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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.
This commit is contained in:
jiversen
2020-02-20 15:30:50 -08:00
committed by GitHub
parent 3df2a2849f
commit 1dbfa782e7
1 changed files with 11 additions and 11 deletions
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22
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
# 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.
#
# 4. BOTH VEHICLE STATE VECTORS UPDATED BY CONIC EQS.
@@ -56,13 +56,13 @@
# 6. GIMBAL ANGLES FROM VECPOINT TRANSFORMED INTO FDAI BALL ANGLES BY
# BALLANGS. FLASH DISPLAY V 06 N 18 AND AWAIT RESPONSE.
#
# 7 RECYCLE -- RETURN TO STEP 4.
# TERMINATE -- EXIT R63
# PROCEED -- RESET 3AXISFLAG AND CALL R60LEM FOR ATTITUDE MANEUVER.
# 7. RECYCLE - RETURN TO STEP 4.
# TERMINATE - EXIT R63.
# PROCEED - RESET 3AXISFLG AND CALL R60LEM FOR ATTITUDE MANEUVER.
#
# CALLING SEQUENCE: V 89 E.
#
# SUBROUTINES CALLED: CHECKP00H, R02BOTH, GOXDSPF, CSMCONIC, LEMCONIC,
# SUBROUTINES CALLED: CHKPOOH, R02BOTH, GOXDSPF, CSMCONIC, LEMCONIC,
# VECPOINT, BALLANGS, R60LEM.
#
# NORMAL EXIT MODES: TC ENDEXT
@@ -75,9 +75,9 @@
#
# ERASABLE INITIALIZATION REQUIRED: NONE
#
# DEBRIS: OPTION1, +1, TDEC1, PCINTVSM, SCAXIS, CPHI, CTHETA, CPSI,
# DEBRIS: OPTION1, +1, TDEC1, PDINTVSM, SCAXIS, CPHI, CTHETA, CPSI,
# Page 339
# 3AXISFLAG.
# 3AXISFLG.
EBANK= RONE
BANK 32
@@ -91,13 +91,13 @@ V89CALL TC BANKCALL # IMU STATUS CHECK. RETURNS IF ORIENTATION
TS OPTIONX # TRACKING ATTITUDE AXIS.
CAF ONE
TS OPTIONX +1
CAF VB04N12 # V 04 N 12.
CAF VB04N12 # V 04 N 12
TC BANKCALL
CADR GOFLASH
TC ENDEXT # TERMINATE
TC +2 # PROCEED
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
LOADTIME # READ PRESENT TIME
DP1MIN
@@ -110,7 +110,7 @@ V89RECL TC INTPRET # 2 FOR X AXIS
TSTART82
STCALL TDEC1 # STORE TIME FOR LEMCONIC CALL
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
RATT
MXV RTB # (REFSMAT X LOS). TRANSFORMS LOS FROM
@@ -128,7 +128,7 @@ ALINEX TC INTPRET # X AXIS ALIGNMENT
# Page 340
V89CALL1 STCALL SCAXIS # STORE SELECTED ALIGNMENT AXIS
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
TC BANKCALL
CADR BALLANGS # PUTS DESIRED BALL ANGLE IN FDAIX,Y,Z