* 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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@ -44,7 +44,7 @@
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#
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#
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# 3. FLASH DISPLAY V 04 N 06. R2 INDICATES WHICH SPACECRAFT AXIS IS TO
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# 3. FLASH DISPLAY V 04 N 06. R2 INDICATES WHICH SPACECRAFT AXIS IS TO
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# BE POINTED AT CSM. INITIAL CHOICE IS PREFERRED (+Z) AXIS (R2=1).
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# BE POINTED AT CSM. INITIAL CHOICE IS PREFERRED (+Z) AXIS (R2=1).
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# ASTRONAUT CAN CHANGE TO (+X) AXIS (R2 NOT =1) BY V 22 E 2 E. CONTINUE
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# ASTRONAUT CAN CHANGE TO (+X) AXIS (R2 NOT = 1) BY V 22 E 2 E. CONTINUE
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# AFTER KEYING IN PROCEED.
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# AFTER KEYING IN PROCEED.
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#
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#
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# 4. BOTH VEHICLE STATE VECTORS UPDATED BY CONIC EQS.
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# 4. BOTH VEHICLE STATE VECTORS UPDATED BY CONIC EQS.
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@ -56,13 +56,13 @@
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# 6. GIMBAL ANGLES FROM VECPOINT TRANSFORMED INTO FDAI BALL ANGLES BY
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# 6. GIMBAL ANGLES FROM VECPOINT TRANSFORMED INTO FDAI BALL ANGLES BY
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# BALLANGS. FLASH DISPLAY V 06 N 18 AND AWAIT RESPONSE.
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# BALLANGS. FLASH DISPLAY V 06 N 18 AND AWAIT RESPONSE.
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#
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#
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# 7 RECYCLE -- RETURN TO STEP 4.
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# 7. RECYCLE - RETURN TO STEP 4.
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# TERMINATE -- EXIT R63
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# TERMINATE - EXIT R63.
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# PROCEED -- RESET 3AXISFLAG AND CALL R60LEM FOR ATTITUDE MANEUVER.
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# PROCEED - RESET 3AXISFLG AND CALL R60LEM FOR ATTITUDE MANEUVER.
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#
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#
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# CALLING SEQUENCE: V 89 E.
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# CALLING SEQUENCE: V 89 E.
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#
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#
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# SUBROUTINES CALLED: CHECKP00H, R02BOTH, GOXDSPF, CSMCONIC, LEMCONIC,
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# SUBROUTINES CALLED: CHKPOOH, R02BOTH, GOXDSPF, CSMCONIC, LEMCONIC,
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# VECPOINT, BALLANGS, R60LEM.
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# VECPOINT, BALLANGS, R60LEM.
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#
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#
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# NORMAL EXIT MODES: TC ENDEXT
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# NORMAL EXIT MODES: TC ENDEXT
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@ -75,9 +75,9 @@
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#
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#
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# ERASABLE INITIALIZATION REQUIRED: NONE
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# ERASABLE INITIALIZATION REQUIRED: NONE
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#
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#
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# DEBRIS: OPTION1, +1, TDEC1, PCINTVSM, SCAXIS, CPHI, CTHETA, CPSI,
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# DEBRIS: OPTION1, +1, TDEC1, PDINTVSM, SCAXIS, CPHI, CTHETA, CPSI,
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# Page 339
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# Page 339
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# 3AXISFLAG.
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# 3AXISFLG.
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EBANK= RONE
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EBANK= RONE
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BANK 32
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BANK 32
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@ -91,13 +91,13 @@ V89CALL TC BANKCALL # IMU STATUS CHECK. RETURNS IF ORIENTATION
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TS OPTIONX # TRACKING ATTITUDE AXIS.
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TS OPTIONX # TRACKING ATTITUDE AXIS.
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CAF ONE
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CAF ONE
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TS OPTIONX +1
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TS OPTIONX +1
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CAF VB04N12 # V 04 N 12.
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CAF VB04N12 # V 04 N 12
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TC BANKCALL
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TC BANKCALL
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CADR GOFLASH
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CADR GOFLASH
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TC ENDEXT # TERMINATE
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TC ENDEXT # TERMINATE
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TC +2 # PROCEED
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TC +2 # PROCEED
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TC -5 # DATA IN. OPTION1+1 = 1 FOR Z AXIS
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TC -5 # DATA IN. OPTION1+1 = 1 FOR Z AXIS
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V89RECL TC INTPRET # 2 FOR X AXIS
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V89RECL TC INTPRET # = 2 FOR X AXIS
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RTB DAD
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RTB DAD
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LOADTIME # READ PRESENT TIME
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LOADTIME # READ PRESENT TIME
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DP1MIN
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DP1MIN
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@ -110,7 +110,7 @@ V89RECL TC INTPRET # 2 FOR X AXIS
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TSTART82
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TSTART82
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STCALL TDEC1 # STORE TIME FOR LEMCONIC CALL
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STCALL TDEC1 # STORE TIME FOR LEMCONIC CALL
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LEMCONIC # LEM STATE VECTOR UPDATE
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LEMCONIC # LEM STATE VECTOR UPDATE
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VLOAD VSU # CSM POSITION -- LEM POSITION -- LOS
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VLOAD VSU # CSM POSITION - LEM POSITION = LOS
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RONE # LOS VECTOR LEFT IN MPAC
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RONE # LOS VECTOR LEFT IN MPAC
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RATT
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RATT
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MXV RTB # (REFSMAT X LOS). TRANSFORMS LOS FROM
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MXV RTB # (REFSMAT X LOS). TRANSFORMS LOS FROM
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@ -128,7 +128,7 @@ ALINEX TC INTPRET # X AXIS ALIGNMENT
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# Page 340
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# Page 340
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V89CALL1 STCALL SCAXIS # STORE SELECTED ALIGNMENT AXIS
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V89CALL1 STCALL SCAXIS # STORE SELECTED ALIGNMENT AXIS
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VECPOINT # PUTS DESIRED GIM ANG (OG,IG,MG) IN TMPAC
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VECPOINT # PUTS DESIRED GIM ANG (OG,IG,MG) IN TMPAC
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STORE CPHI # STOR GIMBAL ANGLES FOR BALLANGS CALL
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STORE CPHI # STORE GIMBAL ANGLES FOR BALLANGS CALL.
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EXIT
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EXIT
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TC BANKCALL
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TC BANKCALL
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CADR BALLANGS # PUTS DESIRED BALL ANGLE IN FDAIX,Y,Z
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CADR BALLANGS # PUTS DESIRED BALL ANGLE IN FDAIX,Y,Z
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