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Apollo-11/Comanche055/CM_ENTRY_DIGITAL_AUTOPILOT.agc

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# Copyright: Public domain.
# Filename: CM_ENTRY_DIGITAL_AUTOPILOT.agc
# Purpose: Part of the source code for Colossus 2A, AKA Comanche 055.
# It is part of the source code for the Command Module's (CM)
# Apollo Guidance Computer (AGC), for Apollo 11.
# Assembler: yaYUL
# Contact: Ron Burkey <info@sandroid.org>.
# Website: www.ibiblio.org/apollo.
# Pages: 1063-1092
# Mod history: 2009-05-13 RSB Adapted from the Colossus249/ file of the
# same name, using Comanche055 page images.
# 2009-05-20 RSB Corrections: Removed an extraneous label
# EXDAPIN, added a missing instruction in
# COMPAT.
#
# 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. The images (with suitable reduction in storage size and
# consequent reduction in image quality as well) are available online at
# www.ibiblio.org/apollo. If for some reason you find that the images are
# illegible, contact me at info@sandroid.org about getting access to the
# (much) higher-quality images which Paul actually created.
#
# Notations on the hardcopy document read, in part:
#
# Assemble revision 055 of AGC program Comanche by NASA
# 2021113-051. 10:28 APR. 1, 1969
#
# This AGC program shall also be referred to as
# Colossus 2A
# Page 1063
# SUBROUTINE TO READ GIMBAL ANGLES AND FORM DIFFERENCES. GIMBAL ANGLES ARE SAVED IN 2S COMPLEMENT, BUT THE
# DIFFERENCES ARE IN 1S COMP. ENTER AND READ ANGLES EACH .1 SEC.
#
# CM/DSTBY = 1 FOR DAP OPERATION
# CM/DSTBY = 0 TO TERMINATE DAP OPERATION.
BANK 15
SETLOC ETRYDAP
BANK
COUNT 15/DAPEN
EBANK= AOG
READGYMB CA TEN # KEEP RESTART DT GOING RELATIVE TO
ADS CM/GYMDT # PIPTIME. (GROUP 6)
# IF A RESTART OCCURS, SKIP PRESENT CYCLE. THE
# PHASCHNG PROTECTION IS IN CM/DAPIC.
CA BIT6 # CHECK FOR FINE ALIGN MODE OF CDU.
MASK IMODES33 # ( PROTECT AOG/PIP ETC AS WELL AS
EXTEND # GIMBAL DIFFERENCES)
BZF READGYM1 # OK
CS BIT1 # NOT IN FINE ALIGN, SO IDLE.
MASK CM/FLAGS # SET GYMDIFSW = 0
TS CM/FLAGS
TC FLUSHJET # QUENCH JETS, SINCE MAY BE A WHILE.
TC CM/GYMIC +2
READGYM1 CA CDUX
XCH AOG
EXTEND
MSU AOG # -DELAOG=AOG(N-1) - AOG(N)
TS -DELAOG
CA CDUY
XCH AIG
EXTEND
MSU AIG
TS -DELAIG
CA CDUZ
XCH AMG
EXTEND
MSU AMG
TS -DELAMG
# Page 1064
DOBRATE? CS CM/FLAGS # CM/DSTBY=103D BIT2 GYMDIFSW=104D BIT1
MASK THREE
INDEX A
TC +1
TC DOBRATE # OK, GO ON
TC CM/GYMIC # DONT CALC BODYRATE ON FIRST PASS.
NOOP
TC FLUSHJET # TURN OFF ALL JETS
TC PHASCHNG
OCT 00006 # DEACTIVATE DAP GROUP 6.
TC TASKOVER
DOBRATE CA ONE # DO BODYRATE
DOBRATE1 TS JETEM # SKIP BODYRATE.
CA TEN # KEEP CDU READ GOING.
TC WAITLIST
EBANK= AOG
2CADR READGYMB
# DOES NOT PROTECT TEMK, SQ IN SPSIN/COS
CCS JETEM
TC BODYRATE
TC TASKOVER # SKIP CALC ON INITIAL PASS. (PASSES)
CM/GYMIC ADS CM/FLAGS # GYMDIFSW: C(A)=1, KNOW BIT IS 0
CAF ZERO
TS JETAG
TS OLDELP
TS OLDELQ
TS OLDELR
TS GAMDOT # NO GYM DIF, PROB NO GAM DIF.
TC DOBRATE1
# Page 1065
# COME HERE TO CORRECT FOR OVERFLOW IN ANGULAR CALCULATIONS
ANGOVCOR TS L # THIS COSTS 2 MCT TO USE.
TC Q # NO OVFL
INDEX A
CAF LIMITS
ADS L
TC Q
BLOCK 3
COUNT 03/DAPEN
FLUSHJET CA 7 # COME HERE TO TURN OFF ALL JETS.
EXTEND
WRITE ROLLJETS # ZERO CHANNEL 6
EXTEND
WRITE PYJETS # ZERO CHANNEL 5
TC Q
BANK 15
COUNT 15/DAPEN
SETLOC ETRYDAP
BANK
RATEAVG COM # SUBROUTINE TO ESTIMATE RATES IN PRESENCE
AD JETEM # OF CONSTANT ACCELERATION.
EXTEND
MP HALF # DELV (EST) = DELV +(DELV-OLDELV)/2
AD JETEM
TC Q
# Page 1066
# THESE ARE CALLED FOR THE VARIOUS INITIALIZATIONS NEEDED.
BANK 20
SETLOC DAPS1
BANK
COUNT 20/DAPEN
EBANK= AOG
CM/DAPON CA EBAOG
TS EBANK
TC DOWNFLAG # RESET DAPBIT1. T5 RESTART IDENTIFIER.
ADRES DAPBIT1 # BIT 15 FLAG 6 CM FLAGS.
TC DOWNFLAG # RESET DAPBIT2
ADRES DAPBIT2 # BIT 14 FLAG 6
EXTEND
DCA T5IDLER1 # DISABLE RCS CALCULATION
DXCH T5LOC
EXTEND
DCA T5IDLER1 # DISABLE RCS JET CALLS
DXCH T6LOC
TC FLUSHJET # JETS DEPARTED ON SM. ZERO JET BITS.
CS 13,14,15
MASK DAPDATR1 # SET CONFIG BITS =0 FOR ENTRY
TS DAPDATR1
TC +4
NOTYET CA .5SEC
TC BANKCALL
CADR DELAYJOB # (DELAYJOB DOES INHINT)
+4 CA BIT11 # GAMDIFSW = 94D BIT11, INITLY=0
MASK CM/FLAGS # IF ZERO, WAIT UNTIL CM/POSE UPDATE.
EXTEND
BZF NOTYET
CS ONE # ACTIVATE CM/DAP
TS RCSFLAGS # USE BIT3 TO INITIALIZE NEEDLER ON
# NEXT PASS.
TS P63FLAG # SO WAKEP62 WILL NOT BE INITIATED UNTIL
# HEADSUP IS SET IN P62.
# FLAG TO PREVENT MULTIPLE CALLS TO WAKEP62.
CA 7
TS JETAG
TS PAXERR1 # KEEP NEEDLES ZERO UNTIL DAP UPDATE
# IN CASE CMDAPMOD IS NOT +1.
# Page 1067
INHINT
EXTEND
DCA ALFA/180 # DO ATTITUDE HOLD UNTIL KEYBOARD
DXCH ALFACOM # ESTABLISHES HEADSUP.
CA ROLL/180
TS ROLLHOLD # FOR ATTITUDE HOLD IN MODE +1.
EXTEND
MP HALF
TS ROLLC # NOT INTERESTED IN LO WORD.
CS CM/FLAGS
MASK BIT12 # CMDAPARM =93D BIT12 INITLY=0
ADS CM/FLAGS # SET BIT TO 1.
CS FLAGWRD2 # SET NODOFLAG TO PREVENT FURTHER
MASK BIT1 # V 37 ENTRIES.
ADS FLAGWRD2
RELINT
TC POSTJUMP
CADR P62.1
# Page 1068
# INITIALIZE CM/DAP. WAITLIST CALL FOR READGYMB. SET SWITCH CM/DSTBY =1
# SO READACCS WILL ENTER A WTLST CALL FOR SETJTAG .
# CMDAPARM = 0, SO ONLY BODY RATE AND ATTITUDE CALCULATIONS ARE DONE.
# SET AVEGEXIT TO CONTINUE AT CM/POSE
CM/DAPIC CA EBAOG
TS EBANK
INHINT
CM/DAP2C CS PIPTIME +1
# PRIO OF P62 L PRIO AVG.:PIPTM=PIPTM1
TS JETEM
CA POS1/2
AD POS1/2
AD TIME1 # OVFL GUARANTEED
ADS JETEM # C(A) = DELTA TIME SINCE PIPUP
CS FIVE
AD JETEM
CCS A
AD -CDUT+1
TCF -2
NOOP
AD ONE # SEND NO ZERO TO WTLST
TS CM/GYMDT # FOR RESTART
TC WAITLIST
EBANK= AOG
2CADR READGYMB
CS CM/SWIC1 # GAMDIFSW, GYMDIFSW, CM/DSTBY
MASK CM/FLAGS # DAPARM, .05GSW, LATSW, ENTRYDSP
AD CM/SWIC2 # SET CM/DSTBY, LATSW
# DISABLE ENTRY DISPLAY, SINCE DES. GIMB.
# CALC. (P62.3) GOES TO ENDEXIT.
TS CM/FLAGS
CA 7
TS BETA/180 # NECESSARY: NO OVFL CORRECTION
CA ONE # INITIALIZE THE TM OF BODY RATES VIA
TS SW/NDX # UPBUFF.
TC 2PHSCHNG # DOES INHINT/RELINT
OCT 40116 # SAVE TBASE6
OCT 05024
OCT 13000
TC POSTJUMP
# Page 1069
CADR P62.2
CM/SWIC1 OCT 16017
CM/SWIC2 = TEN # 00012 : CM/DSTBY, LATSW
-CDUT+1 OCT 77766
EBANK= T5LOC
T5IDLER1 2CADR T5IDLOC
# Page 1070
# THIS SECTION CALCULATES THE ANGULAR BODY RATES EACH .1 SEC. THE ANGULAR RATES ARE THOSE ALONG THE BODY AXES
# XB, YB, ZB, AND ARE NORMALLY DESIGNATED P, Q, R. REQUIREMENT: TEMPORARY ERASE. JETEM, JETEM +1
#
# SINCE RESTARTS ZERO THE JET OUTPUT CHANNELS, NO ATTEMPT IS MADE TO RESTART THE ENTRY DAPS. THAT IS,
# THE 0.1 SEC DAPS WILL MISS A CYCLE, AND WILL PICK UP AT THE NEXT 0.1 SEC UPDATE. MOST OF THE TIME THE 2 SEC
# ROLL SYSTEM WILL MISS ONLY 0.1 SEC OF CONTROL. HOWEVER, IF THE RESTART OCCURS AFTER THE SECTION TIMETST HAS
# STARTED, THEN THE ROLL SYSTEM WILL MISS ONE CYCLE.
# THIS IS NECESSARY UNDER THE GROUNDRULE THAT NO JET COMMANDS SHALL BE LESS THAN 14 MS.
EBANK= AOG
BANK 15
SETLOC ETRYDAP
BANK
COUNT 15/DAPEN
BODYRATE CA AMG # THESE ARE 2S COMPL NOS, BUT USE ANYWAY.
TC SPCOS
TS COSM
CA AOG # C(AOG) = AOG/180
TC SPSIN # SINO
TS SINO # SINO = SIN(AOG)
EXTEND
MP COSM
TS SINOCOSM # SO CM
CA AOG
TC SPCOS # COSO
TS COSO
EXTEND
MP COSM
TS COSOCOSM # CO CM
# PITCHDOT: Q TCDU/180 = IDOT TCDU/180 COSO COSM + MDOT TCDU/180 SINO
CS -DELAMG
EXTEND
MP SINO
DXCH JETEM # 2 LOCS
CS -DELAIG
EXTEND
MP COSOCOSM
DAS JETEM
CA JETEM
XCH OLDELQ
TC RATEAVG
TS QREL # PITCHDOT = Q TCDU/180
# Page 1071
# YAWDOT: R TCDU/180 = -IDOT TCDU/180 COSM SINO + MDOT TCDU/180 COSO
CS -DELAMG
EXTEND
MP COSO
DXCH JETEM
CA -DELAIG
EXTEND
MP SINOCOSM
DAS JETEM
CA JETEM
XCH OLDELR
TC RATEAVG
TS RREL # YAWDOT = R TCDU/180
# ROLLDOT: P TCDU/180 = ODOT TCDU/180 + IDOT TCDU/180 SINM
CA AMG
TC SPSIN
TS SINM
EXTEND
MP -DELAIG
TS JETEM
CA ZERO
DDOUBL # ROUND L INTO A
AD -DELAOG
AD JETEM
CS A
TS JETEM
XCH OLDELP
TC RATEAVG
TS PREL # ROLLDOT = P TCDU/180
# IF GAMDOT < 0.5 DEG/SEC, THEN GAMDOT =0
CCS GAMDOT
TC +2
TC NOGAMDUT
CS ROLL/180
TC SPSIN
EXTEND
MP GAMDOT
TS JETEM +1 # -SR GAMDOT
EXTEND
MP SINTRIM # SIN(-20) (FOR NOMINAL L/D = .3)
ADS PREL # PREL TCDU/180=(P-SALF SR GAMDOT)TCDU/180
CA ROLL/180
TC SPCOS
# Page 1072
COM
EXTEND
MP GAMDOT
ADS QREL # QREL TCDU/180=(Q-CR GAMDOT) TCDU/180
CS JETEM +1 # B( ) = -SR GAMDOT
EXTEND
MP COSTRIM # COS(-20) (FOR NOMINAL L/D = .3)
ADS RREL # RREL TCDU/180=(R+CALF SR GAMDOT)TCDU/180
NOGAMDUT CA BIT12 # CMDAPARM = 93D BIT 12
MASK CM/FLAGS
EXTEND
STBYDUMP BZF TASKOVER # DAP NOT ARMED.
CA POSMAX # PICK UP AT ATTRATES IN 10 MS OR SO.
TS TIME5
EXTEND
DCA ATDOTCAD
DXCH T5LOC
# DOES NOT PROTECT TEMK, SQ IN SPSIN/COS
TC TASKOVER
EBANK= AOG
ATDOTCAD 2CADR ATTRATES
# Page 1073
# CALCULATE BODY ATTITUDE RATES AND INTEGRATE TO OBTAIN ATTITUDE ANGLES.
#
# CB PHIDOT TCDU/180 = (CA PREL + SA RREL) TCDU/180
# BETADOT TCDU/180 = (-SA PREL + CA RREL) TCDU/180
# ALFADOT TCDU = (QREL + SB PHIDOT) TCDU/180
ATTRATES LXCH BANKRUPT # CONTINUE HERE VIA T5
EXTEND # TASK MAY BE SKIPPED AT RESTART.
QXCH QRUPT
CA SR
DOUBLE
TS CM/SAVE
# DOES NOT PROTECT TEMK, SQ IN SPSIN/COS
CA QREL
AD ALFA/180
TC ANGOVCOR
TS ALFA/180
TC SPCOS
TS CALFA # CALFA
TS PHIDOT
EXTEND
MP PREL
XCH PHIDOT # CA PREL
EXTEND
MP RREL # CA RREL
TS BETADOT
CA ALFA/180
TC SPSIN
TS SALFA # SIN(ALFA)
EXTEND
MP RREL # SA RREL
ADS PHIDOT # CB PHIDOT, SAVED.
CS SALFA
EXTEND
MP PREL
ADS BETADOT # SAVE BETADOT TCDU/180
ADS BETA/180 # BETA DONE.
TC SPSIN
EXTEND
MP PHIDOT # NEGLECT CB IN CB PHIDOT
AD ALFA/180
TC ANGOVCOR
TS ALFA/180 # ALFA DONE.
# Page 1074
COM
AD ALFACOM
TC ANGOVCOR # JUST IN CASE ...
TS AK1
TS QAXERR # FOR PITCH FDAI AND EDIT.
CA PHIDOT # PHIDOT TCDU/180, NEGLECTING CB
AD ROLL/180
TC ANGOVCOR
TS ROLLTM # ROLL/180 FOR TM.
TS ROLL/180 # ROLL DONE.
# START YAW AUTOPILOT HERE. RATE DAMPING WITH ENFORCED COORDINATED ROLL MANEUVER.
CS BETA/180 # IF IN ATM, SAVE 'RAXERR' FOR TM DNLST.
AD BETACOM
TS RAXERR # IF OUTSIDE ATM, USE TM REGISTER 'RAXERR'
# AS A TEMPORARY. (DAP OPERATION IS IN INTERRUPT, SO
# IS OK.) FINAL C(RAXERR) AT END OF DAP CYCLE WILL
# BE R-AXIS ERROR.
CA BIT3 # .05GSW = 102D BIT3 SW=0, LESS .05G
MASK CM/FLAGS # SWITCH =1, GREATER THAN .05 G
EXTEND
BZF EXDAP # IF G LESS THAN .05
CS ONE # IF G GEQ THAN .05
TS CMDAPMOD # SAVE -1 FOR USE IN CM/RCS
TS AK1 # TO ZERO PITCH AND YAW FDAI NEEDLES
TS AK2 # IN ATM. (MODE =-1)
CS PREL # YAW ERROR = RREL - PREL TAN(ALFA)
EXTEND
MP SINTRIM # LET SIN(-20) BE APPROX FOR TAN(-20)
AD RREL
TC 2D/SDZ # GO TEST DZ. GET TAG: +0 IF IN DZ
INDEX A # +/- 1 IF NOT
CAF YJETCODE
TS JETEM
# START PITCH AUTOPILOT HERE. RATE DAMPING ONLY.
CA QREL
TC 2D/SDZ
EXDAPIN INDEX A # COME HERE FROM EX ATM DAP
CAF P/RJCODE
ADS JETEM # COMBINE ALL NEW BITS.
EXTEND # DOES NOT REQUIRE SAVING OLD CODES.
# Page 1075
WRITE PYJETS # SET PYCHAN TO DESIRED BIT CONFIG.
CCS JETAG
TC CM/RCS
TC CM/FDAI
TC CM/FDAIR -1 # (JETAG=-1 EQUIVALENT TO CMDAPMOD=+1)
# Page 1076
# DEAD ZONE LOGIC USED BY ENTRY DIGITAL AUTOPILOTS.
3DDZ CCS A # YAWLIM=1.0-3/180=16384-273=16111
AD YAWLIM
TCF DZCOM
AD YAWLIM
TCF DZNOCOM
# BIASED DZ FOR EXT ATM DAP.
BIASEDZ TS JETEM2 # SAVE RATE/180. ERROR/180 IS IN L.
CCS A # START ERROR DZ.
CS CM/BIAS # = .6/180
TCF +2
CA CM/BIAS
AD L # BIAS THE ERROR.
LXCH Q # SAVE CALLERS RETURN ADDRESS.
TC 3DDZ # GO GENERATE THE ERROR BIT.
DXCH L # BIT TO L, RESTORE CALLERS Q.
4D/SDZ CCS JETEM2 # CAME HERE IN EXT ATM. C(L) = ERROR BIT
AD 4D/SLIM # IF RATE GEQ 4D/S, SET L=0 AND TAKE
TCF +2 # JET BITS ACCORDING TO SGN OF RATE.
AD 4D/SLIM
TS A
TCF +2 # RATE OK. CONTINUE
ZL # RATE GEQ 4 D/S. OVER RIDE ERROR BIT
XCH JETEM2 # AND CONTINUE TO GET SIGN.
2D/SDZ CCS A # COME HERE TO TEST IF A WITHIN 2DEG/S DZ
AD YDOTLIM # 1.0 - YDOT DZ (OR PDOT)
TCF +3
AD YDOTLIM # YDOT DZ = 2 DEG/SEC
DZCOM COM
DZNOCOM TS JETEM +1 # GENERATE TAG, SET C(A)= -+1 OUTSIDE DZ
CA ZERO # SET C(A) = +0 INSIDE
TC Q
# Page 1077
# EXTRA ATMOSPHERIC DIGITAL AUTOPILOT
#
# 1. IF ABS(CALF) -C(45) POS, USE IF CALFA POS, CMDAPMOD= +0
# BETA: YAW ERROR = SGN(CALF) (BETACOM -BETA) IF CALFA NEG, CMDAPMOD= -0
# RATE = BETADOT IF CMDAPMOD = -0, RATE = RREL
# R-AXIS = CONTROL
#
# ROLL: ROLL ERROR = SGN(CALF) (ROLLC - ROLL) IF CMDAPMOD = -0, RATE DAMP ONLY.
# RATE = PREL
# P-AXIS = CONTROL
#
# 2. IF C(45) GEQ CALFA GEQ -C(45), USE CMDAPMOD = +1
# BETA: ROLL ERROR = SGN(-SALF) (BETACOM -BETA)
# RATE = BETADOT
# P-AXIS = CONTROL
#
# ROLL: YAW ERROR = SGN(SALF) (ROLLC - ROLL) RATE DAMP ONLY.
# RATE = RREL
# R-AXIS = CONTROL
#
# 3. FOR ALL CASES, USE
# ALFA: PITCH ERROR = (ALFACOM - ALFA)
# RATE = QREL
# Q-AXIS = CONTROL
EXDAP TS CMDAPMOD # +0 FOR NOW
CCS CALFA
AD C45LIM # =1.0-COS(45)
TCF +2
AD C45LIM
TS A
TCF EXDAP2 # HERE IF ABS(CALFA) L COS(45)
CCS CALFA # |CALFA| > 0.707
TCF +1 # CONTINUE IF POS; GO TO EXDAP4 IF NEG.
CCS P63FLAG # VALID VALUES ARE: -1, +1, +0.
TC EXDAP4
TC +2
TC EXDAP4
TC PHASCHNG # SINGLE PASS THROUGH HERE.
OCT 40334
CS ONE
TS P63FLAG # SET FLAG TO ASSURE SINGLE PASS.
CA NSEC
TC WAITLIST
EBANK= AOG
2CADR WAKEP62 # CALL TO TERMINATE P62 IN N SEC.
# Page 1078
# 65 DEG/ 3DEG/SEC = 21 SEC NOMINAL
# TRANSIT TIME FROM ALFA=45 TO ALFA TRIM.
EXDAP4 CCS JETAG # ROLLJET INTERFACE TEST BETWEEN .1 SEC
TCF EXDAP3 # DAP AND THE 2 SEC CM/RCS DAP
TCF EXDAP3
CA ZERO
EXTEND # TURN OFF ROLL JETS IF ON AND WAIT
WRITE ROLLJETS # UNTIL START OF 2 SEC CM/RCS CYCLE
TS JETAG # RESTORE PROPER VALUE +0
# ROLL FDAI WILL BE IN ERROR UNTIL NEXT CM/RCS CALL.
EXDAP3 CCS CALFA # HERE IF ABS(CALFA) GEQ COS(45)
CA RAXERR # C()= BETACOM - BETA/180
TCF EXDAP1
CS ZERO
TS CMDAPMOD # FOR CM/RCS
CS RAXERR # COMPLEMENT OF YAW ERROR.
EXDAP1 TS RAXERR # FOR YAW FDAI
TS AK2 # WANT RAXERR FOR TM.
TS L
CCS CMDAPMOD # COORDINATE BETA CONTROL.
TC +3 # C(CMDAPMOD) CAN BE +1, +0, OR -0.
CA ONE # USE BETADOT TO COORD IN MODE +0
INDEX A # OTHERWISE USE RREL.
CA RREL
TC BIASEDZ # GO TEST DZ. +0 IF IN DZ, +-1 OTHERWISE
# IF GEQ 4D/S, SET ERROR BIT IN L=0
EXTEND
ROR LCHAN # L HAS BETA BIT
INDEX A
CAF YJETCODE
TS JETEM
CA QAXERR # ALFA ERROR.
TS L
CA QREL # FOR ALPHADOT USE QREL
TC BIASEDZ
EXTEND
ROR LCHAN
TCF EXDAPIN # CONTINUE ON IN DAP
EXDAP2 INCR CMDAPMOD # SET CMDAPMOD TO +1
CS ONE # INDICATE CHANGE FROM .1 SEC UPDATE TO
TS JETAG # TO 2 SEC FOR ROLL JETS. (IF CMDAPMOD
# =0 AND JETAG =-1, QUENCHES JETS IF ON)
CCS P63FLAG # IF FLAG WAS +1, SET =0.
TS P63FLAG
# Page 1079
NOOP
CCS SALFA # BETA CONTROL WITH P JETS
CS RAXERR # B()= BETACOM - BETA/180
TCF +2
CA RAXERR
TS PAXERR1 # TEMP SAVE. ERROR/180
EXTEND
MP HALF # CM/FDAI EXPECTS ERROR/360.
XCH PAXERR1 # ERROR/360 FOR FDAI, GET ERROR/180.
TS L
CCS SALFA
CS BETADOT # USE BETADOT TO COORD IN MODE +1
TC +2
CA BETADOT
TC BIASEDZ
EXTEND
ROR LCHAN
INDEX A
CAF P/RJCODE # GET ROLL CODE
EXTEND # ROLL CONTROL WITH YAW JETS.
WRITE ROLLJETS # WE,LL SKIP REGULAR ROLL SYST
CA ROLLHOLD # ROLL/180 AT CM/DAPON TIME.
EXTEND
MSU ROLL/180 # 1,S COMPL, BUT SO WHATS A BIT.?
TS L # FORCE A LIMIT CYCLE IN YAW RATE.
CCS SALFA
CA L # TO REMOVE ITS BIASING EFFECT ON M DOT.
TC EXDAP1
CS L
TC EXDAP1
NSEC DEC 2100 # 65 DEG/ 3 DEG/SEC
# IF NSEC IS CHANGED, REMEMBER TO CHANGE 4.33SPOT.
4D/SLIM DEC 16348 # 1.0 -4/180 D/S = 4/1800 EXP 14
YDOTLIM DEC 16366 # =1.0 - YDOT DZ= 16384 -18
# YDOT DZ = YDOT TCDU/180 = 2/1800 EXP 14
CM/BIAS DEC 55 # =.6/180 B14 = 55
YAWLIM DEC 16055 # YAWLIM=1.0-3.6/180=16384-329=16055
C45LIM DEC .29289 # =1.0-COS(45)
SINTRIM DEC -.34202 # SIN(-20) (FOR NOMINAL L/D = .3)
COSTRIM DEC .93969 # COS(-20) (FOR NOMINAL L/D = .3)
# TO MAKE DAP INSENSITIVE TO PITCH ERRORS DUE TO ACCUMULATED NAV ERRORS, USE NOMINAL VALUE (-20 DEG) FOR TRIM ALFA
# USED DURING ATMOSPHERIC COORDINATION. OUTSIDE ATMOSPHERE, NAV ERRORS WILL BE SLIGHT, BUT ALFA CAN DIFFER GREATLY
# FROM TRIM, SO USE ON-BOARD ESTIMATES.
# Page 1080
# JET CODE TABLES FOLLOW _
OCTAL 00120 # POS Y
YJETCODE OCTAL 00000 # RCS JET BITS
OCTAL 00240 # NEG Y
OCTAL 00005 # POS R JET BITS ALSO POS P JET BITS
P/RJCODE OCTAL 00000
OCTAL 00012 # NEG R ALSO NEG P
# Page 1081
# RCS THIS SECTION IS ENTERED EACH 2 SEC BY WAITLIST CALL FOLLOWING A DELAY OF 1.2 SEC AFTER PIPUP.
# THE TASK SETJTAG SETS A FLAG IN JETAG TO SIGNIFY THAT ROLL UPDATE IS DUE. IN ROUGHLY 5 CS BPDYRATE WILL BE
# EXECUTED AND JETAG WILL CAUSE CM/RCS TO ACT ON ROLLC IMMEDIATELY THEREAFTER. THE
# TASK SAVES THE CALL TIME SO THAT CM/RCS CAN DETERMINE HOW MUCH OF THE 2 SEC INTERVAL REMAINS BEFORE THE
# NEXT UPDATE.
SETJTAG CS TIME1 # SAVE NOMINAL UPDATE TIME FOR SYNCH
TS TUSED
# THE 5 CS APPEARS IN TIMETST.
CA ONE # RATHER THAN INCR, FOR SAFETY
TS JETAG # SET JETAG=1 TO CAUSE CM/RCS TO BE
TC PHASCHNG
OCT 00001
TC TASKOVER # EXECUTED AFTER NEXT BODYRATE UPDATE
# PREDICTIVE ROLL SYSTEM ENTRY STEERING PROVIDES ROLL COMMAND IN LOC ROLLC. THE FOLLOWING CALCULATES THE
# TRAJECTORY TO THE ORIGIN IN PHASE PLANE (X,V). PROGRAM ENTERS JET ON AND OFF CALLS INTO WTLST TO PRODUCE
# THE DESIRED TRAJECTORY. ONLY THOSE CALLS WHICH CAN BE EXECUTED WITHIN THE INTERVAL T (2 SEC) ARE ENTERED IN
# WTLST, THE REMAINDER ARE RECONSIDERED AT NEXT UPDATE.
HALFPR EQUALS NEG1/2 +1
# CLEAR JETAG BEFORE TIMETST. SET TO +0 TO SHOW
# ROLL DAP CALLED. IN EVENT OF RESTART, BODYRATE
# MAY MISS A CYCLE. CM/RCS WILL MISS A CYCLE ONLY
# IF A RESTART OCCURS AFTER TIMETST COMMENCES.
CM/RCS CS ONE
TS JNDX # SET NDX FOR POS ROLL, AND CHANGE LATER
CS 2T/TCDU # ROLLDOT = DELAOG + DELAIG SINM =DELR
EXTEND
MP PREL # DELR/180 = RDOT TCDU/180 = RDOT/1800
AD L # -2 RDOT T/180 IN L
TS -VT/180 # SAVE -2VT/180 HERE
CS ROLL/180
TS SR # SAVE (-R/180) /2
CS CM/FLAGS
MASK BIT4 # LATSW = 101D BIT4
EXTEND # ROLL OVER TOP $
BZF GETLCX # NO, TAKE SHORTEST PATH
ADS CM/FLAGS # YES, ENFORCE ROLL OVER TOP.. (BIT =0)
CA ROLLC # (ROLLC/180) /2
AD SR # -(R/180) /2
XCH LCX/360 # DIFFERENT X REQD HERE. DISCONT AT 180.
TCF COMPAT # POSSIBLE OVFL ABOVE.
# Page 1082
GETLCX CA POS1/2 # FORM RCOM/360
DOUBLE
AD ROLLC
XCH LCX/360 # IGNORE POSSIBLE OVFL.
CA SR # FORM -R/360
AD NEG1/2
AD NEG1/2 # IGNORE OVFL
XCH LCX/360 # -R/360
ADS LCX/360 # LCX/360 = RCOM/360 -R/360 RANGE (-1,1)
# DOES SGN(-VT) (VT/180) (VT/180) (180/(4 A1 TT COSALFA)) + X/360 + SGN(X) / 2 OVFL ?
CCS -VT/180 # TAKE SHORTEST ANGULAR PATH
AD ONE # (BASED ON SINGLE JET ACCELERATION)
TCF +2
AD ONE
EXTEND
MP -VT/180 # C(-VT/180) = -2 VT/180
EXTEND
MP 1/16A1 # = 180/(16 A1 TT)
EXTEND
DV CALFA
TS L
CCS LCX/360
CAF POS1/2
TCF +2
CS POS1/2
AD LCX/360 # IS LCX/360 LESS THAN 180 DEGS $
AD L
TS L
TCF COMPAT # YES, GO ON.
TRTAGXPI INDEX A # NO, SHIFT X BY - SGN(X) 2 PI
CS HALFPR # +A YIELDS -1/2
DOUBLE
ADS LCX/360
COMPAT CA LCX/360 # CORRECT FOR ASSUMED COORD TURN.
EXTEND
MP CALFA # COS ALFA
TS LCX/360 # SCALED LCX OK HERE.
CCS CMDAPMOD # FOUR POSSIBILITIES HERE
TC DZCALL1 # EXIT, SETTING JETAG=0. (C(A)=0)
# ALL 3 AXES ALREADY DONE.
TC +1 # G LESS THAN .05. CA POS. CONTINUE
CA LCX/360 # G GEQ .05. CONTINUE IN CM/RCS
TS LCX/360 # CMDAPMOD=-0. DAMPING ONLY. SET LCX=0
TS ERRORZ # INITIAL ROLL ERROR (UNREFLECTED) FOR TM.
TS PAXERR1 # SAVE LCX FOR FDAI AND EDIT. (/360)
# Page 1083
CA -VT/180 # GET - 2 VT/180
TS SR
CA SR # GET -VT/180, LEAVE -VT/360 IN SR FOR DZ
TS -VT/180E # DIAGNOSTIC ****
XCH -VT/180 # NOW CONTENTS OF -VT/180 AS LABELED
EXTEND
MP -VT/180 # B(A) = -ZVT/180
EXTEND
MP 180/8ATT
TS VSQ/4API
# IS SGN(VT) ( (180/4A1 TT) VT/180 VT/180 - .5 BUFLIM/360 ) -X/360 - .5 BUFLIM/360 POS?
WHICHALF DOUBLE # FOR SECOND BURN, A1
COM
AD BUFLIM # =BUFLIM/(2 360)
TS L
CCS -VT/180
CS L
TCF +2
CA L
AD LCX/360
AD BUFLIM
EXTEND
BZMF REFLECT # POINT (X,V) IN LHP.
# IS SGN(VT) ( (180/4A1 TT) VT/180 VT/180 - .5 BUFLIM/360 ) -X/360 + .5 BUFLIM/360 NEG?
COM
AD BUFLIM
AD BUFLIM
EXTEND
BZMF DZ1 # POINT (X,V) IN RHP.
# IS POINT WITHIN VELOCITY DZ?
CS VSQMIN # IS VSQ/4API - (VSQ/4API) MIN NEG?
AD VSQ/4API
EXTEND
BZMF DZCALL # YES.
# POINT IS IN BUFFER ZONE. THRUST TO X AXIS.
CS JNDX
TS JNDX1
TC OVRLINE1
REFLECT CS -VT/180 # RELFECT LHP INTO RHP REL TO TERM CONTR
TS -VT/180
TS SR # -VT/360 SAVED FOR DZ.
# Page 1084
CS LCX/360
TS LCX/360
CS JNDX
TS JNDX
# IS VSQ/4API - (VSQ/4API) MIN NEG?
DZ1 CS VSQMIN # IS VSQ/4API - (VSQ/4API) MIN NEG $
AD VSQ/4API
EXTEND
BZMF DZ2 # YES, GO TEST FURTHER.
TCF MAXVTEST # NO
# IS X/360 - XMIN/360 -VT/360 NEG?
DZ2 CS XMIN/360 # XMIN/360 = 4/360
AD LCX/360
AD SR # C(SR) = -VT/360
EXTEND # IS X/360 - XMIN/360 -VT/360 NEG $
BZMF DZCALL # YES, IN DZ. EXIT SETTING JETAG=0.
# IS XD/360 - VM/360K - XS/360 POS?
MAXVTEST CS JNDX
TS JNDX1 # NOW CAN SET JNDX1 FOR TON2 JETS.
CS XS/360 # XS/360 = (XMIN -YMIN/K) /360
AD VSQ/4API
AD LCX/360
TS XD/360 # XD/360= X/360 +VSQ/4API X INTERCEPT
# BUT C(XD/360) = (XD - XS) /360
AD -VM/360K # X INTERCEPT FOR MAX V (VM)
COM
EXTEND
BZMF MAXVTIM1 # YES, THRUST TO VM
CA XD/360
EXTEND
MP KTRCS
DDOUBL # GO SAVE PREDICTED DRIFTING VELOCITY.
TC GETON1 # INSURE THAT Q IS POS AS TAG.
MAXVTIM1 EXTEND
ZQ # SET +Q AS TAG
CS -VMT/180
GETON1 TS VDT/180 # VDT/180 OR VMT/180
AD -VT/180
DOUBLE
EXTEND
MP 180/8ATT
TS TON1 # TON1 / 4T
# Page 1085
EXTEND
BZMF OVRLINE
TC GETON2 # RESET Q POS IF CAME FROM MAXVTIM1
OVRLINE CCS Q
TCF OVRLINE1
MAXVTIM2 CA JNDX1 # ABOVE VM, SO THRUST DOWN
TS JNDX
CS TON1
TCF OVRLINE2 +1
OVRLINE1 CS -VT/180 # DRIFT AT V
TS VDT/180
OVRLINE2 CA ZERO
TS TON1
GETON2 CA VDT/180 # VDT/180, OR VMT/180 OR VT/180
DOUBLE
EXTEND
MP 180/8ATT
DOUBLE # FOR SECOND BURN, A1
TS TON2 # = TON2 / 4T
COM
EXTEND
BZMF GETOFF
TS TON2
CA JNDX
TS JNDX1
GETOFF CS TON2 # TON2 / 4T
EXTEND
MP VDT/180 # VDT/180, OR VT/180, OR VMT/180.
TS XD/360 # USE AS TEMP
CS VDT/180
EXTEND
BZF TOFFOVFL # OMIT THE DIVIDE IF DEN = 0.
AD -VT/180
EXTEND
MP TON1 # TON1 /4T
AD XD/360 # TEMP = -VDT/180 / 2 TON2
AD LCX/360
ZL
XCH L # TEST THE DIVIDE
EXTEND
DV VDT/180
EXTEND
BZF GETOFF2 # DIVIDE OK
TOFFOVFL CA 2JETT # OVFL, USE 2T FOR CONVENIENCE.
TCF TIMSCAL
# Page 1086
GETOFF2 XCH L # GET NUMERATOR.
EXTEND
DV VDT/180 # C(A) = TOFF / 2T
EXTEND
MP 2JETT
TIMSCAL TS TOFF # IN CS
CAF 4JETT
EXTEND
MP TON1 # C(TON1) = TON1 / 4T
TS TON1 # IN CS
CAF 4JETT
EXTEND
MP TON2 # C(TON2) = TON2 / 4T
TS TON2 # IN CS
CA ZERO # CANNOT REDO AFTER TIMETST. TUSED GONE
TS JETAG # SET +0 TO SHOW ROLL DAP CALLED.
# CAUSE THE TM OF BODY RATES VIA UPBUFF TO BE
# INITIALIZED. ALSO CAUSE NEEDLES TO BE DONE ON EXIT
# AND ON ALTERNATE PASSES THROUGH CM/DUMPR.
CA ONE
TS SW/NDX
# Page 1087
# TIMETEST SECTION FOR RCS
#
# ENTER WITH THREE TIME INTERVALS AND THE CORRESPONDING JET CODE INDEXES IN ERASABLE LOCS TON1, TOFF, TON2, JNDX
# JNDX1. SECTION PROCESSES TIME INTERVALS FOR WTLST CALLS AND ASSURES THAT WTLST CALLS ARE MADE ONLY
# (1) FOR POS INTERVALS GREATER THAN A SPECIFIED MINIMUM (HERE CHOSEN AS 2 CS) AND
# (2) FOR THE INTERVALS THAT WILL BE EXECUTED WITHIN THE TIME REMAINING IN THE SAMPLE INTERVAL T (2 SEC).
# TIMETST ESTABLISHES 6 LOCS CONTAINING JET CODES AND CORRESPONDING TIME INTERVALS. THUS: TON1, T1BITS,
# TOFF, TBITS, TON2, T2BITS. OF THESE THE FIRST 2 LOCS ARE TEMPORARY, FOR IMMEDIATE ACTION, IN GENERAL.
# SECTION JETCALL BELOW PROCESSES THIS LIST.
TIMETST CA TIME1 # CORRECT FOR POSSIBLE TIME1 OVFL.
AD POS1/2
AD POS1/2 # OVFL GUARANTEED.
ADS TUSED # B(TUSED) =-TUSED =-OLTIME1
CA -T-3 # =-T +2 -5 (SEE SETJTAG)
# THE +2 REQUIRED FOR PROPER BRANCH.
ADS TUSED # TUSED = TIME(K)-TIME(K-1)-T+2
CS TWO # USE 2 SINCE TIME3 UNCERTAIN TO 1
AD TON1
EXTEND
BZMF TIMETST1
INDEX JNDX
CAF P/RJCODE
TS T1BITS
CA TON1
ADS TUSED
EXTEND
BZMF TOFFTEST
CA ZERO
TCF TIMETST3
TIMETST1 CS ONE
TS TON1
TOFFTEST CS TWO
AD TOFF
EXTEND
BZMF TIMETST2
CA TOFF
ADS TUSED
EXTEND
BZMF TON2TEST
CA ZERO
TCF TIMETST4
TIMETST2 CS ONE
TS TOFF
TON2TEST CS TWO
AD TON2
EXTEND
BZMF TIMETST5
# Page 1088
INDEX JNDX1
CAF P/RJCODE
TS T2BITS
CA TON2
ADS TUSED
EXTEND
BZMF JETCALL1
CA ZERO
TCF TIMETST5 +1
TIMETST3 TS TON1
CS ONE
TIMETST4 TS TOFF
TIMETST5 CS ONE
TS TON2
# SECTION JETCALL EXAMINES CONTENTS OF JET TIMES IN LIST, ESTABLISHES WTLST ENTRIES, AND EXECUTES CORRESPONDING
# JET CODES. A POSITIVE NZ NUMBER IN A TIME REGISTER INDICATES THAT A WTLST CALL IS TO BE MADE, AND ITS JET BITS
# EXECUTED. A +0 INDICATES THAT THE TIME INTERVAL DOES NOT APPLY, BUT THE CORRESPONDING JET BITS ARE TO BE
# EXECUTED. A NEG NUMBER INDICATES THAT THE TIME INTERVAL HAS BEEN PROCESSED. IN EVENT OF +0 OR -1, THE
# SUBSEQUENT TIME REGISTER IS EXAMINED FOR POSSIBLE ACTION. THUS JET BITS TO BE EXECUTED MAY COME FROM MORE
# THAN ONE REGISTER.
JETCALL1 CA ZERO
TS OUTTAG
TS NUJET
TS TBITS
DXCH TON1
CCS A
TCF JETCALL2 # CALL WTLST
JETCALL3 LXCH NUJET # WTLST ENTRIES COME HERE FROM JETCALL
CS ONE
DXCH TOFF
CCS A
TCF JETCALL2 # CALL WTLST
LXCH NUJET
CS ONE
DXCH TON2
CCS A
TCF JETCALL2 # CALL WTLST
LXCH NUJET
TC JETACTN # C(A) = +0
JETCALL2 XCH L # SAVE JET BITS FOR AFTER WTLST CALL
ADS NUJET
XCH L
AD ONE # RESTORE FOR CCS
TC WAITLIST
EBANK= AOG
2CADR JETCALL
JETACTN CA NUJET # COME HERE WHEN DESIRED JET CODE IS KNOWN
# Page 1089
EXTEND # NO NEED TO SAVE OLD CODES
WRITE ROLLJETS # SET RCHAN TO NEW BIT CONFIG.
CCS OUTTAG
TC TASKOVER
ROLLDUMP TC CM/FDAIR
# EDIT DUMP AT ABOVE LOCATION.
# WAITLIST ENTRIES COME HERE.
JETCALL CAF BIT2 # CM/DSTBY =103D BIT2
TS OUTTAG # SIGNIFY WTLST ENTRY
MASK CM/FLAGS # IS SYSTEM DISABLED $
EXTEND
BZF JETACTN +1 # YES, QUENCH ROLL JETS, IF ON AND EXIT.
ZL # NO, CONTINUE.
TCF JETCALL3 # C(A) POS, C(L) = +0
# DEAD ZONE ENTRIES COME HERE.
DZCALL CS CMDAPMOD # POSSIBLE VALUES OF CMDAPMOD: -1, +0, -0.
MASK BIT1
TS L # C(L)=0 FOR -0: C(L)=1 FOR -1 OR +0.
INDEX A # ERASABLE ORDER: ROLLTM, ROLLC, ROLLC +1.
CA ROLLTM # GET ROLL/180 OR ROLLC (/360).
INDEX L
TS A # IF C(L)=1, STORE 'ROLLC' IN 'L'.
AD L # (BOTH MUST BE SCALED DEG/180)
TC ANGOVCOR # C(A)=ROLL/180 OR 2 ROLLC.
TS ROLLHOLD # IF CMDAPMOD =-0, SAVE ROLL ANGLE.
# OTHERWISE, SAVE ROLL COMMAND.
CA ZERO # COME HERE IF IN DZ, AND CANCEL JETS.
EXTEND # INHINT NOT NEEDED HERE.
WRITE ROLLJETS # TURN OFF ALL ROLL JETS.
TS VDT/180 # SET =0 TO SHOW IN DEAD ZONE.
DZCALL1 TS JETAG # COME HERE WITH C(A)=0.
TC ROLLDUMP
# Page 1090
# CM ENTRY FDAI DISPLAY
#
# CALCULATE BY INTEGRATION THE ROLL ERROR BETWEEN THE 2 SEC CM/RCS UPDATES. DISPLAY ATTITUDE ERRORS AS FOLLOWS:
# ATM DAP: DISPLAY ONLY ROLL ATTITUDE ERROR.
# EXT ATM DAP: PRESENT 3 ATTITUDE ERRORS RELATIVE TO THE APPROPRIATE BODY AXES EACH .1 SEC.
# ROLL ROLLC-ROLL
# PITCH ALFAC-ALFA
# YAW BETAC-BETA
#
# DURING ENTRY, THE FDAI NEEDLES HAVE FULL SCALE OF 67.5 DEG IN ROLL AND 16.875 DEG IN PITCH AND YAW.
# THE SUBROUTINE NEEDLER EXPECTS (ANGLE/180) AND SCALES TO 16.875 DEG FULL SCALE.
# COME HERE EACH .1 SEC. (CMDAPMOD=+1 COMES BELOW)
CM/FDAI CS PHIDOT # INTEGRATE ROLL ERROR 'TWEEN 2SEC UPDATES
EXTEND
MP CALFA # FOR ASSUMED COORDINATION.
EXTEND
MP HALF
ADS PAXERR1 # ROLL ERROR/360. OVFL OK.
# EDIT DUMP AT ABOVE LOCATION.
CM/FDAIR CA HALF
EXTEND
MP PAXERR1 # FULL SCALE FOR FDAI (ROLL) IS 67.5 D
TS PAXERR # .25 (ROLL ERROR/180) FOR FDAI NEEDLE.
# PROGRAM TO FILE BODY RATES FOR TM ON ONE PASS AND
# TO UPDATE THE NEEDLE DISPLAY ON THE NEXT.
# SYNCHRONIZATION WITH CM/RCS IS USED SO THAT THE TM
# IS DONE WITH THE ROLL SYSTEM AND NEEDLES START ON
# THE SUBSEQUENT PASS.
CM/DUMPR CS SW/NDX # COMBINED ALTERNATION SWITCH AND FILE
TS SW/NDX
EXTEND # INDEX.
BZMF CMTMFILE # FILE STARTS WITH SW/NDX +1 AND GOES TO
# ENDBUF.
# INDEX IS POS FOR NEEDLES.
TC IBNKCALL
CADR NEEDLER
TC CM/END
# INDEX IS NEG FOR TM FILE
CMTMFILE AD THREE
EXTEND
BZMF SAVENDX
# Page 1091
CA TIME1 # INITIALIZE THE TM LIST IN UPBUFF.
TS CMTMTIME
CS THIRTEEN # INITIALIZE COUNTER
SAVENDX TS SW/NDX # A NEGATIVE NUMBER.
EXTEND
DCA PREL
INDEX SW/NDX
DXCH ENDBUF -1
CA RREL
INDEX SW/NDX
TS ENDBUF +1
CM/END CA CM/SAVE
TS SR
# DOES NOT PROTECT TEMK, SQ IN SPSIN/COS
EXTEND
DCA T5IDLER2
DXCH T5LOC
TC RESUME
EBANK= T5LOC
T5IDLER2 2CADR T5IDLOC
# DEFINE THE FOLLOWING 17D REGISTERS IN UPBUFF TO BE
# USED TO TELEMETER CM VEHICLE BODY RATE INFORMATION.
# THE INFORMATION IS FILED EACH 0.2 SEC, GIVING 15D
# DATA POINTS EACH 1 SEC. TM LIST IS READ TWICE
# EACH 2 SECONDS.
#
# THE SEQUENCE IS: SP TIME INITIAL TIME
# SWITCH ALSO INDEX.
# P ROLL RATE
# Q PITCH RATE
# R YAW RATE
# ETC.
#CMTMTIME = UPBUFF
#SW/NDX = UPBUFF +1
#ENDBUF = UPBUFF +16D
# Page 1092
# SPACER
#
# CONSTANTS USED IN THE ROLL CONTROL SYSTEM:
# CONSTANTS ARE THE FOLLOWING: A = 9.1 DEG/SECSQ, VM = 20 DEG/SEC, T = 2 SEC, TCDU = .1 SEC,
# XMIN = 4 DEG, VMIN = 2 DEG/SEC, K = .25, A1 = 4.55 DEG/SECSQ, VI = 1 DEG/SEC, INTERCEPT WITH DZ SIDE
# XBUF = 4 DEG
-T-3 DEC -203 # CS
VSQMIN DEC .61050061 E-3 # VSQ MIN/4 A PI = 4/(4 (9.1) 180)
2T/TCDU = OCT50 # T/TCDU EXP-14 TCDU = .1SEC
180/8ATT DEC .61813187 # 180/(8 (9.1) 4)=(180/ATT) EXP -3
-VMT/180 = -VM/360K # = 20 (2) / 180
2JETT = 4SECS # CS 2 (2) 100 INTEGER
4JETT DEC 800 # CS 4 (2) 100 INTEGER
XMIN/360 DEC 182 # XMIN/360 = 4/ 360 EXP 14 = 182 INTEGER
-VM/360K DEC -.22222222 # =-20/( 360 (.25))
1/16A1 = 180/8ATT
# 1/16A1 = 180/(16 A1 TT)
# = 180/(16 4.55 4)
XS/360 DEC 91 # =(XMIN +VI (T-1/K))/360 = 2/360 EXP 14
BUFLIM = XS/360 # 4/(2 360)
KTRCS = HALF # KT = (.25) 2 = .5
# *** END OF TVCDAPS .011 ***
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