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Proof R63 #629 (#652)

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* Proof R63 #629

* Proof R63 #629 requested changes

* Proof R63 #629 UNDO of mistaken change of GOFLASH to GDFLASH.

GOFLASH occurs throughtout the code, but GDFLASH, never. The O clearly looked like D, but makes no sense in this case.
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jiversen 2020-02-20 15:30:50 -08:00 committed by GitHub
parent 3df2a2849f
commit 1dbfa782e7
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1 changed files with 11 additions and 11 deletions
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Luminary099/R63.agc
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@ -44,7 +44,7 @@
# #
# 3. FLASH DISPLAY V 04 N 06. R2 INDICATES WHICH SPACECRAFT AXIS IS TO # 3. FLASH DISPLAY V 04 N 06. R2 INDICATES WHICH SPACECRAFT AXIS IS TO
# BE POINTED AT CSM. INITIAL CHOICE IS PREFERRED (+Z) AXIS (R2=1). # BE POINTED AT CSM. INITIAL CHOICE IS PREFERRED (+Z) AXIS (R2=1).
# ASTRONAUT CAN CHANGE TO (+X) AXIS (R2 NOT =1) BY V 22 E 2 E. CONTINUE # ASTRONAUT CAN CHANGE TO (+X) AXIS (R2 NOT = 1) BY V 22 E 2 E. CONTINUE
# AFTER KEYING IN PROCEED. # AFTER KEYING IN PROCEED.
# #
# 4. BOTH VEHICLE STATE VECTORS UPDATED BY CONIC EQS. # 4. BOTH VEHICLE STATE VECTORS UPDATED BY CONIC EQS.
@ -56,13 +56,13 @@
# 6. GIMBAL ANGLES FROM VECPOINT TRANSFORMED INTO FDAI BALL ANGLES BY # 6. GIMBAL ANGLES FROM VECPOINT TRANSFORMED INTO FDAI BALL ANGLES BY
# BALLANGS. FLASH DISPLAY V 06 N 18 AND AWAIT RESPONSE. # BALLANGS. FLASH DISPLAY V 06 N 18 AND AWAIT RESPONSE.
# #
# 7 RECYCLE -- RETURN TO STEP 4. # 7. RECYCLE - RETURN TO STEP 4.
# TERMINATE -- EXIT R63 # TERMINATE - EXIT R63.
# PROCEED -- RESET 3AXISFLAG AND CALL R60LEM FOR ATTITUDE MANEUVER. # PROCEED - RESET 3AXISFLG AND CALL R60LEM FOR ATTITUDE MANEUVER.
# #
# CALLING SEQUENCE: V 89 E. # CALLING SEQUENCE: V 89 E.
# #
# SUBROUTINES CALLED: CHECKP00H, R02BOTH, GOXDSPF, CSMCONIC, LEMCONIC, # SUBROUTINES CALLED: CHKPOOH, R02BOTH, GOXDSPF, CSMCONIC, LEMCONIC,
# VECPOINT, BALLANGS, R60LEM. # VECPOINT, BALLANGS, R60LEM.
# #
# NORMAL EXIT MODES: TC ENDEXT # NORMAL EXIT MODES: TC ENDEXT
@ -75,9 +75,9 @@
# #
# ERASABLE INITIALIZATION REQUIRED: NONE # ERASABLE INITIALIZATION REQUIRED: NONE
# #
# DEBRIS: OPTION1, +1, TDEC1, PCINTVSM, SCAXIS, CPHI, CTHETA, CPSI, # DEBRIS: OPTION1, +1, TDEC1, PDINTVSM, SCAXIS, CPHI, CTHETA, CPSI,
# Page 339 # Page 339
# 3AXISFLAG. # 3AXISFLG.
EBANK= RONE EBANK= RONE
BANK 32 BANK 32
@ -91,13 +91,13 @@ V89CALL TC BANKCALL # IMU STATUS CHECK. RETURNS IF ORIENTATION
TS OPTIONX # TRACKING ATTITUDE AXIS. TS OPTIONX # TRACKING ATTITUDE AXIS.
CAF ONE CAF ONE
TS OPTIONX +1 TS OPTIONX +1
CAF VB04N12 # V 04 N 12. CAF VB04N12 # V 04 N 12
TC BANKCALL TC BANKCALL
CADR GOFLASH CADR GOFLASH
TC ENDEXT # TERMINATE TC ENDEXT # TERMINATE
TC +2 # PROCEED TC +2 # PROCEED
TC -5 # DATA IN. OPTION1+1 = 1 FOR Z AXIS TC -5 # DATA IN. OPTION1+1 = 1 FOR Z AXIS
V89RECL TC INTPRET # 2 FOR X AXIS V89RECL TC INTPRET # = 2 FOR X AXIS
RTB DAD RTB DAD
LOADTIME # READ PRESENT TIME LOADTIME # READ PRESENT TIME
DP1MIN DP1MIN
@ -110,7 +110,7 @@ V89RECL TC INTPRET # 2 FOR X AXIS
TSTART82 TSTART82
STCALL TDEC1 # STORE TIME FOR LEMCONIC CALL STCALL TDEC1 # STORE TIME FOR LEMCONIC CALL
LEMCONIC # LEM STATE VECTOR UPDATE LEMCONIC # LEM STATE VECTOR UPDATE
VLOAD VSU # CSM POSITION -- LEM POSITION -- LOS VLOAD VSU # CSM POSITION - LEM POSITION = LOS
RONE # LOS VECTOR LEFT IN MPAC RONE # LOS VECTOR LEFT IN MPAC
RATT RATT
MXV RTB # (REFSMAT X LOS). TRANSFORMS LOS FROM MXV RTB # (REFSMAT X LOS). TRANSFORMS LOS FROM
@ -128,7 +128,7 @@ ALINEX TC INTPRET # X AXIS ALIGNMENT
# Page 340 # Page 340
V89CALL1 STCALL SCAXIS # STORE SELECTED ALIGNMENT AXIS V89CALL1 STCALL SCAXIS # STORE SELECTED ALIGNMENT AXIS
VECPOINT # PUTS DESIRED GIM ANG (OG,IG,MG) IN TMPAC VECPOINT # PUTS DESIRED GIM ANG (OG,IG,MG) IN TMPAC
STORE CPHI # STOR GIMBAL ANGLES FOR BALLANGS CALL STORE CPHI # STORE GIMBAL ANGLES FOR BALLANGS CALL.
EXIT EXIT
TC BANKCALL TC BANKCALL
CADR BALLANGS # PUTS DESIRED BALL ANGLE IN FDAIX,Y,Z CADR BALLANGS # PUTS DESIRED BALL ANGLE IN FDAIX,Y,Z