Proofed pages 1451-1459
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@ -465,7 +465,7 @@ GTSCADR 2CADR GTS
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QERRCALC CAE CDUY # Q-ERROR CALCULATION
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QERRCALC CAE CDUY # Q-ERROR CALCULATION
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EXTEND
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EXTEND
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MSU CDUYD # CDU ANGLE -- ANGLE DESIRED (Y-AXIS)
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MSU CDUYD # CDU ANGLE - ANGLE DESIRED (Y-AXIS)
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TS DAPTEMP1 # SAVE FOR RERRCALC
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TS DAPTEMP1 # SAVE FOR RERRCALC
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EXTEND
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EXTEND
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MP M21 # (CDUY-CDUYD)*M21 SCALED AT PI RADIANS
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MP M21 # (CDUY-CDUYD)*M21 SCALED AT PI RADIANS
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@ -541,7 +541,7 @@ TJLAW CA TJLAWADR
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TS NUMBERT # FALL THROUGH TO JET SELECTION, ETC.
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TS NUMBERT # FALL THROUGH TO JET SELECTION, ETC.
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# Q,R-JET-SELECTION-LOGIC
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# Q,R-JET-SELECTION-LOGIC
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#
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# INPUT: AXISCTR 0,1 FOR U,V
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# INPUT: AXISCTR 0,1 FOR U,V
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# SNUFFBIT ZERO TJETU,V AND TRANS. ONLY IF SET IN A DPS BURN
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# SNUFFBIT ZERO TJETU,V AND TRANS. ONLY IF SET IN A DPS BURN
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# Page 1453
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# Page 1453
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@ -551,9 +551,9 @@ TJLAW CA TJLAWADR
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#
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#
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# OUTPUT: NO.U(V)JETS RATE DERIVATION FEEDBACK
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# OUTPUT: NO.U(V)JETS RATE DERIVATION FEEDBACK
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# CHANNEL 5
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# CHANNEL 5
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# SKIPU,SKIPV FOR LESS THAN 150MS FIRING
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# SKIPU,SKIRV FOR LESS THAN 150MS FIRING
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#
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#
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# NOTES: IN CASE OF FAILURE IN DESIRED ROTATION POLICY, "ALL" UNFAILED
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# NOTES: IN CASE OF FAILURE IN DESIRED ROTATION POLICY,"ALL" UNFAILED
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# JETS OF THE DESIRED POLICY ARE SELECTED. SINCE THERE ARE ONLY
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# JETS OF THE DESIRED POLICY ARE SELECTED. SINCE THERE ARE ONLY
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# TWO JETS, THIS MEANS THE OTHER ONE OR NONE. THE ALARM IS SENT
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# TWO JETS, THIS MEANS THE OTHER ONE OR NONE. THE ALARM IS SENT
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# IF NONE CAN BE FOUND.
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# IF NONE CAN BE FOUND.
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@ -562,7 +562,7 @@ TJLAW CA TJLAWADR
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# MINIMUM IMPULSE, WITH THE JET CHOSEN SEMI-RANDOMLY.
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# MINIMUM IMPULSE, WITH THE JET CHOSEN SEMI-RANDOMLY.
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AFTERTJ CA FLAGWRD5 # IF SNUFFBIT SET DURING A DPS BURN GO TO
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AFTERTJ CA FLAGWRD5 # IF SNUFFBIT SET DURING A DPS BURN GO TO
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MASK SNUFFBIT # XTRANS; THAT IS, INHIBIT CONTROL.
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MASK SNUFFBIT # XTRANS; THAT IS, INHIBIT CONTROL.
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EXTEND
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EXTEND
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BZF DOROTAT
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BZF DOROTAT
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CS FLGWRD10
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CS FLGWRD10
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@ -588,7 +588,7 @@ DOROTAT CAF TWO
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CA AXISCTR
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CA AXISCTR
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AD L
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AD L
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TS ROTINDEX # 0 1 2 3 = -U -V +U +V
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TS ROTINDEX # 0 1 2 3 = -U -V -+U +V
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CA ABSTJ
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CA ABSTJ
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AD -150MS
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AD -150MS
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@ -712,30 +712,30 @@ TJLAWADR GENADR TJLAW +3 # RETURN ADDRESS FOR RCS ATTITUDE CONTROL
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# TS T6FURTHA +1
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# TS T6FURTHA +1
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# TC JTLST
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# TC JTLST
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#
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#
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# EXAMPLE -- U-AXIS AUTOPILOT WILL WRITE ITS ROTATION CODE OF
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# EXAMPLE- U-AXIS AUTOPILOT WILL WRITE ITS ROTATION CODE OF
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# JETS INTO CHANNEL 5. IF IT DESIRES TO TURN OFF THIS POLICY WITHIN
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# JETS INTO CHANNEL 5. IF IT DESIRES TO TURN OFF THIS POLICY WITHIN
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# 150MS AND THEN FIRE NEXTU, A CALL TO JTLST IS MADE WITH T6FURTHA
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# 150MS AND THEN FIRE NEXTU, A CALL TO JTLST IS MADE WITH T6FURTHA
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# CONTAINING THE TIME TO TURN OFF THE POLICY, T6FURTHA +1 THE INDEX
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# CONTAINING THE TIME TO TURN OFF THE POLICY, T6FURTHA +1 THE INDEX
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# OF THE U-AXIS(4), AND NEXTU WILL CONTAIN THE "U-TRANS" POLICY OR ZERO.
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# OF THE U-AXIS(4), AND NEXTU WILL CONTAIN THE "U-TRANS" POLICY OR ZERO.
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#
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#
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# THE LIST IS EXACTLY 3 LONG. (THIS LEADS UP TO SKIP LOGIC AND 150MS LIMIT)
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# THE LIST IS EXACTLY 3 LONG.(THIS LEADS UP TO SKIP LOGIC AND 150MS LIMIT)
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# THE INPUT IS THE LAST MEMBER OF THE LIST.
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# THE INPUT IS THE LAST MEMBER OF THE LIST.
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#
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#
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# RETURNS BY:
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# RETURNS BY:
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# + TC Q
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# + TC Q
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#
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#
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# DEFINITIONS: (OUTPUT)
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# DEFINITIONS:(OUTPUT)
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# TIME6 TIME OF NEXT RUPT
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# TIME6 TIME OF NEXT RUPT
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# T6NEXT DELTA TIME TO NEXT RUPT
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# T6NEXT DELTA TIME TO NEXT RUPT
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# T6FURTHA DELTA TIME FROM 2ND TO LAST RUPT
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# T6FURTHA DELTA TIME FROM 2ND TO LAST RUPT
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# NXT6ADR AXIS INDEX 0 -- P-AXIS
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# NXT6ADR AXIS INDEX Q - P-AXIS
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# T6NEXT +1 AXIS INDEX 4 -- U-AXIS
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# T6NEXT +1 AXIS INDEX 4 - U-AXIS
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# T6FURTHA +1 AXIS INDEX 13 -- V-AXIS
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# T6FURTHA +1 AXIS INDEX 13 - V-AXIS
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JTLST CS T6FURTHA
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JTLST CS T6FURTHA
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AD TIME6
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AD TIME6
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EXTEND
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EXTEND
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BZMF MIDORLST # TIME6 -- TI IS IN A
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BZMF MIDORLST # TIME6 -- T IS IN A
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LXCH NXT6ADR
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LXCH NXT6ADR
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DXCH T6NEXT
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DXCH T6NEXT
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@ -767,9 +767,9 @@ LASTCHG CS A
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TC Q
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TC Q
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# ROT-TOUV IS ENTERED WITH THE Q-COMPONENT OF THE QUANTITY TO BE TRANSFORMED IN A AND THE R-COMPONENT IN L.
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# ROT-TOUV IS ENTERED WITH THE Q-COMPONENT OF THE QUANTITY TO BE TRANSFORMED IN A AND THE R-COMPONENT IN L.
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# ROT-TOUV TRANSFORMS THE QUANTITY INTO THE NON-ORTHOGONAL U-V AXIS SYSTEM. IN THE U-V SYSTEM NO CROSS-COUPLING IS
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# ROT-TOUV TRANSFORMS THE QUANTITY INTO THE NON-ORTHOGONAL U-V AXIS SYSTEM. IN THE U-V SYSTEM NO CROSS-COUPLING IS
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# PRODUCED FROM RCS JET FIRINGS. AT THE COMPLETION OF ROT-TOUV, THE U-COMPONENT OF THE TRANSFORMED QUANTITY IS IN
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# PRODUCED FROM RCS JET FIRINGS. AT THE COMPLETION OF ROT-TOUV, THE U-COMPONENT OF THE TRANSFORMED QUANTITY IS IN
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# A AND THE V-COMPONENT IS IN L.
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# A AND THE V-COMPONENT IS IN L.
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ROT-TOUV LXCH ROTEMP2 # (R) IS PUT INTO ROTEMP2
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ROT-TOUV LXCH ROTEMP2 # (R) IS PUT INTO ROTEMP2
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@ -822,15 +822,16 @@ FAILOOP TS NUMBERT
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TC ALARM
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TC ALARM
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OCT 02004
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OCT 02004
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TCF NOROTAT
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TCF NOROTAT
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ALLJETS OCT 00110 # -U 6 13
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ALLJETS OCT 00110 # -U 6 13
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OCT 00022 # -V 2 9
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OCT 00022 # -V 2 9
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OCT 00204 # +U 5 14
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OCT 00204 # +U 5 14
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OCT 00041 # +V 1 10
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TYPEPOLY OCT 00125 # -X 1 5 9 13
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OCT 00041 # +V 1 10
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OCT 00252 # +X 2 6 10 14
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TYPEPOLY OCT 00125 # -X 1 5 9 13
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OCT 00146 # A 2 5 10 13
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OCT 00252 # +X 2 6 10 14
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OCT 00231 # B 1 6 9 14
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OCT 00146 # A 2 5 10 13
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OCT 00377 # ALL 1 2 5 6 9 10 13 14
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OCT 00231 # B 1 6 9 14
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OCT 00377 # ALL 1 2 5 6 9 10 13 14
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# THE FOLLOWING SETS THE INTERRUPT FLIP-FLOP AS SOON AS POSSIBLE, WHICH PERMITS A RETURN TO THE INTERRUPTED JOB.
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# THE FOLLOWING SETS THE INTERRUPT FLIP-FLOP AS SOON AS POSSIBLE, WHICH PERMITS A RETURN TO THE INTERRUPTED JOB.
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@ -857,4 +858,3 @@ ENDJASK DXCH DAPARUPT
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MAKERUPT EXTEND
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MAKERUPT EXTEND
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EDRUPT MAKERUPT
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EDRUPT MAKERUPT
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