		#                        2
+		ADS	K2CNTRAL	#  DEL*(DEL*OMEGA + ALPHA /(2*K)) NOW IN
 					# K2CNTRAL
 
 DOSHIFT		CA	ININDEX
@@ -538,22 +537,22 @@ DOSHIFT		CA	ININDEX
 		XCH	K2CNTRAL
 		EXTEND
 		MP	K2CNTRAL +1
-		ADS	K2THETA +1
+		ADS	K2THETA  +1
 		TS	L
-		TCF	+2
+		TCF	 +2
 		ADS	K2THETA
 
 		TCF	NEGUSUM
 
 ADDITIN		EXTEND
 		DCA	K2CNTRAL
-		DAS	K2THETA		# NO ADD IN THE K2THETA TERM.
+		DAS	K2THETA		# NOW ADD IN THE K2THETA TERM.
 NEGUSUM		CCS	K2THETA		# TEST SIGN OF HIGH ORDER PART.
 		TCF	NEGDRIVE
-		TCF	+2
+		TCF	 +2
 		TCF	POSDRIVE
 
-		CCS	K2THETA +1	# SIGN TEST FOR LOW ORDER PART.
+		CCS	K2THETA  +1	# SIGN TEST FOR LOW ORDER PART.
 NEGDRIVE	CA	BIT1
 		TCF	+2		# STOP GIMBAL DRIVE FOR A ZERO NEGUSUM.
 POSDRIVE	CS	BIT1
@@ -597,17 +596,15 @@ CLOSEADR	2CADR	CLOSEOUT	# TERMINATE THE JASK.
 
 TWELVE		EQUALS	OCT14
 ROOTHALF	OCTAL	26501		# SQUARE ROOT OF 1/2
-GMBLBITA	OCTAL	01400		# INDEXED WRT GMBLBITB	DO NOT MOVE *******
-OCT11276	OCTAL	11276		# POSMAX -- ROOTHALF
-GMBLBITB	OCTAL	06000		# INDEXED WRT GMBLBITA	DO NOT MOVE *******
+GMBLBITA	OCTAL	01400		# INDEXED WRT GMBLBITB   DO NOT MOVE******
+OCT11276	OCTAL	11276		# POSMAX - ROOTHALF
+GMBLBITB	OCTAL	06000		# INDEXED WRT GMBLBITA   DO NOT MOVE******
 
-# SUBROUTINE ROOTCYCL:	BY CRAIG WORK, 3 APRIL 68
-#
-# ROOTCYCL IS A SUBROUTINE WHICH EXECUTES ONE NEWTON SQUARE ALGORITHM ITERATION.  THE INITIAL GUESS AT THE
-# SQUARE ROOT IS PRESUMED TO BE IN THE A REGISTER AND ONE-HALF THE SQUARE IS TAKEN FROM HALFARG.  THE NEW APPROXIMATION
-# TO THE SQUARE ROOT IS RETURNED IN THE A REGISTER.  DEBRIS:  A, L, SR, SCRATCH.  ROOTCYCL IS CALLED FROM
+# SUBROUTINE ROOTCYCL:	BY CRAIG WORK,3 APRIL 68
+# ROOTCYCL IS A SUBROUTINE WHICH EXECUTES ONE NEWTON SQUARE ROOT ALGORITHM ITERATION.  THE INITIAL GUESS AT THE
+# SQUARE ROOT IS PRESUMED TO BE IN THE A REGISTER AND ONE-HALF THE SQUARE IS TAKEN FROM HALFARG.  THE NEW APPROXI-
+# MATION TO THE SQUARE ROOT IS RETURNED IN THE A REGISTER.  DEBRIS:   A,L,SR,SCRATCH.  ROOTCYCL IS CALLED FROM
 # LOCATION (LOC) BY A TC ROOTCYCL, AND RETURNS (TC Q) TO LOC +1.
-#
 # WARNING:  IF THE INITIAL GUESS IS NOT GREATER THAN THE SQUARE, DIVIDE OR ADD OVERFLOW IS A REAL POSSIBILITY.
 
 ROOTCYCL	TS	SCRATCH		# STORE X
@@ -618,5 +615,3 @@ ROOTCYCL	TS	SCRATCH		# STORE X
 		DV	SCRATCH		# (ARG/X)/2
 		AD	SR		# (X + ARG/X)/2 IN THE A REG
 		TC	Q
-
-

Luminary099/WAITLIST.agc

@@ -203,7 +203,7 @@ SVCT3X		TC	FIXDELAY	# DELAY MAX OF 2 TIMES FOR IMUZERO.
 WAIT2		TS	WAITBANK	# BBANK OF CALLING PROGRAM.
 		CA	Q
 		EXTEND
-		BZMF	WAITP00H
+		BZMF	WAITPOOH
 
 		CS	TIME3
 		AD	BIT8		# BIT 8 = OCT 200
@@ -506,10 +506,10 @@ LNGCALL2	LXCH	LONGEXIT +1	# SAVE THE CORRECT BB FOR RETURN
 		CCS	A
 		TCF	LONGCYCL	# HI-ORDER OK --> ALL IS OK.
 		TCF	+2		# HI-ORDER ZERO --> CHECK LO-ORDER.
-		TCF	LONGP00H	# HI-ORDER NEG. --> NEG. DT
+		TCF	LONGPOOH	# HI-ORDER NEG. --> NEG. DT
  +2		CA	LONGTIME +1	# CHECK LO-ORDER FOR ZERO OR NEGATIVE.
 		EXTEND
-		BZMF	LONGP00H	# BAD DELTA-TIME.  ABORT
+		BZMF	LONGPOOH	# BAD DELTA-TIME.  ABORT
 
 # *** WAITLIST TASK LONGCYCL ***
 
@@ -556,9 +556,9 @@ GETCADR		DXCH	LONGCADR	# GET THE LONGCALL THAT WE WISHED TO START
 		DTCB			# AND TRANSFER CONTROL TO IT
 
 TSKOVCDR	GENADR	TASKOVER
-LONGP00H	DXCH	LONGEXIT
+LONGPOOH	DXCH	LONGEXIT
 		TCF	+2
-WAITP00H	DXCH	WAITEXIT
+WAITPOOH	DXCH	WAITEXIT
  +2		TC	POODOO1
 		OCT	01204
 

README.ar.md

@@ -18,15 +18,18 @@
 [Italiano][IT]،
 [Kurdi][KU]،
 [Nederlands][NL]،
+[Norsk][NO]،
 [Polski][PL]،
 [Português][PT_BR]،
 [Română][RO]،
 [Tiếng Việt][VI]،
 [Türkçe][TR]،
+[Ελληνικά][GR]،
 [Русский][RU]،
 **العربية**،
 [فارسی][FA]،
 [हिंदी][HI_IN]،
+[অসমীয়া][AS_IN]،
 [বাংলা][BD_BN]،
 [မြန်မာ][MM]،
 [日本語][JA]،
@@ -35,6 +38,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -43,13 +47,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -58,7 +66,6 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
 الكود المصدري الأصلي لحاسوب الارشاد لأبولو 11 (AGC) للمركبة القيادية (Comanche055) والمركبة القمرية (Luminary099). تم ترقيمه من قبل [AGC الافتراضية][3] و[متحف MIT][4]. الهدف أن تكون مستودع للكود المصدري الأصلي لأبولو 11 (AGC). لهذا فإن طلبات السحب مرحب بها لأي اختلاف يتم رصده بين النسخ في هذا المستودع والمسح الأصلي ل[Luminary 099][5] و[Comanche 055][6]، أو أي ملف قد فاتني.
 

README.as_in.md

@@ -0,0 +1,120 @@
+# Apollo-11
+
+[![NASA][1]][2]
+[![SWH]][SWH_URL]
+[![Comanche]][ComancheMilestone]
+[![Luminary]][LuminaryMilestone]
+
+🎌
+[Bahasa Indonesia][ID],
+[Català][CA],
+[Čeština][CZ],
+[Deutsch][DE],
+[English][EN],
+[Español][ES],
+[Français][FR],
+[Italiano][IT],
+[Kurdi][KU],
+[Nederlands][NL],
+[Polski][PL],
+[Português][PT_BR],
+[Română][RO],
+[Tiếng Việt][VI],
+[Türkçe][TR],
+[Русский][RU],
+[العربية][AR],
+[فارسی][FA],
+[हिंदी][HI_IN],
+**অসমীয়া**,
+[বাংলা][BD_BN],
+[မြန်မာ][MM],
+[日本語][JA],
+[正體中文][ZH_TW],
+[简体中文][ZH_CN],
+[한국어][KO_KR]
+
+[AR]:README.ar.md
+[AS_IN]:README.as_in.md
+[BD_BN]:README.bd_bn.md
+[CA]:README.ca.md
+[CZ]:README.cz.md
+[DE]:README.de.md
+[EN]:README.md
+[ES]:README.es.md
+[FA]:README.fa.md
+[FR]:README.fr.md
+[HI_IN]:README.hi_in.md
+[ID]:README.id.md
+[IT]:README.it.md
+[JA]:README.ja.md
+[KO_KR]:README.ko_kr.md
+[KU]:README.ku.md
+[MM]:README.mm.md
+[PL]:README.pl.md
+[PT_BR]:README.pt_br.md
+[RO]:README.ro.md
+[RU]:README.ru.md
+[TR]:README.tr.md
+[VI]:README.vi.md
+[ZH_CN]:README.zh_cn.md
+[ZH_TW]:README.zh_tw.md
+[NL]:README.nl.md
+
+মূল এপোলো 11 গাইডেন্স কম্পিউটাৰ (AGC) কমাণ্ড মডিউল (Comanche055) আৰু লুনাৰ মডিউলৰ বাবে উৎস ক'ড (Luminary099)। [Virtual AGC][3] আৰু [MIT Museum][4] থকা লোকৰ দ্বাৰা ডিজিটাইজ কৰা হৈছে। লক্ষ্যটো হৈছে মূল এপলো 11 উৎস ক'ডৰ বাবে repo হোৱা। এনেদৰে, এই ভঁৰালত প্ৰতিলিপি আৰু লুমিনাৰী 099 আৰু কোমানচে 055-ৰ বাবে মূল উৎসৰ মাজত চিনাক্ত কৰা যিকোনো সমস্যাৰ বাবে পি.আৰ. স্বাগতম, লগতে মোৰ থাকি যাব পৰা যিকোনো ফাইল সংলগ্ন কৰিব পাৰে।
+
+## অৱদান
+
+অনুগ্ৰহ কৰি pull requestৰ আগতে [COMPINING.md][7] পঢ়ক।
+
+## কম্পাইল
+
+যদি আপুনি মূল উৎস ক'ড কম্পাইল কৰাত আগ্ৰহী, [Virtual AGC][8] চাওক।
+
+## Attribution
+
+          |  
+:------------- | :-----
+কপিৰাইট       | ৰাজহুৱা ডমেইন
+Comanche055    | কলোচাছ (Colossus) 2A ৰ উৎস কোডৰ অংশ, এপলো 11-ৰ কমাণ্ড মডিউলৰ (CM) এপলো গাইডেচন কম্পিউটাৰ (AGC)<br>`Assemble revision 055 of AGC program Comanche by NASA`<br>`2021113-051. 10:28 APR. 1, 1969`
+Luminary099    | লুমিনাৰী (Luminary) 1A-ৰ বাবে উৎস কোডৰ অংশ, এপোলো 11-ৰ বাবে লুনাৰ মডিউলৰ (LM) এপোলো গাইডেচন কম্পিউটাৰ (AGC)<br>`Assemble revision 001 of AGC program LMY99 by NASA`<br>`2021112-061. 16:27 JUL. 14, 1969`
+Assembler      | yaYUL
+যোগাযোগ        | Ron Burkey <info@sandroid.org>
+ৱেবছাইট        | www.ibiblio.org/apollo
+Digitalisation | This source code has been transcribed or otherwise adapted from digitized images of a hardcopy from the MIT Museum. The digitization was performed by Paul Fjeld, and arranged for by Deborah Douglas of the Museum. Many thanks to both.
+
+## চুক্তি আৰু অনুমোদন
+
+*এই বিভাগটো [CONTRACT_AND_APPROVALS.agc]ৰ পৰা আহৰণ কৰা হৈছে*
+
+এই এজিচি প্ৰ'গ্ৰামক কোলচাছ 2এ বুলিও কোৱা হ'ব।
+
+প্ৰতিবেদন 'R-577'ত নিৰ্ধাৰিত অনুসৰি এই প্ৰ'গ্ৰামটো চি.এম.-ত ব্যৱহাৰ হৈছিল। এই কাৰ্য্যসূচীটো DSR প্ৰকল্প '55-23870'ৰ অধীনত প্ৰস্তুত কৰা হৈছিল, যাৰ পৃষ্ঠপোষকতা কৰিছিল National Aeronautics and Space Administrationৰ Manned Spacecraft Centerএ, Instrumentation Laboratory, Massachusetts Institute of Technologyৰ সৈতে চুক্তি 'NAS 9-4065'ৰ যোগেৰে।
+
+দাখিলকাৰী             | ভূমিকা | দিনাংক
+:------------------- | :--- | :---
+Margaret H. Hamilton | Colossus Programming Leader<br>Apollo Guidance and Navigation | ২৮ মাৰ্চ '৬৯
+
+অনুমোদক          | ভূমিকা | দিনাংক
+:---------------- | :--- | :---
+Daniel J. Lickly  | পৰিচালক, Mission Program Development<br>Apollo Guidance and Navigation Program | ২৮ মাৰ্চ '৬৯
+Fred H. Martin    | Colossus প্ৰকল্প ব্যৱস্থাপক<br>Apollo Guidance and Navigation Program | ২৮ মাৰ্চ '৬৯
+Norman E. Sears   | পৰিচালক, Mission Development<br>Apollo Guidance and Navigation Program | ২৮ মাৰ্চ '৬৯
+Richard H. Battin | পৰিচালক, Mission Development<br>Apollo Guidance and Navigation Program | ২৮ মাৰ্চ '৬৯
+David G. Hoag     | পৰিচালক<br>Apollo Guidance and Navigation Program | ২৮ মাৰ্চ '৬৯
+Ralph R. Ragan    | উপ-পৰিচালক<br>Instrumentation Laboratory | ২৮ মাৰ্চ '৬৯
+
+[CONTRACT_AND_APPROVALS.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Comanche055/CONTRACT_AND_APPROVALS.agc
+[1]:https://flat.badgen.net/badge/NASA/Mission%20Overview/0B3D91
+[2]:https://www.nasa.gov/mission_pages/apollo/missions/apollo11.html
+[3]:http://www.ibiblio.org/apollo/
+[4]:http://web.mit.edu/museum/
+[5]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/
+[6]:http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/
+[7]:https://github.com/chrislgarry/Apollo-11/blob/master/CONTRIBUTING.md
+[8]:https://github.com/rburkey2005/virtualagc
+[SWH]:https://flat.badgen.net/badge/Software%20Heritage/Archive/0B3D91
+[SWH_URL]:https://archive.softwareheritage.org/browse/origin/https://github.com/chrislgarry/Apollo-11/
+[Comanche]:https://flat.badgen.net/github/milestones/chrislgarry/Apollo-11/1
+[ComancheMilestone]:https://github.com/chrislgarry/Apollo-11/milestone/1
+[Luminary]:https://flat.badgen.net/github/milestones/chrislgarry/Apollo-11/2
+[LuminaryMilestone]:https://github.com/chrislgarry/Apollo-11/milestone/2

README.bd_bn.md

@@ -16,15 +16,18 @@
 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 **বাংলা**,
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,35 +64,34 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
 অ্যাপোলো ১১ গাইডেন্স কম্পিউটারের মূল ম্যানুয়াল (AGC), অ্যাপোলো ১১ কমান্ড মডিউল (Comanche055) এবং লুনার মডিউল (Luminary099)। এটি [Virtual AGC][3] এবং [MIT Museum][4] সদস্যদের দ্বারা সূচিত করা হয়েছে। আমাদের মূল লক্ষ্য অ্যাপোলো ১১ এর মূল কোডটি সংকলন করা। আপনি যদি এই বিরোধের প্রতিলিপি এবং [Luminary 099][5] এবং [Comanche 055][6] এর মধ্যে কোনও বৈষম্য উন্মোচন করেছেন, সেক্ষেত্রে আপনার সহযোগিতা PR হিসাবে প্রশংসিত হবে।
 
 ## অবদান
 
-একটি পুল রিকুয়েস্ট খোলার আগে দয়া করে পড়ুন [CONTRIBUTING.md][7]।
+কোনো পুল রিকুয়েস্ট খোলার আগে দয়া করে [CONTRIBUTING.md][7] তা পড়ুন।
 
 ## সংগ্রহ
 
-যদি আপনি এই নিয়মগুলি পরিচালনা করেন তবে তা [Virtual AGC][8] দেখুন।
+যদি আপনি এই নিয়মগুলি পরিচালনা করেন তবে [Virtual AGC][8] তা দেখুন।
 
 ## আরোপণ
 
         |  
 :----------- | :-----
 কপিরাইট       | পাবলিক ডোমেইন
-Comanche055  | Colossus 2A, কমান্ড মডিউলটির (CM) উত্স কোডের একটি অংশ, অ্যাপোলো ১১ গাইডেন্স কম্পিউটার (AGC)<br>`নাসা 055 দ্বারা AGC প্রোগ্রাম কোমঞ্চের একীভূত সংশোধনী`<br>`2021113-051. 10:28 APR. 1, 1969`
+Comanche055  | Colossus 2A, কমান্ড মডিউলটির (CM) উৎস কোডের একটি অংশ, অ্যাপোলো ১১ গাইডেন্স কম্পিউটার (AGC)<br>`নাসা 055 দ্বারা AGC প্রোগ্রাম কোমঞ্চের একীভূত সংশোধনী`<br>`2021113-051. 10:28 APR. 1, 1969`
 Luminary099  | লুমিনারি ১ এ, অ্যাপোলো ১১-এর চন্দ্র অংশ (LM) জন্য ফ্লোটেশন ডিভাইস (AGC) কোডের অংশ `নাসার দ্বারা এজিসি (AGC)প্রোগ্রাম LMY99 এর একীভূত সংশোধনী ০০১`<br>`2021112-061. 16:27 JUL. 14, 1969`
 অ্যাসেম্বলার     | yaYUL
 যোগাযোগ      | Ron Burkey <info@sandroid.org>
 ওয়েবসাইট      | www.ibiblio.org/apollo
-ডিজিটালাইজেশন | এই উত্স কোডটি MIT Museum থেকে একটি হার্ডকপির ডিজিটাইজড চিত্র থেকে অনুলিপি করা হয়েছে বা অন্যথায় রূপান্তরিত হয়েছে। ডিজিটালাইজেশনটি Paul Fjeld সঞ্চালনা করেছিলেন এবং যাদুঘরের Deborah Douglas দ্বারা ব্যবস্থা করেছিলেন। উভয়কে অনেক ধন্যবাদ।
+ডিজিটালাইজেশন | এই উৎস কোডটি এমআইটি জাদুঘরের একটি হার্ডকপির ডিজিটাইজড চিত্র থেকে অনুলিপি করা হয়েছে বা অন্যথায় রূপান্তরিত হয়েছে। ডিজিটালাইজেশনটি Paul Fjeld সঞ্চালনা করেছিলেন এবং যাদুঘরের Deborah Douglas দ্বারা ব্যবস্থা করেছিলেন। উভয়কে অনেক ধন্যবাদ।
 
 ### চুক্তি এবং গ্রহণযোগ্যতা
 
-*থেকে প্রাপ্ত [CONTRACT_AND_APPROVALS.agc]*
+*[CONTRACT_AND_APPROVALS.agc] হতে প্রাপ্ত*
 
-এই AGC প্রোগ্রামটিকে Colossus 2A এ হিসাবেও উল্লেখ করা হবে।
+এই AGC প্রোগ্রামটিকে Colossus 2A হিসাবেও উল্লেখ করা হবে।
 
 এই প্রোগ্রামটি CM প্রতিবেদনে নির্দিষ্ট হিসাবে ব্যবহারের জন্য উদ্দিষ্ট `R-577`. এই প্রোগ্রামটি DSR প্রকল্পের আওতায় প্রস্তুত করা হয়েছিল `55-23870`, এই চুক্তির মাধ্যমে দ্য ন্যাশনাল অ্যারোনটিকস অ্যান্ড স্পেস অ্যাডমিনিস্ট্রেশনের ম্যানড স্পেসক্র্যাফট সেন্টার স্পনসর করে `NAS 9-4065` যন্ত্রানুষঙ্গের ল্যাবরেটরি সহ, Massachusetts Institute of Technology, Cambridge, Mass.
 
@@ -92,7 +99,7 @@ Luminary099  | লুমিনারি ১ এ, অ্যাপোলো ১১
 :------------------- | :---- | :---
 Margaret H. Hamilton | কলসাস(Colossus) প্রোগ্রামিং লিডার<br>অ্যাপোলো গাইডেন্স এবং নেভিগেশন | ২৮ মার্চ ১৯৬৯
 
-দ্বারা অনুমোদিত      | ভূমিকা | তারিখ
+যাদের দ্বারা অনুমোদিত      | ভূমিকা | তারিখ
 :---------------- | :--- | :---
 Daniel J. Lickly  | পরিচালক, মিশন প্রোগ্রাম উন্নয়ন<br>অ্যাপোলো গাইডেন্স এবং নেভিগেশন প্রোগ্রাম | ২৮ মার্চ ১৯৬৯
 Fred H. Martin    | কলসাস প্রজেক্ট ম্যানেজার<br>অ্যাপোলো গাইডেন্স এবং নেভিগেশন প্রোগ্রাম | ২৮ মার্চ ১৯৬৯

README.ca.md

@@ -7,8 +7,8 @@
 
 🎌
 [Bahasa Indonesia][ID],
-[Čeština][CZ],
 **Català**,
+[Čeština][CZ],
 [Deutsch][DE],
 [English][EN],
 [Español][ES],
@@ -16,15 +16,18 @@
 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,7 +64,8 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
+[ZH_CN]:README.zh_cn.md
+[ZH_TW]:README.zh_tw.md
 
 Codi font original del Mòdul de Comandament (Comanche055) i del Mòdul Lunar (Comanche055) de l'ordinador de navegació de l'Apollo 11 (AGC, per les seves sigles en anglès). Digitalitzat per la gent de [Virtual AGC][3] i [MIT Museum][4]. L'objectiu és esdevenir un repositori del codi font original de l'Apollo 11. Per això els *pull requests* són benvinguts davant de qualsevol problema que s'identifiqui entre les transcripcions d'aquests repositori i les còpies originals del codi font de [Luminary 099][5] i [Comanche 055][6], així com qualsevol fitxer que m'hagi pogut deixar.
 

README.cz.md

@@ -10,21 +10,24 @@
 [Català][CA],
 **Čeština**,
 [Deutsch][DE],
-[English][EN]
+[English][EN],
 [Español][ES],
 [Français][FR],
 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,7 +64,12 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
+[ZH_CN]:README.zh_cn.md
+[ZH_TW]:README.zh_tw.md
+[ZH_CN]:README.zh_cn.md
+[ZH_TW]:README.zh_tw.md
+[ZH_CN]:README.zh_cn.md
+[ZH_TW]:README.zh_tw.md
 
 Originální zdrojové kódy navigačního počítače (AGC) Apolla 11 pro Velitelský Modul (Comanche055) a Lunární Modul (Luminary099). Digitalizováno s pomocí [Virtual AGC][3] a [MIT Museum][4]. Cílem repozitáře je udržovat původní zdrojové kódy Apolla 11. Vítáme všechny PR s úpravami problémů identifikovaných mezi přepisy v tomto repozitáři a originálními skeny pro [Luminary 099][5] a [Comanche 055][6], stejně jako soubory které mohly být přehlédnuty.
 

README.de.md

@@ -16,15 +16,18 @@
 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,7 +64,8 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
+[ZH_CN]:README.zh_cn.md
+[ZH_TW]:README.zh_tw.md
 
 Dieses Repository beinhaltet den originalen Quellcode des Apollo 11 Navigationscomputers (kurz AGC) für das Kommandomodul (Comanche055) und die Mondlandefähre (Luminary099). Digitalisiert wurde der Code durch das [Virtual AGC][3] Projekt und das [MIT Museum][4]. Ziel dieses Projektes ist es, den originalen Apollo 11 Source Code an einem zentralen Ort zu sammeln. Daher sind PRs, die Diskrepanzen zwischen den Transkripten in diesem Repository und den originalen Scans des Source Codes von [Luminary 099][5] und [Comanche 055][6] beheben, gern gesehen.
 

README.es.md

@@ -16,15 +16,18 @@
 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,7 +64,6 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
 Código fuente original del ordenador guía del Apolo 11 (AGC) para el módulo de comando (Comanche055) y del módulo lunar (Luminary099). Digitalizado por los chicos de [Virtual AGC][3] y [el museo del MIT][4]. El objetivo es ser un repositorio del código fuente original del Apolo 11. De este modo, serán bienvenidos los PRs relacionados con las transcripciones en este repositorio y los escaneos del código fuente original para el [Luminary 099][5] y el [Comanche 055][6], así como cualquier archivo que se me haya olvidado.
 

README.fa.md

@@ -18,15 +18,18 @@
 [Italiano][IT]،
 [Kurdi][KU]،
 [Nederlands][NL]،
+[Norsk][NO]،
 [Polski][PL]،
 [Português][PT_BR]،
 [Română][RO]،
 [Tiếng Việt][VI]،
 [Türkçe][TR]،
+[Ελληνικά][GR]،
 [Русский][RU]،
 [العربية][AR]،
 **فارسی**،
 [हिंदी][HI_IN]،
+[অসমীয়া][AS_IN]،
 [বাংলা][BD_BN]،
 [မြန်မာ][MM]،
 [日本語][JA]،
@@ -35,6 +38,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -43,13 +47,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -58,7 +66,6 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
 سورس کد اصلی سیستم هدایت آپولو ۱۱ (AGC) برای سفینه فرمان (Comanche055) و سفینه ماه‌نشین (Luminary099). دیجیتال شده توسط جمعی از در [مجازی AGC][3] و [MIT موزه][4]. مقصود این است که یک مخزن برای سورس کد اصلی آپولو ۱۱ باشد. همین‌طور، از پول‌ریکوئست‌ها برای هر تفاوتی بین نسخه‌ی موجود در این مخزن با اسکن‌ فایل‌های اصلی برای [Luminary 099][5] و [Comanche 055][6] و همچنین هر فایل دیگری که از دست من در رفته باشد،‌ استقبال می‌شود.
 

README.fr.md

@@ -16,15 +16,18 @@
 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,17 +64,16 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
 Code source original de l'ordinateur de guidage Apollo 11 (AGC) pour le module de commande (Comanche055) et le module lunaire (Luminary099). Numérisé par les gens du [Virtual AGC][3] et du [MIT Museum][4]. Le but est d'être un repo pour le code source original d'Apollo 11. En tant que tel, les PR sont les bienvenues pour tous les problèmes identifiés entre les transcriptions dans ce référentiel et les scans source originaux pour [Luminary 099][5] et [Comanche 055][6], ainsi que pour tous les fichiers que j'ai pu manquer.
 
 ## Contribuer
 
-Merci de lire [CONTRIBUTING.fr.md][7] avant d'ouvrir une pull request.
+Merci de lire [CONTRIBUTING.fr.md][7] avant d'ouvrir un pull request.
 
 ## Compilation
 
-Si vous êtes intéressés par la compilation du code source original visitez [Virtual AGC][8].
+Si vous êtes intéressé par la compilation du code source original, visitez [Virtual AGC][8].
 
 ## Attribution
 

README.gr.md

@@ -0,0 +1,125 @@
+# Apollo-11
+
+[![NASA][1]][2]
+[![SWH]][SWH_URL]
+[![Comanche]][ComancheMilestone]
+[![Luminary]][LuminaryMilestone]
+
+🎌
+[Bahasa Indonesia][ID],
+[Català][CA],
+[Čeština][CZ],
+[Deutsch][DE],
+[English][EN],
+[Español][ES],
+[Français][FR],
+[Italiano][IT],
+[Kurdi][KU],
+[Nederlands][NL],
+[Norsk][NO],
+[Polski][PL],
+[Português][PT_BR],
+[Română][RO],
+[Tiếng Việt][VI],
+[Türkçe][TR],
+**Ελληνικά**,
+[Русский][RU],
+[العربية][AR],
+[فارسی][FA],
+[हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
+[বাংলা][BD_BN],
+[မြန်မာ][MM],
+[日本語][JA],
+[正體中文][ZH_TW],
+[简体中文][ZH_CN],
+[한국어][KO_KR]
+
+[AR]:README.ar.md
+[AS_IN]:README.as_in.md
+[BD_BN]:README.bd_bn.md
+[CA]:README.ca.md
+[CZ]:README.cz.md
+[DE]:README.de.md
+[EN]:README.md
+[ES]:README.es.md
+[FA]:README.fa.md
+[FR]:README.fr.md
+[GR]:README.gr.md
+[HI_IN]:README.hi_in.md
+[ID]:README.id.md
+[IT]:README.it.md
+[JA]:README.ja.md
+[KO_KR]:README.ko_kr.md
+[KU]:README.ku.md
+[LT]:README.lt.md
+[MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
+[PL]:README.pl.md
+[PT_BR]:README.pt_br.md
+[RO]:README.ro.md
+[RU]:README.ru.md
+[TR]:README.tr.md
+[VI]:README.vi.md
+[ZH_CN]:README.zh_cn.md
+[ZH_TW]:README.zh_tw.md
+
+Ο πρωτότυπος πηγαίος κώδικας του υπολογιστή πλοήγησης (guidance computer) του Apollo 11 (AGC) για το Command Module (Comanche055) και το Lunar Module (Luminary099). Ψηφιοποίηση από ανθρώπους στο [Virtual AGC][3] και το [MIT Museum][4]. Ο στόχος είναι αυτό το αποθετήριο να παρέχει όλο τον πηγαίο κώδικα του Apollo 11. Ως εκ τούτου, τα PRs είναι ευπρόσδεκτα για τυχόν ζητήματα που εντοπίζονται μεταξύ των μεταγραφών σε αυτό το αποθετήριο και των αρχικών σαρώσεων προέλευσης για το [Luminary 099][5] και το [Comanche 055][6], καθώς επίσης και για αρχεία που λείπουν.
+
+## Συνεισφορά
+
+Παρακαλώ διαβάστε το [CONTRIBUTING.gr.md][7] πριν ανοίξετε ένα pull request.
+
+## Σύνταξη πηγαίου κώδικα (Compiling)
+
+Αν ενδιαφέρεστε να κάνετε compile τον πρωτότυπο πηγαίο κώδικα, δείτε το [Virtual AGC][8].
+
+## Απόδοση
+
+                 |  
+:-------------        | :-----
+Πνευματική ιδιοκτησία | Δημόσιος τομέας (Public domain)
+Comanche055           | Μέρος του πηγαίου κώδικα για το Colossus 2A, το Command Module's (CM) Apollo Guidance Computer (AGC) για το Apollo 11<br>`Assemble revision 055 of AGC program Comanche by NASA`<br>`2021113-051. 10:28 APR. 1, 1969`
+Luminary099           | Μέρος του πηγαίου κώδικα για το Luminary 1A, το Lollar Module's (LM) Apollo Guidance Computer (AGC) για το Apollo 11<br>`Assemble revision 001 of AGC program LMY99 by NASA`<br>`2021112-061. 16:27 JUL. 14, 1969`
+Συμβολομεταφράστης    | yaYUL
+Επικοινωνία           | Ron Burkey <info@sandroid.org>
+Ιστοσελίδα            | www.ibiblio.org/apollo
+Ψηφιοποίηση           | Αυτός ο πηγαίος κώδικας έχει μεταγραφεί ή αλλιώς προσαρμοστεί από ψηφιοποιημένες εικόνες έντυπου αντιγράφου από το Μουσείο MIT. Η ψηφιοποίηση πραγματοποιήθηκε από τον Paul Fjeld και διευθετήθηκε από την Deborah Douglas του Μουσείου. Ευχαριστώ πολύ και τους δύο.
+
+### Σύμβαση και εγκρίσεις
+
+Προέρχεται από το [CONTRACT_AND_APPROVALS.agc]*
+
+Το πρόγραμμα του AGC αναφέρεται επίσης και ως Colossus 2A.
+
+Αυτό το πρόγραμμα προορίζεται για χρήση στο CM, όπως ορίζεται στην αναφορά R-577. Αυτό το πρόγραμμα προετοιμάστηκε στο πλαίσιο του έργου DSR 55-23870, που χρηματοδοτήθηκε από το Manned Spacecraft Center of the National Aeronautics and Space Administration μέσω της σύμβασης NAS 9-4065 με το Instrumentation Laboratory, Massachusetts Institute of Technology, Cambridge, Mass.
+
+Υποβλήθηκε από       | Ρόλος | Ημερομηνία
+:------------------- | :--- | :---
+Margaret H. Hamilton | Colossus Programming Leader<br>Apollo Guidance and Navigation | 28 Mar 69
+
+Εγκρίθηκε από     | Ρόλος | Ημερομηνία
+:---------------- | :--- | :---
+Daniel J. Lickly  | Διευθυντής, Mission Program Development<br>Apollo Guidance and Navigation Program | 28 Mar 69
+Fred H. Martin    | Colossus Project Manager<br>Apollo Guidance and Navigation Program | 28 Mar 69
+Norman E. Sears   | Διευθυντής, Mission Development<br>Apollo Guidance and Navigation Program | 28 Mar 69
+Richard H. Battin | Διευθυντής, Mission Development<br>Apollo Guidance and Navigation Program | 28 Mar 69
+David G. Hoag     | Διευθυντής<br>Apollo Guidance and Navigation Program | 28 Mar 69
+Ralph R. Ragan    | Αναπληρωτής Διευθυντής<br>Instrumentation Laboratory | 28 Mar 69
+
+[CONTRACT_AND_APPROVALS.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Comanche055/CONTRACT_AND_APPROVALS.agc
+[1]:https://flat.badgen.net/badge/NASA/Mission%20Overview/0B3D91
+[2]:https://www.nasa.gov/mission_pages/apollo/missions/apollo11.html
+[3]:http://www.ibiblio.org/apollo/
+[4]:http://web.mit.edu/museum/
+[5]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/
+[6]:http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/
+[7]:https://github.com/chrislgarry/Apollo-11/blob/master/CONTRIBUTING.gr.md
+[8]:https://github.com/rburkey2005/virtualagc
+[SWH]:https://flat.badgen.net/badge/Software%20Heritage/Archive/0B3D91
+[SWH_URL]:https://archive.softwareheritage.org/browse/origin/https://github.com/chrislgarry/Apollo-11/
+[Comanche]:https://flat.badgen.net/github/milestones/chrislgarry/Apollo-11/1
+[ComancheMilestone]:https://github.com/chrislgarry/Apollo-11/milestone/1
+[Luminary]:https://flat.badgen.net/github/milestones/chrislgarry/Apollo-11/2
+[LuminaryMilestone]:https://github.com/chrislgarry/Apollo-11/milestone/2

README.hi_in.md

@@ -16,15 +16,18 @@
 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 **हिंदी**,
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,7 +64,6 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
 अपोलो ११ मार्गदर्शन कम्प्यूटर (Apollo 11 Guidance computer, AGC) कमांड मॉड्यूल (Comanche055) तथा चंद्र मॉड्यूल (Luminary099) का मूल नियम संग्रह। इसे [Virtual AGC][3] एवं [MIT Museum][4] के सदस्यों द्वारा अंक्रिकित किया गया है। हमारा मुख्य उद्देश्य अपोलो ११ के मूल नियम संग्रह को संकलित करना है। यदि आपने इस संघ्रह के प्रतिलेखन एवं [Luminary 099][5] और [Comanche 055][6] के बीच में किसी भी फर्क का अनावरण किया है, उस दशा में आपका सहयोग PR के रूप में बहुत ही अभिवादित है।
 

README.id.md

@@ -16,15 +16,18 @@
 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,7 +64,6 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
 Kode sumber orisinil Komputer Pemandu Apollo 11 (AGC) untuk Modul Komando (Comanche055) dan Modul Bulan (Luminary099). Didigitalkan oleh [Virtual AGC][3] dan [MIT Museum][4]. Tujuan dari repo ini adalah untuk menjadi repo kode sumber Apollo 11 yang orisinil. Dengan demikian, siapapun dipersilakan untuk mengirimkan Pull Request untuk issue atau perbedaan apapun yang ditemukan antara transkripsi di repositori ini dengan kode sumber orisinil hasil scan untuk [Luminary 099][5] dan [Comanche 055][6], juga file apapun yang mungkin lupa saya masukkan.
 

README.it.md

@@ -16,15 +16,18 @@
 **Italiano**,
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,13 +64,12 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
 Codice sorgente dell'Apollo 11 Guidance Computer (AGC) utilizzato dal Command Module (Comanche055) e dal Lunar Module (Luminary099). Digitalizzato dagli autori del [Virtual AGC][3] e dal [MIT Museum][4]. L'obbiettivo è quello di avere un repository contenente il codice usato dalla missione Apollo 11. Di conseguenza, le PRs volte a correggere qualsiasi problema, identificato confrontando le trascrizioni in questo repository e le scansioni originali del codice del [Luminary 099][5] e del [Comanche 055][6], sono benvenute.
 
 ## Contribuire
 
-Leggere [CONTRIBUTING.md][7] prima di aprire una pull request (PR).
+Leggere [CONTRIBUTING.it.md][7] prima di aprire una pull request (PR).
 
 ## Compilare
 
@@ -108,7 +115,7 @@ Ralph R. Ragan    | Deputy Director<br>Instrumentation Laboratory | 28 Mar 69
 [4]:http://web.mit.edu/museum/
 [5]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/
 [6]:http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/
-[7]:https://github.com/chrislgarry/Apollo-11/blob/master/CONTRIBUTING.md
+[7]:https://github.com/chrislgarry/Apollo-11/blob/master/CONTRIBUTING.it.md
 [8]:https://github.com/rburkey2005/virtualagc
 [SWH]:https://flat.badgen.net/badge/Software%20Heritage/Archive/0B3D91
 [SWH_URL]:https://archive.softwareheritage.org/browse/origin/https://github.com/chrislgarry/Apollo-11/

README.ja.md

@@ -16,15 +16,18 @@
 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 **日本語**,
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,7 +64,6 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
 司令船・機械船(Comanche055)および月着陸船(Luminary099)用のオリジナルのアポロ11号誘導コンピュータ(AGC)のソースコード。[Virtual AGC][3] と [MIT Museum][4] によってデジタル化された。このリポジトリは、オリジナルのアポロ11号のソースコードを完全に再現して保管することを目的としています。そのため、このリポジトリと [Luminary 099][5] および [Comanche 055][6] の間に発見された問題や見落としがある可能性のあるファイルに対してのPRは歓迎します。
 

README.ko_kr.md

@@ -16,15 +16,18 @@
 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 **한국어**
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,9 +64,8 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
-사령선 모듈 (Comanche055) 및 달 착륙선 모듈 (Luminary099)을 위한 아폴로 11호 유도 컴퓨터(AGC)의 소스코드입니다. [Virtual AGC][3] 및 [MIT Museum][4]에 의해 디지털화 되었습니다. 이 레포지토리는 아폴로 11호의 원본 소스코드를 완벽하게 재현하여 보관하는 것을 목표로 합니다. 따라서 원본과 본 디지털본 간에 발견된 모든 이슈, 또한 빠뜨렸을 듯한 파일들에 대해 PR을 환영합니다.
+사령선 모듈 (Comanche055) 및 달 착륙선 모듈 (Luminary099)을 위한 아폴로 11호 유도 컴퓨터(AGC)의 소스코드입니다. [Virtual AGC][3] 및 [MIT Museum][4]에 의해 디지털화되었습니다. 이 레포지토리는 아폴로 11호의 원본 소스코드를 완벽하게 재현하여 보관하는 것을 목표로 합니다. 따라서 원본과 본 디지털본 간에 발견된 모든 이슈, 또한 빠뜨렸을 듯한 파일들에 대해 PR을 환영합니다.
 
 ## 기여하기
 
@@ -78,7 +85,7 @@ Luminary099 | Part of the source code for Luminary 1A, the Lunar Module's (LM) A
 어셈블러     | yaYUL
 연락처       | Ron Burkey <info@sandroid.org>
 웹사이트     | www.ibiblio.org/apollo
-디지털화     | 이 소스코드는 MIT Museum에서 하드카피본을 디지털화, 옮긴 것 입니다. 디지털화는 Paul Fjeld에 의해 이루어졌으며, Deborah Douglas가 정리하였습니다. 두 분께 깊은 감사를 표합니다.
+디지털화     | 이 소스코드는 MIT Museum에서 하드 카피본을 디지털화, 옮긴 것입니다. 디지털화는 Paul Fjeld에 의해 이루어졌으며, Deborah Douglas가 정리하였습니다. 두 분께 깊은 감사를 표합니다.
 
 ### Contract and Approvals
 
@@ -86,7 +93,7 @@ Luminary099 | Part of the source code for Luminary 1A, the Lunar Module's (LM) A
 
 본 아폴로 유도 컴퓨터 프로그램은 다음에 의해 참조됩니다 : 콜로서스 2A
 
-이 프로그램은 R-577에 명세된 사령선 모듈에 사용됩니다. DSR 프로젝트 55-23870 에 의해 준비되었으며, NASA 유인 우주선 센터가 MIT 기계 연구소 와의 NAS 9-4065 계약에 의해 스폰싱 하였습니다.
+이 프로그램은 R-577에 명세된 사령선 모듈에 사용됩니다. DSR 프로젝트 55-23870에 의해 준비되었으며, NASA 유인 우주선 센터가 MIT 기계 연구소와의 NAS 9-4065 계약에 의해 스폰싱 하였습니다.
 
 제출됨                | Role | 일시
 :------------------- | :--- | :--

README.ku.md

@@ -16,15 +16,18 @@
 [Italiano][IT],
 **Kurdî**,
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,7 +64,6 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
 Koda xwerû ya kompûterê rêbernameya Apollo 11 (AGC) ya orîjînal ji bo Wesayîta Rêvebirinê (Comanche055) û Wesayîta Hêvê (Luminary099). Hat jimarekirin ji aliyê [Virtual AGC][3] û [MIT Museum][4] va. Armanc ew e ku bibe wek depoyekê ji bo koda xwerû ya orîjînal ya Apollo 11. Ji bo wê yekê, daxwazê kişandinê tên pêşwazîkirin ji bo her pirsgirêkekî ku tê nîşankirin di nava vê depoyê de û kopiyên orîjînal yê [Luminary 099][5] û [Comanche 055][6], herweha çi dosya ku min ji bîr kirî.
 

README.md

@@ -16,15 +16,18 @@
 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,7 +64,6 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
 Original Apollo 11 guidance computer (AGC) source code for Command Module (Comanche055) and Lunar Module (Luminary099). Digitized by the folks at [Virtual AGC][3] and [MIT Museum][4]. The goal is to be a repo for the original Apollo 11 source code. As such, PRs are welcome for any issues identified between the transcriptions in this repository and the original source scans for [Luminary 099][5] and [Comanche 055][6], as well as any files I may have missed.
 

README.mm.md

@@ -16,15 +16,18 @@
 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 **မြန်မာ**,
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,7 +64,6 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
 မူရင်း Apollo 11​​ ထိန်းချုပ်မှု ကွန်ပျူတာ (AGC) တွင်ပါဝင်သော ကွပ်ကဲမှုအစိတ်အပိုင်း (Comanche055) နဲ့ လပေါ်တွင်ဆင်းသက်သည့် အစိတ်အပိုင်း (Luminary099) တို့ရဲ့ ကုဒ်။ [Virtual AGC][3] နှင့် [MIT Museum][4] အကူအညီဖြင့် ဒီဂျစ်တယ်ပုံစံသို့ ပြောင်းထားခြင်းဖြစ်သည်။​ မူရင်း Apollo 11 ကုဒ်များ သိမ်းစည်းထားသော ရီပိုတစ်ခုဖြစ်လာစေရန်ရည်ရွယ်သည်။ ဒါကြောင့် [Luminary 099][5] နဲ့ [Comanche 055][6] တို့ရဲ့ အရင်းအမြစ်စာတမ်းများနဲ့ ဒီရီပိုကြား ကွဲလွဲချက်များတွေ့ရင် Pull Request (PR) တွေဖွင့်ပေးဖို့ ကြိုဆိုပါတယ်။ ကျွန်တော် ကျန်ခဲ့တဲ့ ဖိုင်လ်လေးတွေရှိရင်လည်း ပြောပေးကြပါဉီး။
 

README.nl.md

@@ -16,15 +16,18 @@
 [Italiano][IT],
 [Kurdi][KU],
 **Nederlands**,
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,7 +64,6 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
 Originele broncode voor de Apollo 11 besturingscomputer (AGC). Broncode voor de besturingsmodule (Comanche055) en maanmodule (Luminary099). Gedigitalizeerd door [Virtual GC][3] en het [MIT Museum][4]. Het doel is om een repository te zijn van de oorspronkelijke Apollo 11 broncode en dus zijn PRs welkom voor elk probleem in de overgenomen broncode van [Luminary 099][5] en [Comanche 055][6] en elk bestand dat ik vergeten ben.
 

README.no.md

@@ -0,0 +1,125 @@
+# Apollo-11
+
+[![NASA][1]][2]
+[![SWH]][SWH_URL]
+[![Comanche]][ComancheMilestone]
+[![Luminary]][LuminaryMilestone]
+
+🎌
+[Bahasa Indonesia][ID],
+[Català][CA],
+[Čeština][CZ],
+[Deutsch][DE],
+[English][EN],
+[Español][ES],
+[Français][FR],
+[Italiano][IT],
+[Kurdi][KU],
+[Nederlands][NL],
+**Norsk**,
+[Polski][PL],
+[Português][PT_BR],
+[Română][RO],
+[Tiếng Việt][VI],
+[Türkçe][TR],
+[Ελληνικά][GR],
+[Русский][RU],
+[العربية][AR],
+[فارسی][FA],
+[हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
+[বাংলা][BD_BN],
+[မြန်မာ][MM],
+[日本語][JA],
+[正體中文][ZH_TW],
+[简体中文][ZH_CN],
+[한국어][KO_KR]
+
+[AR]:README.ar.md
+[AS_IN]:README.as_in.md
+[BD_BN]:README.bd_bn.md
+[CA]:README.ca.md
+[CZ]:README.cz.md
+[DE]:README.de.md
+[EN]:README.md
+[ES]:README.es.md
+[FA]:README.fa.md
+[FR]:README.fr.md
+[GR]:README.gr.md
+[HI_IN]:README.hi_in.md
+[ID]:README.id.md
+[IT]:README.it.md
+[JA]:README.ja.md
+[KO_KR]:README.ko_kr.md
+[KU]:README.ku.md
+[LT]:README.lt.md
+[MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
+[PL]:README.pl.md
+[PT_BR]:README.pt_br.md
+[RO]:README.ro.md
+[RU]:README.ru.md
+[TR]:README.tr.md
+[VI]:README.vi.md
+[ZH_CN]:README.zh_cn.md
+[ZH_TW]:README.zh_tw.md
+
+Original kildekode til Apollo 11’s veilednings datamaskin for kommando ( Comanche055 ) og måne ( Luminary099 ) modulene. Digitalisert av folkene ifra Virtual AGC og MIT Museet. Målet er og være et «repo» for den originale Apollo 11 kilde koden. «Pull Requests» er ønskelige for problemer som måtte finnes i oversettelser i dette «repository» og de originale kilde kode bildene til Luminary 099 og Comanche 055, samt bortglemte filer
+
+## Bidra
+
+Venligst les [CONTRIBUTING.no.md][7] før en "pull request" åpnes.
+
+## Kompilere
+
+Om du er interesert i og kompilere den originale kilde koden så sjekk [Virtual AGC][8].
+
+## Bidragsytere
+
+          |  
+:------------- | :-----
+Opphavsrett    | Public domain
+Comanche055    | Deler av kilde koden til Colossus 2A, kommando modulen ( CM ) til Apollo Veiledningsdatamaskin ( AGC ) til Apollo 11<br>`Assemble revision 055 of AGC program Comanche by NASA`<br>`2021113-051. 10:28 APR. 1, 1969`
+Luminary099    | Deler av kilde koden til Luminary 1A, the Lunar Module's ( LM ) Apollo Veiledningsdatamaskin ( AGC ) til Apollo 11<br>`Assemble revision 001 of AGC program LMY99 by NASA`<br>`2021112-061. 16:27 JUL. 14, 1969`
+Assembler      | yaYUL
+Kontakt        | Ron Burkey <info@sandroid.org>
+Webside        | www.ibiblio.org/apollo
+Digitalisering | Denne kilde koden er tydet og adoptert fra de digitaliserte bildene som finnes på MIT Museet. Digitaliseringen er utført av Paul Fjeld, og sortert av Deborah Douglas som jobber på Museet. Takk til dere begge.
+
+### Kontrakt og godkjenninger
+
+*Fra [CONTRACT_AND_APPROVALS.agc]*
+
+Dette AGC programmet skal også refereres til som Colossus 2A.
+
+Dette programmet brukes i «CM» som spesifisert i rapport `R-577`. Dette programmet var også laget under DST prosjekt `55-23870`, som var sponset av «Manned Spacecraft Center of The National Aeronautics and Space Administration» via kontrakt `NAS 9-4065` med instrumentasjon laboratoriet ved «Massachusetts Institute of Technology, Cambridge, Mass»
+
+Innsendt av          | Rolle | Dato
+:------------------- | :---- | :---
+Margaret H. Hamilton | Colossus Programming Leader<br>Apollo Guidance and Navigation | 28 Mar 69
+
+Godkjent av       | Rolle | Dato
+:---------------- | :---- | :---
+Daniel J. Lickly  | Director, Mission Program Development<br>Apollo Guidance and Navigation Program | 28 Mar 69
+Fred H. Martin    | Colossus Project Manager<br>Apollo Guidance and Navigation Program | 28 Mar 69
+Norman E. Sears   | Director, Mission Development<br>Apollo Guidance and Navigation Program | 28 Mar 69
+Richard H. Battin | Director, Mission Development<br>Apollo Guidance and Navigation Program | 28 Mar 69
+David G. Hoag     | Director<br>Apollo Guidance and Navigation Program | 28 Mar 69
+Ralph R. Ragan    | Deputy Director<br>Instrumentation Laboratory | 28 Mar 69
+
+[CONTRACT_AND_APPROVALS.agc]:https://github.com/chrislgarry/Apollo-11/blob/master/Comanche055/CONTRACT_AND_APPROVALS.agc
+[1]:https://flat.badgen.net/badge/NASA/Mission%20Overview/0B3D91
+[2]:https://www.nasa.gov/mission_pages/apollo/missions/apollo11.html
+[3]:http://www.ibiblio.org/apollo/
+[4]:http://web.mit.edu/museum/
+[5]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/
+[6]:http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/
+[7]:https://github.com/chrislgarry/Apollo-11/blob/master/CONTRIBUTING.no.md
+[8]:https://github.com/rburkey2005/virtualagc
+[SWH]:https://flat.badgen.net/badge/Software%20Heritage/Archive/0B3D91
+[SWH_URL]:https://archive.softwareheritage.org/browse/origin/https://github.com/chrislgarry/Apollo-11/
+[Comanche]:https://flat.badgen.net/github/milestones/chrislgarry/Apollo-11/1
+[ComancheMilestone]:https://github.com/chrislgarry/Apollo-11/milestone/1
+[Luminary]:https://flat.badgen.net/github/milestones/chrislgarry/Apollo-11/2
+[LuminaryMilestone]:https://github.com/chrislgarry/Apollo-11/milestone/2

README.pl.md

@@ -16,15 +16,18 @@
 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 **Polski**,
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,13 +64,12 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
-Oryginalny kod źródłowy komputera pokładowego w programie Apollo 11 (AGC) dla modułu dowodzenia (Comanche055) i modułu księżycowego (Luminary099). Zdigitalizowany przez ludzi z [Virtual AGC][3] i [MIT Museum][4]. Celem jest bycie repozytorium dla oryginalnego kodu źródłowego Apollo 11. Z tego powodu, PRy są mile widziane dla każdego przekłamania między transkrypcją w tym repozytorium a oryginalnymi skanami dla [Luminary 099][5] i [Comanche 055][6], jak również dla każdego pliku który mogłem przegapić.
+Oryginalny kod źródłowy komputera pokładowego Apollo 11 (AGC) dla modułu dowodzenia (Comanche055) i modułu księżycowego (Luminary099). Zdigitalizowany przez ludzi z [Virtual AGC][3] i [MIT Museum][4]. Celem jest ukazanie repozytorium dla oryginalnego kodu źródłowego Apollo 11. Z tego powodu, PRy są mile widziane dla każdego przekłamania między transkrypcją w tym repozytorium a oryginalnymi skanami dla [Luminary 099][5] i [Comanche 055][6], jak również dla każdego pliku który mogłem przegapić.
 
 ## Kontrybucje
 
-Proszę przeczytaj [CONTRIBUTING.md][7] zanim otworzysz nowy pull request.
+Proszę przeczytaj [CONTRIBUTING.pl.md][7] zanim otworzysz nowy pull request.
 
 ## Kompilowanie
 
@@ -108,7 +115,7 @@ Ralph R. Ragan     | Deputy Director<br>Instrumentation Laboratory | 28 Mar 69
 [4]:http://web.mit.edu/museum/
 [5]:http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/
 [6]:http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/
-[7]:https://github.com/chrislgarry/Apollo-11/blob/master/CONTRIBUTING.md
+[7]:https://github.com/chrislgarry/Apollo-11/blob/master/CONTRIBUTING.pl.md
 [8]:https://github.com/rburkey2005/virtualagc
 [SWH]:https://flat.badgen.net/badge/Software%20Heritage/Archive/0B3D91
 [SWH_URL]:https://archive.softwareheritage.org/browse/origin/https://github.com/chrislgarry/Apollo-11/

README.pt_br.md

@@ -16,15 +16,18 @@
 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 **Português**,
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,7 +64,6 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
 Código fonte do Computador de Orientação da Apollo 11 (AGC) para o Módulo de Comando (Comanche055) e Módulo Lunar (Luminary099). Digitalizado pelo pessoal da [Virtual AGC][3] e [Museu do MIT][4]. O objetivo é ser um repositório para o código fonte original da Apollo 11. Como tal, os PRs são bem-vindos para quaisquer problemas identificados entre as transcrições neste repositório e as verificações do código fonte original para [Luminary 099][5] e [Comanche 055][6], bem como quaisquer arquivos que eu possa ter perdido.
 

README.ro.md

@@ -16,15 +16,18 @@
 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 **Română**,
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
 [AR]:README.ar.md
+[AS_IN]:README.as_in.md
 [BD_BN]:README.bd_bn.md
 [CA]:README.ca.md
 [CZ]:README.cz.md
@@ -41,13 +45,17 @@
 [ES]:README.es.md
 [FA]:README.fa.md
 [FR]:README.fr.md
+[GR]:README.gr.md
 [HI_IN]:README.hi_in.md
 [ID]:README.id.md
 [IT]:README.it.md
 [JA]:README.ja.md
 [KO_KR]:README.ko_kr.md
 [KU]:README.ku.md
+[LT]:README.lt.md
 [MM]:README.mm.md
+[NL]:README.nl.md
+[NO]:README.no.md
 [PL]:README.pl.md
 [PT_BR]:README.pt_br.md
 [RO]:README.ro.md
@@ -56,7 +64,6 @@
 [VI]:README.vi.md
 [ZH_CN]:README.zh_cn.md
 [ZH_TW]:README.zh_tw.md
-[NL]:README.nl.md
 
 Codul sursă original al computerului de orientare Apollo 11 (AGC) pentru modulul de comandă (Comanche055) și modulul lunar (Luminary099). Digitalizat de persoanele de la [Virtual AGC][3] și [MIT Museum][4]. Scopul este de a avea un repo pentru codul sursă original Apollo 11. Prin urmare, PR-urile sunt bine venite pentru orice problemă identificată între transcrierile din acest repository și scanările originale pentru [Luminary 099][5] și [Comanche 055][6], precum și pentru alte fișiere pe care aș fi putut să le uit.
 

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 Оригинальный исходный код бортового управляющего компьютера Аполлон 11 (AGC) для командного модуля (Comanche055) и лунного модуля (Luminary099). Оцифровано людьми из [Virtual AGC][3] и [MIT Museum][4]. Цель - это создание репозитория с оригинальным исходным кодом миссии Аполлон 11. Таким образом приветствуются pull requests (PRs) с исправлениями для любых найденных ошибок в файлах этого репозитория и оригинальных сканах исходного кода для [Luminary 099][5] и [Comanche 055][6], так же как и для любых файлов, которые я мог пропустить.
 

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 [Italiano][IT],
 [Kurdi][KU],
 [Nederlands][NL],
+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 **Türkçe**,
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
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 [한국어][KO_KR]
 
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 Orijinal Apollo 11 Yönlendirme Bilgisayarı'nın (AGC) Yönetim Modülü (Comanche055) ve Ay Modülü (Luminary099)'nün kaynak kodu. [Virtual AGC][3] ve [MIT Museum][4] çalışanları tarafından sayısallaştırılmıştır. Amaç orijinal Apollo 11 kaynak kodunu içeren bir repo oluşturmak. Bu yüzden bu repoda, [Luminary 099][5]'de ve [Comanche 055][6]'da tespit edilen hatalarla ilgili veya benim kaçırdığım herhangi bir dosya hakkında yollanacak pull request'lere açığız.
 

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 [Italiano][IT],
 [Kurdi][KU],
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+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 **Tiếng Việt**,
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
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 Mã nguồn của máy tính hướng dẫn Apollo 11 (AGC) thông qua Command Module (Comanche055) và Lunar Module (Luminary099). Được số hóa bởi những người ở [Virtual AGC][3] và [Bảo tàng MIT][4]. Mục tiêu là tạo ra một kho lưu trữ mã nguồn cho Apollo 11. Do vậy, PRs là một điều bình thường cho bất kì một vấn đề được xác định giữa các bản dịch trong kho lưu trữ này và nguồn gốc quét mã cho [Luminary 099][5] và [Comanche 055][6], cũng như bất kì file nào mà chúng tôi có thể bỏ lỡ.
 

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 [Italiano][IT],
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+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
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 [မြန်မာ][MM],
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 阿波罗 11 号制导计算机（AGC）中指令模块（Comanche055）和登月模块（Luminary099）原始代码。由 [虚拟 AGC][3] 和 [MIT 科学博物馆][4] 的伙计们完成电子化。本仓库存在的目的是存储阿波罗 11 号原始代码。当然，倘若在本仓库或原始代码扫描件 [Luminary 099][5] 及 [Comanche 055][6] 发现问题，或者任何我可能漏掉的文件，欢迎提交 PR。
 

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 [Italiano][IT],
 [Kurdi][KU],
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+[Norsk][NO],
 [Polski][PL],
 [Português][PT_BR],
 [Română][RO],
 [Tiếng Việt][VI],
 [Türkçe][TR],
+[Ελληνικά][GR],
 [Русский][RU],
 [العربية][AR],
 [فارسی][FA],
 [हिंदी][HI_IN],
+[অসমীয়া][AS_IN],
 [বাংলা][BD_BN],
 [မြန်မာ][MM],
 [日本語][JA],
@@ -33,6 +36,7 @@
 [한국어][KO_KR]
 
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 最初用於阿波羅 11 號的導航電腦 (Apollo 11 Guidance computer, AGC) 裡頭駕駛艙 (Comanche055) 和登月艙 (Luminary099) 的原始程式碼，由 [Virtual AGC](http://www.ibiblio.org/apollo/) 及 [MIT Museum](http://web.mit.edu/museum/) 的工作人員進行數位化，著眼於建立阿波羅 11 號原始程式碼的封存。正因如此，若您發現文件抄錄或於查看 [Luminary 099](http://www.ibiblio.org/apollo/ScansForConversion/Luminary099/) 和 [Comanche 055](http://www.ibiblio.org/apollo/ScansForConversion/Comanche055/) 這兩部分原始程式碼過程中遇到問題的話，歡迎提交 pull request。當然，也包括那些我可能遺忘的檔案。