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Proof GROUND_TRACKING_DETERMINATION_PROGRAM (closes #210) (#312)

pull/328/head
Glenn Dwiyatcita 2018-04-02 12:19:34 +02:00 committed by James Harris
parent d04fea42dc
commit c8fa53b43d
1 changed files with 43 additions and 42 deletions
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85
Comanche055/GROUND_TRACKING_DETERMINATION_PROGRAM.agc
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@ -29,59 +29,61 @@
# Please report any errors to info@sandroid.org.
# Page 456
# GROUND TRACKING DETERMINATION PROGRAM -- P21
#
# GROUND TRACKING DETERMINATION PROGRAM P21
# PROGRAM DESCRIPTION
# MOD NO -- 1
# MOD BY -- N. M. NEVILLE
# MOD NO - 1
# MOD BY - N.M.NEVILLE
# FUNCTIONAL DECRIPTION-
#
# FUNCTIONAL DESCRIPTION --
# TO PROVIDE THE ASTRONAUT DETAILS OF THE LM OR CSM GROUND TRACK WITHOUT
# THE NEED FOR GROUND COMMUNICATION (REQUESTED BY DSKY).
# TO PROVIDE THE ASTRONAUT DETAILS OF THE LM OR CSM GROUND TRACK WITHOUT
# THE NEED FOR GROUND COMMUNICATION (REQUESTED BY DSKY).
# CALLING SEQUENCE -
#
# CALLING SEQUENCE --
# ASTRONAUT REQUEST THROUGH DSKY V37E21E
# ASTRONAUT REQUEST THROUGH DSKY V37E21E
# SUBROUTINES CALLED-
#
# SUBROUTINES CALLED --
# GOPERF4
# GOFLASH
# THISPREC
# OTHPREC
# LAT-LONG
# GOPERF4
# GOFLASH
# THISPREC
# OTHPREC
# LAT-LONG
# NORMAL EXIT MODES-
#
# NORMAL EXIT MODES --
# ASTRONAUT REQUEST THROUGH DSKY TO TERMINATE PROGRAM V34E
# ASTRONAUT REQUEST THROUGH DSKY TO TERMINATE PROGRAM V34E
# ALARM OR ABORT EXIT MODES-
#
# ALARM OR ABORT EXIT MODES --
# NONE
#
# OUTPUT --
# OCTAL DISPLAY OF OPTION CODE AND VEHICLE WHOSE GROUND TRACK IS TO BE
# COMPUTED
# OPTION CODE 00002
# THIS 00001
# OTHER 00002
# DECIMAL DISPLAY OF TIME TO BE INTEGRATED TO HOURS , MINUTES , SECONDS
# DECIMAL DISPLAY OF LAT,LONG,ALT
# NONE
# OUTPUT -
#
# OCTAL DISPLAY OF OPTION CODE AND VEHICLE WHOSE GROUND TRACK IS TO BE
# COMPUTED
# OPTION CODE 00002
# THIS 00001
# OTHER 00002
# DECIMAL DISPLAY OF TIME TO BE INTEGRATED TO HOURS , MINUTES , SECONDS
# DECIMAL DISPLAY OF LAT,LONG,ALT
# ERASABLE INITIALIZATION REQUIRED
# AX0 2DEC 4.652459653 E-5 RADIANS "68-69 CONSTANTS"
# -AY0 2DEC 2.147535898 E-5 RADIANS
# AZ0 2DEC .7753206164 REVOLUTIONS
# FOR LUNAR ORBITS 504LM VECTOR IS NEEDED
# 504LM 2DEC -2.700340600 E-5 RADIANS
# 504LM _2 2DEC -7.514128400 E-4 RADIANS
# 504LM _4 2DEC _2.553198641 E-4 RADIANS
#
# NONE
# AX0 2DEC 4.652459653 E-5 RADIANS "68-69 CONSTANTS"
#
# -AY0 2DEC 2.147535898 E-5 RADIANS
#
# AZ0 2DEC .7753206164 REVOLUTIONS
# FOR LUNAR ORBITS 504LM VECTOR IS NEEDED
#
# 504LM 2DEC -2.700340600 E-5 RADIANS
#
# 504LM _2 2DEC -7.514128400 E-4 RADIANS
#
# 504LM _4 2DEC _2.553198641 E-4 RADIANS
#
# NONE
# DEBRIS
# Page 457
# CENTRALS -- A,Q,L
# OTHER -- THOSE USED BY THE ABOVE LISTED SUBROUTINES
# SEE LEMPREC, LAT-LONG
# CENTRALS-A,Q,L
# OTHER-THOSE USED BY THE ABOVE LISTED SUBROUTINES
# SEE LEMPREC,LAT-LONG
SBANK= LOWSUPER # FOR LOW 2CADR'S.
BANK 33
@ -92,7 +94,7 @@
COUNT 24/P21
PROG21 CAF ONE
TS OPTION2 # ASSUMED VEHICLE IS LM, R2 = 00001
TS OPTION2 # ASSUMED VEHICLE IS LM , R2 = 00001
CAF BIT2 # OPTION 2
TC BANKCALL
CADR GOPERF4
@ -193,7 +195,6 @@ P21DSP CLEAR SLOAD # GENERATE DISPLAY DATA
STORE DSPTEM1
RTB
P21PROG1
600SEC 2DEC 60000 # 10 MIN
P21ONENN OCT 00001 # NEEDED TO DETERMINE VEHICLE