Proof ASSEMBLY_AND_OPERATION_INFORMATION (#337)
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@ -62,7 +62,7 @@
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# STABLE ORBIT - P38-P39
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# TROUBLE
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# P11
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# TP1 SEARCH
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# TPI SEARCH
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# P20-P25
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# P30,P37
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# P32-P33, P72-P73
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@ -77,14 +77,14 @@
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# P37,P70
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# S-BAND ANTENNA FOR CM
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# TVCDAPS
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# TVC INITIALIZE
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# TVCINITIALIZE
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# Page 3
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# TVC EXECUTIVE
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# TVC MASSPROP
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# TVC RESTARTS
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# TVC DAPS
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# TVC STROKE TEST
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# TVC ROLLDAP
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# TVCEXECUTIVE
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# TVCMASSPROP
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# TVCRESTARTS
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# TVCDAPS
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# TVCSTROKETEST
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# TVCROLLDAP
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# MYSUBS
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# RCS-CSM DIGITAL AUTOPILOT
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# AUTOMATIC MANEUVERS
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@ -190,7 +190,7 @@
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# 43 LOAD IMU ATT ERROR METERS
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# 44 SET SURFACE FLAG
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# 45 RESET SURFACE FLAG
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# 46 ESTABLISH G&C CONTROL
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# 46 ESTABLISH G+C CONTROL
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# 47 MOVE LM STATE VECTOR INTO CM STATE VECTOR.
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# 48 REQUEST DAP DATA LOAD ROUTINE (R03)
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# 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
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@ -250,14 +250,14 @@
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# IN THE FOLLOWING NOUN LIST THE :NO LOAD: RESTRICTION MEANS THE NOUN
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# CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
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# SCALE TYPE L (MIN/SEC) OR PP (2 INTEGERS).
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# IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22, OR 23
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# IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22 OR 23
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# MAY BE USED TO LOAD ANY OF THE NOUN:S COMPONENTS WHICH ARE NOT OF THE
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# ABOVE SCALE TYPES.
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# THE :DEC ONLY: RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
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# EVERY COMPONENT IN THE NOUN. (NOTE THAT :NO LOAD: IMPLIES :DEC ONLY:.)
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# NORMAL NOUNS COMPONENTS SCALE & DECIMAL POINT RESTRICTIONS
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#
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# NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
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# 00 NOT IN USE
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# 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .XXXXX FOR EACH
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# 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP XXXXX. FOR EACH
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@ -297,16 +297,12 @@
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# 0XX.XX SEC
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# 25 CHECKLIST 3COMP XXXXX. FOR EACH
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# (USED WITH PLEASE PERFORM ONLY)
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# Page 9
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# 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH
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# 27 SELF TEST ON/OFF SWITCH 1COMP XXXXX.
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# 28 SPARE
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# 29 XSM LAUNCH AZIMUTH 1COMP XXX.XX DEG DEC ONLY
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# Page 10
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# 30 TARGET CODES 3COMP XXXXX. FOR EACH
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# 31 TIME OF LANDING SITE 3COMP 00XXX. HRS DEC ONLY
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# 000XX. MIN MUST LOAD 3 COMPS
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@ -338,7 +334,7 @@
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# Page 11
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# MIXED NOUNS COMPONENTS SCALE & DECIMAL POINT RESTRICTIONS
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# MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
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#
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# 40 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
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# VG, XXXX.X FT/SEC
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@ -373,7 +369,7 @@
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# 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP XXX.XX DEG
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# 53 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY
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# RANGE RATE, XXXX.X FT/SEC
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# PHI XXX.X DEG
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# PHI XXX.XX DEG
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# 54 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY
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# RANGE RATE, XXXX.X FT/SEC
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# THETA XXX.XX DEG
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@ -388,9 +384,7 @@
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# DELTA V TPF XXXX.X FT/SEC
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# 59 DELTA VELOCITY LOS 3COMP XXXX.X FT/SEC FOR EA. DEC ONLY
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# 60 GMAX, 3COMP XXX.XX G DEC ONLY
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# Page 12
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# VPRED, XXXXX. FT/SEC
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# GAMMA EI XXX.XX DEG
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# 61 IMPACT LATITUDE, 3COMP XXX.XX DEG DEC ONLY
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@ -417,7 +411,7 @@
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# 68 COMMAND BANK ANGLE (BETA), 3COMP XXX.XX DEG DEC ONLY
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# INERTIAL VELOCITY (VI), XXXXX. FT/SEC
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# ALT RATE CHANGE (RDOT) XXXXX. FT/SEC
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# 69 BETA 3COMP XXX.XX DEG
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# 69 BETA 3COMP XXX.XX DEG DEC ONLY
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# DL XXX.XX G
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# VL XXXXX. FT/SEC
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# 70 STAR CODE, 3COMP OCTAL ONLY
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@ -441,9 +435,7 @@
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# 78 SPARE
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# 79 SPARE
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# 80 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
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# Page 13
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# VG XXXXX. FT/SEC
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# DELTA V (ACCUMULATED) XXXXX. FT/SEC
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# 81 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
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@ -451,7 +443,7 @@
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# 83 DELTA V (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
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# 84 DELTA V (OTHER VEHICLE) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
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# 85 VG (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
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# 86 DELTA V (LV) 3COMP XXXXX. FT/SEC FOR EACH DEC ONLY
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# 86 DELTA V(LV) 3COMP XXXXX. FT/SEC FOR EACH DEC ONLY
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# 87 MARK DATA SHAFT, 2COMP XXX.XX DEG
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# TRUNION XX.XXX DEG
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# 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .XXXXX FOR EACH DEC ONLY
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@ -468,7 +460,7 @@
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# 93 DELTA GYRO ANGLES 3COMP XX.XXX DEG FOR EACH
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# 94 NEW OPTICS ANGLES SHAFT 2COMP XXX.XX DEG
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# TRUNNION XX.XXX DEG
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# 95 PREFERRED ATTITUDE ICDU ANGLES 3COMP XXX.XX FOR EACH
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# 95 PREFERRED ATTITUDE ICDU ANGLES 3COMP XXX.XX FOR FOR EACH
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# 96 +X-AXIS ATTITUDE ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
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# 97 SYSTEM TEST INPUTS 3COMP XXXXX. FOR EACH
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# 98 SYSTEM TEST RESULTS AND INPUTS 3COMP XXXXX.
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@ -521,7 +513,7 @@
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# 34 DSPTEM1 K
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# 35 TTOGO K
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# 36 TIME2 K
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# 37 TTP1 K
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# 37 TTPI K
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# 38 TET K
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# 39 T3TOT4 K
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@ -577,9 +569,7 @@
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# 57 1 DELTAR Q
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# 58 1 POSTTPI Q
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# 2 DELVTPI S
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# Page 16
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# 3 DELVTPF S
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# 59 1 DVLOS S
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# 2 DVLOS +2 S
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@ -630,9 +620,7 @@
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# 75 1 DIFFALT Q
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# 2 T1TOT2 L
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# 3 T2TOT3 L
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# Page 17
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# 76 SPARE
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# 77 SPARE
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# 78 SPARE
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@ -660,9 +648,9 @@
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# 3 DELVLVC +4 P
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# 87 1 MRKBUF1 +3 D
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# 2 MRKBUF1 +5 J
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# 88 1 STARSAV ZZ
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# 2 STARSAV +2 ZZ
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# 3 STARSAV +4 ZZ
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# 88 1 STARSAV3 ZZ
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# 2 STARSAV3 +2 ZZ
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# 3 STARSAV3 +4 ZZ
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# 89 1 LANDLAT G
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# 2 LANDLONG G
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# 3 LANDALT JJ
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@ -683,9 +671,7 @@
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# 3 PRAXIS +2 D
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# 96 1 CPHIX D
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# 2 CPHIX +1 D
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# Page 18
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# 3 CPHIX +2 D
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# 97 1 DSPTEM1 C
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# 2 DSPTEM1 +1 C
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@ -750,9 +736,7 @@
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# LOADED.
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#
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# -K-
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# Page 20
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# TIME (HR, MIN, SEC) 00XXX. HR DP BIT 1 OF LOW REGISTER =
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# 000XX. MIN -2
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# 0XX.XX SEC 10 SEC
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@ -795,16 +779,14 @@
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# 2 METERS/CENTI-SEC
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#
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# -Q-
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# POSITION 4 XXXX.XX NAUTICAL MILES DP BIT 1 OF LOW REGISTER =
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# POSITION 4 XXXX.X NAUTICAL MILES DP BIT 1 OF LOW REGISTER =
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# 2 METERS
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#
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# -S-
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# VELOCITY 3 XXXX.X FT/SEC DP BIT 1 OF HIGH REGISTER =
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# -7
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# 2 METERS/CENTI-SEC
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# Page 21
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# -T- -2
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# G XXX.XX G SP BIT 1 = 10 G
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# (MAX 163.83)
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@ -846,7 +828,7 @@
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# 2 INTEGERS +XXBYY DP BIT 1 OF HIGH REGISTER =
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# (B IS A BLANK 1 UNIT OF XX
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# POSITION. DECIMAL BIT 1 OF LOW REGISTER =
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# ONLY, DISPLAY, OR 1 UNIT OF YY
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# ONLY, DISPLAY OR 1 UNIT OF YY
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# MONITOR ONLY. CANNOT (EACH REGISTER MUST
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# BE LOADED.) CONTAIN A POSITIVE INTEGER
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# (MAX 99B99) LESS THAN 100)
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@ -855,9 +837,7 @@
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# VELOCITY/2VS XXXXX. FEET/SEC DP FRACTIONAL PART OF
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# (MAX 51532.) 2VS FEET/SEC
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# (VS = 25766.1973)
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# Page 22
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# -VV-
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# POSITION8 XXXX.X NAUT MI DP BIT 1 OF LOW REGISTER =
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# -28
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@ -913,7 +893,7 @@
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# 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT ALARM
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# 00210 IMU NOT OPERATING IMU MODE SWITCH, IMU-2, R02, P51 ALARM,VARALARM
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# 00211 COARSE ALIGN ERROR - DRIVE > 2 DEGREES IMU MODE SWITCH ALARM
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# 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH,T4RUPT ALARM
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# 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH,T4RPT ALARM
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# 00213 IMU NOT OPERATING WITH TURN-ON REQUEST T4RUPT ALARM
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# 00214 PROGRAM USING IMU WHEN TURNED OFF T4RUPT ALARM
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# 00215 PREFERRED ORIENTATION NOT SPECIFIED P52,P54 ALARM
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# 00401 DESIRED GIMBAL ANGLES YIELD GIMBAL LOCK IMF ALIGN, IMU-2 ALARM
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# 00404 TARGET OUT OF VIEW - TRUN ANGLE > 90 DEG R52 PRIOLARM
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# 00405 TWO STARS NOT AVAILABLE P52,P54 ALARM
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# 00406 REND NAVIGATION NOT OPERATING P21,R23 ALARM
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# 00406 REND NAVIGATION NOT OPERATING R21,R23 ALARM
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# 00407 AUTO OPTICS REQUEST TRUN ANGLE > 50 DEG. R52 ALARM
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# 00421 W-MATRIX OVERFLOW INTEGRV ALARM
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# 00421 W-MATRIX OVERFLOW INTEGRV VARALARM
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# 00430 * INTEG. ABORT DUE TO SUBSURFACE S. V. ALL CALLS TO INTEG POODOO
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# 00600 IMAGINARY ROOTS ON FIRST ITERATION P32, P72 VARALARM
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# 00601 PERIGEE ALTITUDE LT PMIN1 P32,P72, VARALARM
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@ -934,16 +914,14 @@
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# 00605 NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM P32,P72,P37 VARALARM
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# 00606 DV EXCEEDS MAXIMUM P32,P72 VARALARM
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# 00607 * NO SOLN FROM TIME-THETA OR TIME-RADIUS TIMETHET,TIMERAD POODOO
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# Page 24
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# 00610 * LAMBDA LESS THAN UNITY P37 POODOO
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# 00611 NO TIG FOR GIVEN ELEV ANGLE P34,P74 VARALARM
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# 00612 STATE VECTOR IN WRONG SPHERE OF INFLUENCE P37 VARALARM
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# 00613 REENTRY ANGLE OUT OF LIMITS P37 VARALARM
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# 00777 PIPA FAIL CAUSED ISS WARNING. T4RUPT VARALARM
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# 01102 CMC SELF TEST ERROR ALARM2
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# 01103 * UNUSED CCS BRANCH EXECUTED ABORT ALARM2
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# 01103 * UNUSED CCS BRANCH EXECUTED ABORT POODOO
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# 01104 * DELAY ROUTINE BUSY EXEC BAILOUT
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# 01105 DOWNLINK TOO FAST T4RUPT ALARM
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# 01106 UPLINK TOO FAST T4RUPT ALARM
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@ -1000,7 +978,7 @@
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# 00204 PERFORM SPS GIMBAL TRIM
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# 00403 SWITCH OPTICS TO MANUAL OR ZERO
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# SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
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# PERFORM DENOTES START OF END OF A TASK
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# PERFORM DENOTES START OR END OF A TASK
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# KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
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# Page 26
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@ -1027,6 +1005,6 @@
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# 00007 SPECIFY PROPULSION SYSTEM 1=SPS 2=RCS P37 COLOSSUS
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# 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
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# 2=TWO BODIES 3=ONE BODY + G
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# 00011 SPEC. SEPARATION MONITOR PHASE 1=DELTAV 2=STATE VECTOR UPDATE P46 LUMINARY
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# 00011 SPECIFY SEPARATION MONITOR PHASE 1=DELTAV 2=STATE VECTOR UPDATE P46 LUMINARY
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# 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
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# ORBIT TO PASS OVER LM
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