Proofed pages 1451-1459
Murtaza
parent
d9af7cbf2e
commit
aa5cd1cb7a
|
|
@ -465,7 +465,7 @@ GTSCADR 2CADR GTS
|
|||
|
||||
QERRCALC CAE CDUY # Q-ERROR CALCULATION
|
||||
EXTEND
|
||||
MSU CDUYD # CDU ANGLE -- ANGLE DESIRED (Y-AXIS)
|
||||
MSU CDUYD # CDU ANGLE - ANGLE DESIRED (Y-AXIS)
|
||||
TS DAPTEMP1 # SAVE FOR RERRCALC
|
||||
EXTEND
|
||||
MP M21 # (CDUY-CDUYD)*M21 SCALED AT PI RADIANS
|
||||
|
|
@ -541,7 +541,7 @@ TJLAW CA TJLAWADR
|
|||
TS NUMBERT # FALL THROUGH TO JET SELECTION, ETC.
|
||||
|
||||
# Q,R-JET-SELECTION-LOGIC
|
||||
#
|
||||
|
||||
# INPUT: AXISCTR 0,1 FOR U,V
|
||||
# SNUFFBIT ZERO TJETU,V AND TRANS. ONLY IF SET IN A DPS BURN
|
||||
# Page 1453
|
||||
|
|
@ -551,9 +551,9 @@ TJLAW CA TJLAWADR
|
|||
#
|
||||
# OUTPUT: NO.U(V)JETS RATE DERIVATION FEEDBACK
|
||||
# CHANNEL 5
|
||||
# SKIPU,SKIPV FOR LESS THAN 150MS FIRING
|
||||
# SKIPU,SKIRV FOR LESS THAN 150MS FIRING
|
||||
#
|
||||
# NOTES: IN CASE OF FAILURE IN DESIRED ROTATION POLICY, "ALL" UNFAILED
|
||||
# NOTES: IN CASE OF FAILURE IN DESIRED ROTATION POLICY,"ALL" UNFAILED
|
||||
# JETS OF THE DESIRED POLICY ARE SELECTED. SINCE THERE ARE ONLY
|
||||
# TWO JETS, THIS MEANS THE OTHER ONE OR NONE. THE ALARM IS SENT
|
||||
# IF NONE CAN BE FOUND.
|
||||
|
|
@ -562,7 +562,7 @@ TJLAW CA TJLAWADR
|
|||
# MINIMUM IMPULSE, WITH THE JET CHOSEN SEMI-RANDOMLY.
|
||||
|
||||
AFTERTJ CA FLAGWRD5 # IF SNUFFBIT SET DURING A DPS BURN GO TO
|
||||
MASK SNUFFBIT # XTRANS; THAT IS, INHIBIT CONTROL.
|
||||
MASK SNUFFBIT # XTRANS; THAT IS, INHIBIT CONTROL.
|
||||
EXTEND
|
||||
BZF DOROTAT
|
||||
CS FLGWRD10
|
||||
|
|
@ -588,7 +588,7 @@ DOROTAT CAF TWO
|
|||
|
||||
CA AXISCTR
|
||||
AD L
|
||||
TS ROTINDEX # 0 1 2 3 = -U -V +U +V
|
||||
TS ROTINDEX # 0 1 2 3 = -U -V -+U +V
|
||||
|
||||
CA ABSTJ
|
||||
AD -150MS
|
||||
|
|
@ -712,30 +712,30 @@ TJLAWADR GENADR TJLAW +3 # RETURN ADDRESS FOR RCS ATTITUDE CONTROL
|
|||
# TS T6FURTHA +1
|
||||
# TC JTLST
|
||||
#
|
||||
# EXAMPLE -- U-AXIS AUTOPILOT WILL WRITE ITS ROTATION CODE OF
|
||||
# EXAMPLE- U-AXIS AUTOPILOT WILL WRITE ITS ROTATION CODE OF
|
||||
# JETS INTO CHANNEL 5. IF IT DESIRES TO TURN OFF THIS POLICY WITHIN
|
||||
# 150MS AND THEN FIRE NEXTU, A CALL TO JTLST IS MADE WITH T6FURTHA
|
||||
# CONTAINING THE TIME TO TURN OFF THE POLICY, T6FURTHA +1 THE INDEX
|
||||
# OF THE U-AXIS(4), AND NEXTU WILL CONTAIN THE "U-TRANS" POLICY OR ZERO.
|
||||
#
|
||||
# THE LIST IS EXACTLY 3 LONG. (THIS LEADS UP TO SKIP LOGIC AND 150MS LIMIT)
|
||||
# THE INPUT IS THE LAST MEMBER OF THE LIST.
|
||||
# THE LIST IS EXACTLY 3 LONG.(THIS LEADS UP TO SKIP LOGIC AND 150MS LIMIT)
|
||||
# THE INPUT IS THE LAST MEMBER OF THE LIST.
|
||||
#
|
||||
# RETURNS BY:
|
||||
# + TC Q
|
||||
#
|
||||
# DEFINITIONS: (OUTPUT)
|
||||
# TIME6 TIME OF NEXT RUPT
|
||||
# T6NEXT DELTA TIME TO NEXT RUPT
|
||||
# T6FURTHA DELTA TIME FROM 2ND TO LAST RUPT
|
||||
# NXT6ADR AXIS INDEX 0 -- P-AXIS
|
||||
# T6NEXT +1 AXIS INDEX 4 -- U-AXIS
|
||||
# T6FURTHA +1 AXIS INDEX 13 -- V-AXIS
|
||||
# DEFINITIONS:(OUTPUT)
|
||||
# TIME6 TIME OF NEXT RUPT
|
||||
# T6NEXT DELTA TIME TO NEXT RUPT
|
||||
# T6FURTHA DELTA TIME FROM 2ND TO LAST RUPT
|
||||
# NXT6ADR AXIS INDEX Q - P-AXIS
|
||||
# T6NEXT +1 AXIS INDEX 4 - U-AXIS
|
||||
# T6FURTHA +1 AXIS INDEX 13 - V-AXIS
|
||||
|
||||
JTLST CS T6FURTHA
|
||||
AD TIME6
|
||||
EXTEND
|
||||
BZMF MIDORLST # TIME6 -- TI IS IN A
|
||||
BZMF MIDORLST # TIME6 -- T IS IN A
|
||||
|
||||
LXCH NXT6ADR
|
||||
DXCH T6NEXT
|
||||
|
|
@ -767,9 +767,9 @@ LASTCHG CS A
|
|||
|
||||
TC Q
|
||||
|
||||
# ROT-TOUV IS ENTERED WITH THE Q-COMPONENT OF THE QUANTITY TO BE TRANSFORMED IN A AND THE R-COMPONENT IN L.
|
||||
# ROT-TOUV TRANSFORMS THE QUANTITY INTO THE NON-ORTHOGONAL U-V AXIS SYSTEM. IN THE U-V SYSTEM NO CROSS-COUPLING IS
|
||||
# PRODUCED FROM RCS JET FIRINGS. AT THE COMPLETION OF ROT-TOUV, THE U-COMPONENT OF THE TRANSFORMED QUANTITY IS IN
|
||||
# ROT-TOUV IS ENTERED WITH THE Q-COMPONENT OF THE QUANTITY TO BE TRANSFORMED IN A AND THE R-COMPONENT IN L.
|
||||
# ROT-TOUV TRANSFORMS THE QUANTITY INTO THE NON-ORTHOGONAL U-V AXIS SYSTEM. IN THE U-V SYSTEM NO CROSS-COUPLING IS
|
||||
# PRODUCED FROM RCS JET FIRINGS. AT THE COMPLETION OF ROT-TOUV, THE U-COMPONENT OF THE TRANSFORMED QUANTITY IS IN
|
||||
# A AND THE V-COMPONENT IS IN L.
|
||||
|
||||
ROT-TOUV LXCH ROTEMP2 # (R) IS PUT INTO ROTEMP2
|
||||
|
|
@ -822,15 +822,16 @@ FAILOOP TS NUMBERT
|
|||
TC ALARM
|
||||
OCT 02004
|
||||
TCF NOROTAT
|
||||
ALLJETS OCT 00110 # -U 6 13
|
||||
OCT 00022 # -V 2 9
|
||||
OCT 00204 # +U 5 14
|
||||
OCT 00041 # +V 1 10
|
||||
TYPEPOLY OCT 00125 # -X 1 5 9 13
|
||||
OCT 00252 # +X 2 6 10 14
|
||||
OCT 00146 # A 2 5 10 13
|
||||
OCT 00231 # B 1 6 9 14
|
||||
OCT 00377 # ALL 1 2 5 6 9 10 13 14
|
||||
ALLJETS OCT 00110 # -U 6 13
|
||||
OCT 00022 # -V 2 9
|
||||
OCT 00204 # +U 5 14
|
||||
|
||||
OCT 00041 # +V 1 10
|
||||
TYPEPOLY OCT 00125 # -X 1 5 9 13
|
||||
OCT 00252 # +X 2 6 10 14
|
||||
OCT 00146 # A 2 5 10 13
|
||||
OCT 00231 # B 1 6 9 14
|
||||
OCT 00377 # ALL 1 2 5 6 9 10 13 14
|
||||
|
||||
# THE FOLLOWING SETS THE INTERRUPT FLIP-FLOP AS SOON AS POSSIBLE, WHICH PERMITS A RETURN TO THE INTERRUPTED JOB.
|
||||
|
||||
|
|
@ -856,5 +857,4 @@ ENDJASK DXCH DAPARUPT
|
|||
COUNT* $$/DAP
|
||||
|
||||
MAKERUPT EXTEND
|
||||
EDRUPT MAKERUPT
|
||||
|
||||
EDRUPT MAKERUPT
|
||||
Loading…
Reference in New Issue