Notations on the program listing read, in part:
GAP: ASSEMBLE REVISION 56 OF AGC PROGRAM ZERLINA BY ZOROASTER 9:12 OCT. 21,1970Note that the date is the date of the printout, not the date of the program revision.
Source Code
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These source-code files were transcribed from a printout in Don Eyles's personal
collection, scanned by archive.org, and financially sponsored by Linden Sims.
A team of volunteers performed the transcription and proof-reading. The scanned
page images are available at
the Virtual AGC Project website, as well as higher-quality (but much larger)
images at
the Virtual AGC Project's collection in the Internet Archive. Report any problems by creating
"issues" at
the Virtual AGC Project's GitHub Repository. Notations on the program listing read, in part: GAP: ASSEMBLE REVISION 56 OF AGC PROGRAM ZERLINA BY ZOROASTER 9:12 OCT. 21,1970Note that the date is the date of the printout, not the date of the program revision. |
000067,000002: ## Copyright: Public domain.
000068,000003: ## Filename: ASSEMBLY_AND_OPERATION_INFORMATION.agc
000069,000004: ## Purpose: A log section of Zerlina 56, the final revision of
000070,000005: ## Don Eyles's offline development program for the variable
000071,000006: ## guidance period servicer. It also includes a new P66 with LPD
000072,000007: ## (Landing Point Designator) capability, based on an idea of John
000073,000008: ## Young's. Neither of these advanced features were actually flown,
000074,000009: ## but Zerlina was also the birthplace of other big improvements to
000075,000010: ## Luminary including the terrain model and new (Luminary 1E)
000076,000011: ## analog display programs. Zerlina was branched off of Luminary 145,
000077,000012: ## and revision 56 includes all changes up to and including Luminary
000078,000013: ## 183. It is therefore quite close to the Apollo 14 program,
000079,000014: ## Luminary 178, where not modified with new features.
000080,000015: ## Reference: pp. 2-27
000081,000016: ## Assembler: yaYUL
000082,000017: ## Contact: Ron Burkey <info@sandroid.org>.
000083,000018: ## Website: www.ibiblio.org/apollo/index.html
000084,000019: ## Mod history: 2017-07-28 MAS Created from Luminary 210.
000085,000020: ## 2017-08-12 MAS Updated for Zerlina 56
000086,000021:
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000088,000023: # THIS LGC PROGRAM IS INTENDED FOR USE IN THE LM DURING THE MANNED LUNAR LANDING MISSION OR ANY SUBSET THEREOF.
000089,000024: # THE DETAILS OF IMPLEMENTATION ARE SPECIFIED IN REPORT R-567, AS AMENDED.
000090,000025:
000091,000026:
000092,000027: # GUIDANCE SYSTEM OPERATIONS PLAN
000093,000028: # FOR MANNED LM EARTH ORBITAL AND LUNAR MISSIONS
000094,000029: # USING PROGRAM LUMINARY
000095,000030:
000096,000031:
000097,000032: # THIS PROGRAM AND R-567 HAVE BEEN PREPARED BY THE INSTRUMENTATION LABORATORY, MASSACHUSETTS INSTITUTE OF
000098,000033: # TECHNOLOGY 75 CAMBRIDGE PARKWAY, CAMBRIDGE, MASSACHUSETTS UNDER PROJECT55-238-70, SPONSORED BY THE MANNED
000099,000034: # SPACECRAFT CENTER OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, CONTRACT NAS 9-4065.
000100,000035:
000101,000036:
000102,000037: # THIS PROGRAM IS A VERSION OF LUMINARY FOR DEVELOPING A NEW VARIABLE GUIDANCE PERIOD SERVICER.
000103,000038:
000104,000039: # TABLE OF LOG CARDS
000105,000040:
000106,000041: # ABSOLUTE ADDRESSES FOR UPDATE PROGRAM
000107,000042: # ASSEMBLY AND OPERATION INFORMATION
000108,000043: # TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
000109,000044: # CONTROLLED CONSTANTS
000110,000045: # INPUT/OUTPUT CHANNEL BIT DESCRIPTIONS
000111,000046: # FLAGWORD ASSIGNMENTS
000112,000047: # SUBROUTINE CALLS
000113,000048:
000114,000049:
000115,000050: # TABLE OF SUBROUTINE LOG SECTIONS
000116,000051: # ZERASE
000117,000052: # ERASABLE ASSIGNMENTS
000118,000053: # ZERLAID
000119,000054: # INTERRUPT LEAD INS
000120,000055: # T4RUPT PROGRAM
000121,000056: # RCS FAILURE MONITOR
000122,000057: # DOWNLINK LISTS
000123,000058: # AGS INITIALIZATION
000124,000059: # FRESH START AND RESTART
000125,000060: # RESTART TABLES
000126,000061: # AOTMARK
000127,000062: # EXTENDED VERBS
000128,000063: # PINBALL NOUN TABLES
000129,000064: # LEM GEOMETRY
000130,000065: # IMU COMPENSATION PACKAGE
000131,000066: # R63
000132,000067: # ATTITUDE MANEUVER ROUTINE
000133,000068: # GIMBAL LOCK AVOIDANCE
000134,000069: # KALCMANU STEERING
000135,000070: # SYSTEM TEST STANDARD LEAD INS
000136,000071: # IMU PERFORMANCE TESTS 2
000137,000072: # IMU PERFORMANCE TESTS 4
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000139,000074: # PINBALL GAMES BUTTONS AND LIGHTS
000140,000075: # R60,R62
000141,000076: # S-BAND ANTENNA FOR LM
000142,000077: # ZLEMP20S
000143,000078: # RADAR LEADIN ROUTINES
000144,000079: # P20-P25
000145,000080: # LEMP30S
000146,000081: # P30,P37
000147,000082: # P32-P35, P72-P75
000148,000083: # KISSING
000149,000084: # GROUND TRACKING DETERMINATION PROGRAM - P21
000150,000085: # P34-P35, P74-P75
000151,000086: # R31
000152,000087: # P76
000153,000088: # R30
000154,000089: # ZFLY
000155,000090: # BURN, BABY, BURN -- MASTER IGNITION ROUTINE
000156,000091: # P40-P47
000157,000092: # THE LUNAR LANDING
000158,000093: # THROTTLE CONTROL ROUTINES
000159,000094: # LUNAR LANDING GUIDANCE EQUATIONS
000160,000095: # P70-P71
000161,000096: # P12
000162,000097: # ASCENT GUIDANCE
000163,000098: # SERVICER
000164,000099: # LANDING ANALOG DISPLAYS
000165,000100: # FINDCDUW - GUIDAP INTERFACE
000166,000101: # LEMP50S
000167,000102: # P51-P53
000168,000103: # LUNAR AND SOLAR EPHEMERIDES SUBROUTINES
000169,000104: # SKIPPER
000170,000105: # DOWN-TELEMETRY PROGRAM
000171,000106: # INTER-BANK COMMUNICATION
000172,000107: # INTERPRETER
000173,000108: # FIXED-FIXED CONSTANT POOL
000174,000109: # INTERPRETIVE CONSTANTS
000175,000110: # SINGLE PRECISION SUBROUTINES
000176,000111: # EXECUTIVE
000177,000112: # WAITLIST
000178,000113: # LATITUDE LONGITUDE SUBROUTINES
000179,000114: # PLANETARY INERTIAL ORIENTATION
000180,000115: # MEASUREMENT INCORPORATION
000181,000116: # CONIC SUBROUTINES
000182,000117: # INTEGRATION INITIALIZATION
000183,000118: # ORBITAL INTEGRATION
000184,000119: # INFLIGHT ALIGNMENT ROUTINES
000185,000120: # POWERED FLIGHT SUBROUTINES
000186,000121: # TIME OF FREE FALL
000187,000122: # AGC BLOCK TWO SELF-CHECK
000188,000123: # PHASE TABLE MAINTENANCE
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000190,000125: # RESTARTS ROUTINE
000191,000126: # IMU MODE SWITCHING ROUTINES
000192,000127: # KEYRUPT, UPRUPT
000193,000128: # DISPLAY INTERFACE ROUTINES
000194,000129: # SERVICE ROUTINES
000195,000130: # ALARM AND ABORT
000196,000131: # UPDATE PROGRAM
000197,000132: # RTB OP CODES
000198,000133: # ZLMDAP1
000199,000134: # T6-RUPT PROGRAMS
000200,000135: # DAP INTERFACE SUBROUTINES
000201,000136: # DAPIDLER PROGRAM
000202,000137: # P-AXIS RCS AUTOPILOT
000203,000138: # Q,R-AXIS RCS AUTOPILOT
000204,000139: # TJET LAW
000205,000140: # KALMAN FILTER
000206,000141: # TRIM GIMBAL CONTROL SYSTEM
000207,000142: # AOSTASK AND AOSJOB
000208,000143: # SPS BACK-UP RCS CONTROL
000209,000144:
000210,000145:
000211,000146: # SYMBOL TABLE LISTING
000212,000147: # UNREFERENCED SYMBOL LISTING
000213,000148: # ERASABLE & EQUALS CROSS-REFERENCE TABLE
000214,000149: # SUMMARY OF SYMBOL TABLE LISTINGS
000215,000150: # MEMORY TYPE & AVAILABLITY DISPLAY
000216,000151: # COUNT TABLE
000217,000152: # PARAGRAPHS GENERATED FOR THIS ASSEMBLY
000218,000153: # OCTAL LISTING
000219,000154: # OCCUPIED LOCATIONS TABLE
000220,000155: # SUBROS CALLED & PROGRAM STATUS
000221,000156:
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000223,000158: # VERB LIST FOR LUMINARY
000224,000159:
000225,000160: # REGULAR VERBS
000226,000161:
000227,000162: # 00 NOT IN USE
000228,000163: # 01 DISPLAY OCTAL COMP 1 IN R1
000229,000164: # 02 DISPLAY OCTAL COMP 2 IN R1
000230,000165: # 03 DISPLAY OCTAL COMP 3 IN R1
000231,000166: # 04 DISPLAY OCTAL COMP 1,2 IN R1,R2
000232,000167: # 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3
000233,000168: # 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000234,000169: # 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY)
000235,000170: # 08
000236,000171: # 09
000237,000172: # 10
000238,000173: # 11 MONITOR OCTAL COMP 1 IN R1
000239,000174: # 12 MONITOR OCTAL COMP 2 IN R1
000240,000175: # 13 MONITOR OCTAL COMP 3 IN R1
000241,000176: # 14 MONITOR OCTAL COMP 1,2 IN R1,R2
000242,000177: # 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3
000243,000178: # 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000244,000179: # 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY)
000245,000180: # 18
000246,000181: # 19
000247,000182: # 20
000248,000183: # 21 LOAD COMPONENT 1 INTO R1
000249,000184: # 22 LOAD COMPONENT 2 INTO R2
000250,000185: # 23 LOAD COMPONENT 3 INTO R3
000251,000186: # 24 LOAD COMPONENT 1,2 INTO R1,R2
000252,000187: # 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3
000253,000188: # 26
000254,000189: # 27 DISPLAY FIXED MEMORY
000255,000190: # 28
000256,000191: # 29
000257,000192: # 30 REQUEST EXECUTIVE
000258,000193: # 31 REQUEST WAITLIST
000259,000194: # 32 RECYCLE PROGRAM
000260,000195: # 33 PROCEED WITHOUT DSKY INPUTS
000261,000196: # 34 TERMINATE FUNCTION
000262,000197: # 35 TEST LIGHTS
000263,000198: # 36 REQUEST FRESH START
000264,000199: # 37 CHANGE PROGRAM (MAJOR MODE)
000265,000200: # 38
000266,000201: # 39
000267,000202:
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000269,000204: # EXTENDED VERBS
000270,000205:
000271,000206: # 40 ZERO CDU-S
000272,000207: # 41 COARSE ALIGN CDU-S
000273,000208: # 42 FINE ALIGN IMU
000274,000209: # 43 LOAD IMU ATT ERROR METERS
000275,000210: # 44 TERMINATE RR CONTINUOUS DESIGNATE (V41N72 OPTION 2)
000276,000211: # 45
000277,000212: # 46
000278,000213: # 47 INITIALIZE AGS (R47)
000279,000214: # 48 REQUEST DAP DATA LOAD ROUTINE (R03)
000280,000215: # 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
000281,000216: # 50 PLEASE PERFORM
000282,000217: # 51
000283,000218: # 52 MARK X-RETICLE
000284,000219: # 53 MARK Y-RETICLE
000285,000220: # 54 MARK X OR Y-RETICLE
000286,000221: # 55 INCREMENT AGC TIME (DECIMAL)
000287,000222: # 56 TERMINATE TRACKING (P20 + P25)
000288,000223: # 57 PERMIT LANDING RADAR UPDATES
000289,000224: # 58 INHIBIT LANDING RADAR UPDATES
000290,000225: # 59 COMMAND LR TO POSITION 2.
000291,000226: # 60 DISPLAY VEHICLE ATTITUDE RATES ON FDAI ERROR NEEDLES.
000292,000227: # 61 DISPLAY DAP FOLLOWING ATTITUDE ERRORS.
000293,000228: # 62 DISPLAY TOTAL ATTITUDE ERRORS WITH RESPECT TO NOUN 22.
000294,000229: # 63 SAMPLE RADAR ONCE PER SECOND (R04).
000295,000230: # 64 REQUEST S-BAND ANTENNA ROUTINE (R05)
000296,000231: # 65 DISABLE U AND V JET FIRINGS DURING DPS BURNS.
000297,000232: # 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
000298,000233: # 67 DISPLAY W MATRIX
000299,000234: # 68 DISABLE TERRAIN MODEL
000300,000235: # 69 CAUSE RESTART
000301,000236: # 70 UPDATE LIFTOFF TIME
000302,000237: # 71 UNIVERSAL UPDATE-BLOCK ADR
000303,000238: # 72 UNIVERSAL UPDATE-SINGLE ADR
000304,000239: # 73 UPDATE AGC TIME (OCTAL)
000305,000240: # 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK
000306,000241: # 75 ENABLE U AND V JET FIRINGS DURING DPS BURNS.
000307,000242: # 76 MINIMUM IMPULSE COMMAND MODE
000308,000243: # 77 RATE COMMAND AND ATTITUDE HOLD MODE
000309,000244: # 78 LR SPURIOUS RETURN TEST START (R77)
000310,000245: # 79 LR SPURIOUS RETURN TEST STOP
000311,000246: # 80 UPDATE LEM STATE VECTOR
000312,000247: # 81 UPDATE CSM STATE VECTOR
000313,000248: # 82 REQUEST ORBIT PARAM DISPLAY (R30)
000314,000249: # 83 REQUEST REND PARAM DISPLAY (R31)
000315,000250: # 84
000316,000251: # 85 DISPLAY RR LOS AZ AND ELEV
000317,000252: # 86
000318,000253: # 87
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000320,000255: # 88
000321,000256: # 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
000322,000257: # 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
000323,000258: # 91 DISPLAY BANK SUM
000324,000259: # 92 OPERATE IMU PERFORMANCE TEST (P07)
000325,000260: # 93 ENABLE W MATRIX INITIALIZATION
000326,000261: # 94
000327,000262: # 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
000328,000263: # 96 INTERRUPT INTEGRATION AND GO TO POO
000329,000264: # 97 PERFORM ENGINE FAIL PROCEDURE
000330,000265: # 98
000331,000266: # 99 PLEASE ENABLE ENGINE
000332,000267:
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000334,000269: # IN THE FOLLOWING NOUN LIST THE :NO LOAD: RESTRICTION MEANS THE NOUN
000335,000270: # CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
000336,000271: # SCALE TYPE L (MIN/SEC), PP (2 INTEGERS) OR TT (LANDING RADAR POSITION).
000337,000272: # IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22 OR 23
000338,000273: # MAY BE USED TO LOAD ANY OF THE NOUN:S COMPONENTS WHICH ARE NOT OF THE
000339,000274: # ABOVE SCALE TYPES.
000340,000275: # THE :DEC ONLY: RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
000341,000276: # EVERY COMPONENT IN THE NOUN. (NOTE THAT :NO LOAD: IMPLIES :DEC ONLY:.)
000342,000277:
000343,000278: # NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000344,000279:
000345,000280: # 00 NOT IN USE
000346,000281: # 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .XXXXX FOR EACH
000347,000282: # 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP XXXXX. FOR EACH
000348,000283: # 03 SPECIFY MACHINE ADDRESS (DEGREES) 3COMP XXX.XX DEG FOR EACH
000349,000284: # 04 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000350,000285: # 05 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000351,000286: # 06 OPTION CODE 3COMP OCTAL ONLY FOR EACH
000352,000287: # LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER
000353,000288: # 07 ECADR OF WORD TO BE MODIFIED 3COMP OCTAL ONLY FOR EACH
000354,000289: # ONES FOR BITS TO BE MODIFIED
000355,000290: # 1 TO SET OR 0 TO RESET SELECTED BITS
000356,000291: # 08 ALARM DATA 3COMP OCTAL ONLY FOR EACH
000357,000292: # 09 ALARM CODES 3COMP OCTAL ONLY FOR EACH
000358,000293: # 10 CHANNEL TO BE SPECIFIED 1COMP OCTAL ONLY
000359,000294: # 11 TIG OF CSI 3COMP 00XXX. HRS DEC ONLY
000360,000295: # 000XX. MIN MUST LOAD 3 COMPS
000361,000296: # 0XX.XX SEC
000362,000297: # 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH
000363,000298: # (USED BY EXTENDED VERBS ONLY)
000364,000299: # 13 TIG OF CDH 3COMP 00XXX. HRS DEC ONLY
000365,000300: # 000XX. MIN MUST LOAD 3 COMPS
000366,000301: # 0XX.XX SEC
000367,000302: # 14 CHECKLIST 3COMP XXXXX. FOR EACH
000368,000303: # (USED BY EXTENDED VERBS ONLY)
000369,000304: # (NOUN 25 IS PASTED AFTER DISPLAY)
000370,000305: # 15 INCREMENT MACHINE ADDRESS 1COMP OCTAL ONLY
000371,000306: # 16 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000372,000307: # (USED BY EXTENDED VERBS ONLY) 000XX. MIN MUST LOAD 3 COMPS
000373,000308: # 0XX.XX SEC
000374,000309: # 17 SPARE
000375,000310: # 18 AUTO MANEUVER BALL ANGLES 3COMP XXX.XX DEG FOR EACH
000376,000311: # 19 SPARE
000377,000312: # 20 ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000378,000313: # 21 PIPAS 3COMP XXXXX. PULSES FOR EACH
000379,000314: # 22 NEW ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000380,000315: # 23 SPARE
000381,000316: # 24 DELTA TIME FOR AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000382,000317: # 000XX. MIN MUST LOAD 3 COMPS
000383,000318: # 0XX.XX SEC
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000385,000320: # 25 CHECKLIST 3COMP XXXXX. FOR EACH
000386,000321: # (USED WITH PLEASE PERFORM ONLY)
000387,000322: # 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH
000388,000323: # 27 SELF TEST ON/OFF SWITCH 1COMP XXXXX.
000389,000324: # 28 SPARE
000390,000325: # 29 SPARE
000391,000326: # 30 SPARE
000392,000327: # 31 SPARE
000393,000328: # 32 TIME FROM PERIGEE 3COMP 00XXX. HRS DEC ONLY
000394,000329: # 000XX. MIN MUST LOAD 3 COMPS
000395,000330: # 0XX.XX SEC
000396,000331: # 33 TIME OF IGNITION 3COMP 00XXX. HRS DEC ONLY
000397,000332: # 000XX. MIN MUST LOAD 3 COMPS
000398,000333: # 0XX.XX SEC
000399,000334: # 34 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000400,000335: # 000XX. MIN MUST LOAD 3 COMPS
000401,000336: # 0XX.XX SEC
000402,000337: # 35 TIME FROM EVENT 3COMP 00XXX. HRS DEC ONLY
000403,000338: # 000XX. MIN MUST LOAD 3 COMPS
000404,000339: # 0XX.XX SEC
000405,000340: # 36 TIME OF AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000406,000341: # 000XX. MIN MUST LOAD 3 COMPS
000407,000342: # 0XX.XX SEC
000408,000343: # 37 TIG OF TPI 3COMP 00XXX. HRS DEC ONLY
000409,000344: # 000XX. MIN MUST LOAD 3 COMPS
000410,000345: # 0XX.XX SEC
000411,000346: # 38 TIME OF STATE BEING INTEGRATED 3COMP 00XXX. HRS DEC ONLY
000412,000347: # 000XX. MIN MUST LOAD 3 COMPS
000413,000348: # 0XX.XX SEC
000414,000349: # 39 SPARE
000415,000350:
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000417,000352: # MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000418,000353:
000419,000354: # 40 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000420,000355: # VG, XXXX.X FT/SEC
000421,000356: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000422,000357: # 41 TARGET AZIMUTH, 2COMP XXX.XX DEG (FOR SYSTEM TEST)
000423,000358: # ELEVATION XX.XXX DEG
000424,000359: # 42 APOGEE, 3COMP XXXX.X NAUT MI DEC ONLY
000425,000360: # PERIGEE, XXXX.X NAUT MI
000426,000361: # DELTA V (REQUIRED) XXXX.X FT/SEC
000427,000362: # 43 LATITUDE, 3COMP XXX.XX DEG DEC ONLY
000428,000363: # LONGITUDE, XXX.XX DEG
000429,000364: # ALTITUDE XXXX.X NAUT MI
000430,000365: # 44 APOGEE, 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000431,000366: # PERIGEE, XXXX.X NAUT MI
000432,000367: # TFF XXBXX MIN/SEC
000433,000368: # 45 MARKS, 3COMP XXXXX. NO LOAD, DEC ONLY
000434,000369: # TFI OF NEXT BURN XXBXX MIN/SEC
000435,000370: # MGA XXX.XX DEG
000436,000371: # 46 AUTOPILOT CONFIGURATION 1COMP OCTAL ONLY
000437,000372: # 47 LEM WEIGHT, 2COMP XXXXX. LBS DEC ONLY
000438,000373: # CSM WEIGHT XXXXX. LBS
000439,000374: # 48 GIMBAL PITCH TRIM, 2COMP XXX.XX DEG DEC ONLY
000440,000375: # GIMBAL ROLL TRIM XXX.XX DEG
000441,000376: # 49 DELTA R, 3COMP XXXX.X NAUT MI DEC ONLY
000442,000377: # DELTA V, XXXX.X FT/SEC
000443,000378: # RADAR DATA SOURCE CODE XXXXX.
000444,000379: # 50 SPARE
000445,000380: # 51 S-BAND ANTENNA ANGLES PITCH 2COMP XXX.XX DEG DEC ONLY
000446,000381: # YAW XXX.XX DEG
000447,000382: # 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP XXX.XX DEG
000448,000383: # 53 SPARE
000449,000384: # 54 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY
000450,000385: # RANGE RATE, XXXX.X FT/SEC
000451,000386: # THETA XXX.XX DEG
000452,000387: # 55 NO. OF APSIDAL CROSSINGS 3COMP XXXXX. DEC ONLY
000453,000388: # ELEVATION ANGLE XXX.XX DEG
000454,000389: # CENTRAL ANGLE OF PASSIVE VEHICLE XXX.XX DEG
000455,000390: # 56 RR LOS AZIMUTH 2COMP XXX.XX DEG
000456,000391: # ELEVATION XXX.XX DEG
000457,000392: # 57 SPARE
000458,000393: # 58 PERIGEE ALT (POST TPI) 3COMP XXXX.X NAUT MI DEC ONLY
000459,000394: # DELTA V TPI XXXX.X FT/SEC
000460,000395: # DELTA V TPF XXXX.X FT/SEC
000461,000396: # 59 DELTA VELOCITY LOS 3COMP XXXX.X FT/SEC FOR EA. DEC ONLY
000462,000397: # 60 FORWARD VELOCITY - LPD ANGLE 3COMP XXBXX NO LOAD, DEC ONLY
000463,000398: # ALTITUDE RATE XXXX.X FT/SEC
000464,000399: # COMPUTED ALTITUDE XXXXX. FEET
000465,000400: # 61 TIME TO GO IN BRAKING PHASE 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000466,000401: # TIME FROM IGNITION XXBXX MIN/SEC
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000468,000403: # CROSS RANGE DISTANCE XXXX.X NAUT MI
000469,000404: # 62 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC NO LOAD, DEC ONLY
000470,000405: # TIME FROM IGNITION XXBXX MIN/SEC
000471,000406: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000472,000407: # 63 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000473,000408: # ALTITUDE RATE XXXX.X FT/SEC
000474,000409: # COMPUTED ALTITUDE XXXXX. FEET
000475,000410: # 64 TIME LEFT FOR REDESIGNATION- LPD ANGLE 3COMP XXBXX NO LOAD, DEC ONLY
000476,000411: # ALTITUDE RATE XXXX.X FT/SEC
000477,000412: # COMPUTED ALTITUDE XXXXX. FEET
000478,000413: # 65 SAMPLED AGC TIME 3COMP 00XXX. HRS DEC ONLY
000479,000414: # (FETCHED IN INTERRUPT) 000XX. MIN MUST LOAD 3 COMPS
000480,000415: # 0XX.XX SEC
000481,000416: # 66 LR RANGE 2COMP XXXXX. FEET NO LOAD, DEC ONLY
000482,000417: # POSITION +0000X
000483,000418: # 67 LRVX 3COMP XXXXX. FT/SEC
000484,000419: # LRVY XXXXX. FT/SEC
000485,000420: # LRVZ XXXXX. FT/SEC
000486,000421: # 68 SLANT RANGE TO LANDING SITE 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000487,000422: # TIME TO GO IN BRAKING PHASE XXBXX MIN/SEC
000488,000423: # LR ALTITUDE - COMPUTED ALTITUDE XXXXX. FEET
000489,000424: # 69 LANDING SITE CORRECTION, Z-COMPONENT 3COMP XXXXX. FEET DEC ONLY
000490,000425: # LANDING SITE CORRECTION, Y-COMPONENT XXXXX. FEET
000491,000426: # LANDING SITE CORRECTION, X-COMPONENT XXXXX. FEET
000492,000427: # 70 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000493,000428: # 71 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000494,000429: # 72 RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000495,000430: # SHAFT ANGLE XXX.XX DEG
000496,000431: # 73 NEW RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000497,000432: # SHAFT ANGLE XXX.XX DEG
000498,000433: # 74 TIME FROM IGNITION 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000499,000434: # YAW AFTER VEHICLE RISE XXX.XX DEG
000500,000435: # PITCH AFTER VEHICLE RISE XXX.XX DEG
000501,000436: # 75 DELTA ALTITUDE CDH 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000502,000437: # DELTA TIME (CDH-CSI OR TPI-CDH) XXBXX MIN/SEC
000503,000438: # DELTA TIME (TPI-CDH OR TPI-NOMTPI) XXBXX MIN/SEC
000504,000439: # 76 DESIRED HORIZONTAL VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000505,000440: # DESIRED RADIAL VELOCITY XXXX.X FT/SEC
000506,000441: # CROSS-RANGE DISTANCE XXXX.X NAUT MI
000507,000442: # 77 TIME TO ENGINE CUTOFF 2COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000508,000443: # VELOCITY NORMAL TO CSM PLANE XXXX.X FT/SEC
000509,000444: # 78 RR RANGE 3COMP XXX.XX NAUT MI NO LOAD, DEC ONLY
000510,000445: # RANGE RATE XXXX.X FT/SEC
000511,000446: # TIME FROM IGNITION XXBXX MIN/SEC
000512,000447: # 79 CURSOR ANGLE 3COMP XXX.XX DEG DEC ONLY
000513,000448: # SPIRAL ANGLE XXX.XX DEG
000514,000449: # POSITION CODE XXXXX.
000515,000450: # 80 DATA INDICATOR, 2COMP XXXXX.
000516,000451: # OMEGA XXX.XX DEG
000517,000452: # 81 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
|
|
Page 12 |
000519,000454: # 82 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000520,000455: # 83 DELTA V (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000521,000456: # 84 DELTA V (OTHER VEHICLE) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000522,000457: # 85 VG (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000523,000458: # 86 VG (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000524,000459: # 87 BACKUP OPTICS LOS AZIMUTH 2COMP XXX.XX DEG
000525,000460: # ELEVATION XXX.XX DEG
000526,000461: # 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .XXXXX FOR EACH DEC ONLY
000527,000462: # 89 LANDMARK LATITUDE 3COMP XX.XXX DEG DEC ONLY
000528,000463: # LONGITUDE/2 XX.XXX DEC
000529,000464: # ALTITUDE XXX.XX NAUT MI
000530,000465: # 90 Y 3COMP XXX.XX NM DEC ONLY
000531,000466: # Y DOT XXXX.X FPS
000532,000467: # PSI XXX.XX DEG
000533,000468: # 91 ALTITUDE 3COMP XXXXXB. NAUT MI
000534,000469: # VELOCITY XXXXX. FT/SEC
000535,000470: # FLIGHT PATH ANGLE XXX.XX DEG
000536,000471: # 92 PCT FTP(10,5KLB) AT PRESENT THRUST 3COMP XXXXX.
000537,000472: # ALTITUDE RATE XXXX.X FT/SEC
000538,000473: # COMPUTED ALTITUDE XXXXX.FEET
000539,000474: # 93 DELTA GYRO ANGLES 3COMP XX.XXX DEG FOR EACH
000540,000475: # 94 SPARE
000541,000476: # 95 SPARE
000542,000477: # 96 SPARE
000543,000478: # 97 SYSTEM TEST INPUTS 3COMP XXXXX. FOR EACH
000544,000479: # 98 SYSTEM TEST RESULTS AND INPUTS 3COMP XXXXX.
000545,000480: # .XXXXX
000546,000481: # XXXXX.
000547,000482: # 99 RMS IN POSITION 3COMP XXXXX.FT DEC ONLY
000548,000483: # RMS IN VELOCITY XXXX.X FT/SEC
000549,000484: # RMS IN BIAS XX.XXX RADIANS
000550,000485:
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Page 13 |
000552,000487: # REGISTERS AND SCALING FOR NORMAL NOUNS
000553,000488:
000554,000489: # NOUN REGISTER SCALE TYPE
000555,000490:
000556,000491: # 00 NOT IN USE
000557,000492: # 01 SPECIFY ADDRESS B
000558,000493: # 02 SPECIFY ADDRESS C
000559,000494: # 03 SPECIFY ADDRESS D
000560,000495: # 04 DSPTEM1 H
000561,000496: # 05 DSPTEM1 H
000562,000497: # 06 OPTION1 A
000563,000498: # 07 XREG A
000564,000499: # 08 ALMCADR A
000565,000500: # 09 FAILREG A
000566,000501: # 10 SPECIFY CHANNEL A
000567,000502: # 11 TCSI K
000568,000503: # 12 OPTIONX A
000569,000504: # 13 TCDH K
000570,000505: # 14 DSPTEMX C
000571,000506: # 15 INCREMENT ADDRESS A
000572,000507: # 16 DSPTEMX K
000573,000508: # 17 SPARE
000574,000509: # 18 FDAIX D
000575,000510: # 19 SPARE
000576,000511: # 20 CDUX D
000577,000512: # 21 PIPAX C
000578,000513: # 22 THETAD D
000579,000514: # 23 SPARE
000580,000515: # 24 DSPTEM2 +1 K
000581,000516: # 25 DSPTEM1 C
000582,000517: # 26 DSPTEM1 A
000583,000518: # 27 SMODE C
000584,000519: # 28 SPARE
000585,000520: # 29 SPARE
000586,000521: # 30 SPARE
000587,000522: # 31 SPARE
000588,000523: # 32 -TPER K
000589,000524: # 33 TIG K
000590,000525: # 34 DSPTEM1 K
000591,000526: # 35 TTOGO K
000592,000527: # 36 TIME2 K
000593,000528: # 37 TTPI K
000594,000529: # 38 TET K
000595,000530: # 39 SPARE
000596,000531:
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|
Page 14 |
000598,000533: # REGISTERS AND SCALING FOR MIXED NOUNS
000599,000534:
000600,000535: # NOUN COMP REGISTER SCALE TYPE
000601,000536:
000602,000537: # 40 1 TTOGO L
000603,000538: # 2 VGDISP S
000604,000539: # 3 DVTOTAL S
000605,000540: # 41 1 DSPTEM1 D
000606,000541: # 2 DSPTEM1 +1 E
000607,000542: # 42 1 HAPO Q
000608,000543: # 2 HPER Q
000609,000544: # 3 VGDISP S
000610,000545: # 43 1 LAT H
000611,000546: # 2 LONG H
000612,000547: # 3 ALT Q
000613,000548: # 44 1 HAPOX Q
000614,000549: # 2 HPERX Q
000615,000550: # 3 TFF L
000616,000551: # 45 1 TRKMKCNT C
000617,000552: # 2 TTOGO L
000618,000553: # 3 +MGA H
000619,000554: # 46 1 DAPDATR1 A
000620,000555: # 47 1 LEMMASS KK
000621,000556: # 2 CSMMASS KK
000622,000557: # 48 1 PITTIME NN
000623,000558: # 2 ROLLTIME NN
000624,000559: # 49 1 R22DISP Q
000625,000560: # 2 R22DISP +2 S
000626,000561: # 3 WHCHREAD C
000627,000562: # 50 SPARE
000628,000563: # 51 1 ALPHASB H
000629,000564: # 2 BETASB H
000630,000565: # 52 1 ACTCENT H
000631,000566: # 53 SPARE
000632,000567: # 54 1 RANGE JJ
000633,000568: # 2 RRATE S
000634,000569: # 3 RTHETA H
000635,000570: # 55 1 NN C
000636,000571: # 2 ELEV H
000637,000572: # 3 CENTANG H
000638,000573: # 56 1 RR-AZ H
000639,000574: # 2 RR-ELEV H
000640,000575: # 57 SPARE
000641,000576: # 58 1 POSTTPI Q
000642,000577: # 2 DELVTPI S
000643,000578: # 3 DELVTPF S
000644,000579: # 59 1 DVLOS S
000645,000580: # 2 DVLOS +2 S
000646,000581: # 3 DVLOS +4 S
000647,000582: # 60 1 FORVEL ZZ
|
|
Page 15 |
000649,000584: # 2 HDOTDISP S
000650,000585: # 3 ALTITUDE BBB
000651,000586: # 61 1 TTFDISP L
000652,000587: # 2 TTOGO L
000653,000588: # 3 OUTOFPLN QQ
000654,000589: # 62 1 ABVEL S
000655,000590: # 2 TTOGO L
000656,000591: # 3 DVTOTAL S
000657,000592: # 63 1 ABVEL S
000658,000593: # 2 HDOTDISP S
000659,000594: # 3 HCALC1 RR
000660,000595: # 64 1 FUNNYDSP PP
000661,000596: # 2 HDOTDISP S
000662,000597: # 3 HCALC RR
000663,000598: # 65 1 SAMPTIME K
000664,000599: # 2 SAMPTIME K
000665,000600: # 3 SAMPTIME K
000666,000601: # 66 1 RSTACK +6 W
000667,000602: # 2 CHANNEL 33 TT
000668,000603: # 67 1 RSTACK X
000669,000604: # 2 RSTACK +2 Y
000670,000605: # 3 RSTACK +4 Z
000671,000606: # 68 1 RANGEDSP QQ
000672,000607: # 2 TTFDISP L
000673,000608: # 3 DELTAH RR
000674,000609: # 69 1 DLANDZ RR
000675,000610: # 2 DLANDY RR
000676,000611: # 3 DLANDX RR
000677,000612: # 70 1 AOTCODE A
000678,000613: # 2 AOTCODE +1 A
000679,000614: # 3 AOTCODE +2 A
000680,000615: # 71 1 AOTCODE A
000681,000616: # 2 AOTCODE +1 A
000682,000617: # 3 AOTCODE +2 A
000683,000618: # 72 1 CDUT WW
000684,000619: # 2 CDUS D
000685,000620: # 73 1 TANG WW
000686,000621: # 2 TANG +1 D
000687,000622: # 74 1 TTOGO L
000688,000623: # 2 YAW H
000689,000624: # 3 PITCH H
000690,000625: # 75 1 DIFFALT Q
000691,000626: # 2 T1TOT2 L
000692,000627: # 3 T2TOT3 L
000693,000628: # 76 1 ZDOTD S
000694,000629: # 2 RDOTD S
000695,000630: # 3 XRANGE Q
000696,000631: # 77 1 TTOGO L
000697,000632: # 2 YDOT S
000698,000633: # 78 1 DNRRANGE U
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|
Page 16 |
000700,000635: # 2 DNRRDOT V
000701,000636: # 3 TTOTIG L
000702,000637: # 79 1 CURSOR D
000703,000638: # 2 SPIRAL D
000704,000639: # 3 POSCODE C
000705,000640: # 80 1 DATAGOOD C
000706,000641: # 2 OMEGAD H
000707,000642: # 81 1 DELVLVC S
000708,000643: # 2 DELVLVC +2 S
000709,000644: # 3 DELVLVC +4 S
000710,000645: # 82 1 DELVLVC S
000711,000646: # 2 DELVLVC +2 S
000712,000647: # 3 DELVLVC +4 S
000713,000648: # 83 1 DELVIMU S
000714,000649: # 2 DELVIMU +2 S
000715,000650: # 3 DELVIMU +4 S
000716,000651: # 84 1 DELVOV S
000717,000652: # 2 DELVOV +2 S
000718,000653: # 3 DELVOV +4 S
000719,000654: # 85 1 VGBODY S
000720,000655: # 2 VGBODY +2 S
000721,000656: # 3 VGBODY +4 S
000722,000657: # 86 1 DELVLVC S
000723,000658: # 2 DELVLVC +2 S
000724,000659: # 3 DELVLVC +4 S
000725,000660: # 87 1 AZ D
000726,000661: # 2 EL D
000727,000662: # 88 1 STARAD B
000728,000663: # 2 STARAD +2 B
000729,000664: # 3 STARAD +4 B
000730,000665: # 89 1 LANDLAT G
000731,000666: # 2 LANDLONG G
000732,000667: # 3 LANDALT JJ
000733,000668: # 90 1 RANGE JJ
000734,000669: # 2 RRATE S
000735,000670: # 3 RTHETA H
000736,000671: # 91 1 P21ALT Q (MEMORY/100 TO DIPLAY TENS N.M.)
000737,000672: # 2 P21VEL P
000738,000673: # 3 P21GAM H
000739,000674: # 92 1 THRDISP C
000740,000675: # 2 HDOTDISP S
000741,000676: # 3 HCALC1 RR
000742,000677: # 93 1 OGC G
000743,000678: # 2 OGC +2 G
000744,000679: # 3 OGC +4 G
000745,000680: # 94 SPARE
000746,000681: # 95 SPARE
000747,000682: # 96 SPARE
000748,000683: # 97 1 DSPTEM1 C
000749,000684: # 2 DSPTEM1 +1 C
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|
Page 17 |
000751,000686: # 3 DSPTEM1 +2 C
000752,000687: # 98 1 DSPTEM2 C
000753,000688: # 2 DSPTEM2 +1 B
000754,000689: # 3 DSPTEM2 +2 C
000755,000690: # 99 1 WWPOS XX
000756,000691: # 2 WWVEL YY
000757,000692: # 3 WWBIAS AAA
000758,000693:
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|
Page 18 |
000760,000695: # NOUN SCALES AND FORMATS
000761,000696:
000762,000697: # -SCALE TYPE- PRECISION
000763,000698: # UNITS DECIMAL FORMAT -- AGC FORMAT
000764,000699: # ------------ -------------- -- ----------
000765,000700:
000766,000701: # -A-
000767,000702: # OCTAL XXXXX SP OCTAL
000768,000703:
000769,000704: # -B- -14
000770,000705: # FRACTIONAL .XXXXX SP BIT 1 = 2 UNITS
000771,000706: # (MAX .99996)
000772,000707:
000773,000708: # -C-
000774,000709: # WHOLE XXXXX. SP BIT 1 = 1 UNIT
000775,000710: # (MAX 16383.)
000776,000711:
000777,000712: # -D- 15
000778,000713: # CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360/2 DEGREES
000779,000714: # (MAX 359.99) (USES 15 BITS FOR MAGNI-
000780,000715: # TUDE AND 2-S COMP.)
000781,000716:
000782,000717: # -E- 14
000783,000718: # ELEVATION DEGREES XX.XXX DEGREES SP BIT 1 = 90/2 DEGREES
000784,000719: # (MAX 89.999)
000785,000720:
000786,000721: # -F- 14
000787,000722: # DEGREES (180) XXX.XX DEGREES SP BIT 1 = 180/2 DEGREES
000788,000723: # (MAX 179.99)
000789,000724:
000790,000725: # -G-
000791,000726: # DP DEGREES(90) XX.XXX DEGREES DP BIT 1 OF LOW REGISTER =
000792,000727: # 28
000793,000728: # 360/2 DEGREES
000794,000729:
000795,000730: # -H-
000796,000731: # DP DEGREES (360) XXX.XX DEGREES DP BIT 1 OF LOW REGISTER =
000797,000732: # 28
000798,000733: # (MAX 359.99) 360/2 DEGREES
000799,000734:
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|
Page 19 |
000801,000736: # -K-
000802,000737: # TIME (HR, MIN, SEC) 00XXX. HR DP BIT 1 OF LOW REGISTER =
000803,000738: # 000XX. MIN -2
000804,000739: # 0XX.XX SEC 10 SEC
000805,000740: # (DECIMAL ONLY.
000806,000741: # MAX MIN COMP=59
000807,000742: # MAX SEC COMP=59.99
000808,000743: # MAX CAPACITY=745 HRS
000809,000744: # 39 MINS
000810,000745: # 14.55 SECS.
000811,000746: # WHEN LOADING, ALL 3
000812,000747: # COMPONENTS MUST BE
000813,000748: # SUPPLIED.)
000814,000749:
000815,000750: # -L-
000816,000751: # TIME (MIN/SEC) XXBXX MIN/SEC DP BIT 1 OF LOW REGISTER =
000817,000752: # (B IS A BLANK -2
000818,000753: # POSITION, DECIMAL 10 SEC
000819,000754: # ONLY, DISPLAY OR
000820,000755: # MONITOR ONLY. CANNOT
000821,000756: # BE LOADED.
000822,000757: # MAX MIN COMP=59
000823,000758: # MAX SEC COMP=59
000824,000759: # VALUES GREATER THAN
000825,000760: # 59 MIN 59 SEC
000826,000761: # ARE DISPLAYED AS
000827,000762: # 59 MIN 59 SEC.)
000828,000763:
000829,000764: # -M- -2
000830,000765: # TIME (SEC) XXX.XX SEC SP BIT 1 = 10 SEC
000831,000766: # (MAX 163.83)
000832,000767:
000833,000768: # -N-
000834,000769: # TIME(SEC) DP XXX.XX SEC DP BIT 1 OF LOW REGISTER =
000835,000770: # -2
000836,000771: # 10 SEC
000837,000772:
000838,000773: # -P-
000839,000774: # VELOCITY 2 XXXXX. FEET/SEC DP BIT 1 OF HIGH REGISTER =
000840,000775: # (MAX 41994.) -7
000841,000776: # 2 METERS/CENTI-SEC
000842,000777:
000843,000778: # -Q-
000844,000779: # POSITION 4 XXXX.X NAUTICAL MILES DP BIT 1 OF LOW REGISTER =
000845,000780: # 2 METERS
000846,000781:
000847,000782: # -S-
000848,000783: # VELOCITY 3 XXXX.X FT/SEC DP BIT 1 OF HIGH REGISTER =
000849,000784: # -7
000850,000785: # 2 METERS/CENTI-SEC
000851,000786:
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|
Page 20 |
000853,000788: # -T- -2
000854,000789: # G XXX.XX G SP BIT 1 = 10 G
000855,000790: # (MAX 163.83)
000856,000791:
000857,000792: # -U-
000858,000793: # RENDEZVOUS XXX.XX NAUT MI SP USES 15 BITS FOR UNSIGNED
000859,000794: # RADAR RANGE (DECIMAL ONLY. MAGNITUDE.
000860,000795: # DISPLAY OR MONITOR BIT 1 = 9.38 FEET
000861,000796: # ONLY. CANNOT BE
000862,000797: # LOADED.)
000863,000798:
000864,000799: # -V-
000865,000800: # RENDEZVOUS XXXX.X FEET/SEC SP USES 15 BITS FOR UNSIGNED
000866,000801: # RADAR RANGE RATE (DECIMAL ONLY. MAGNITUDE.
000867,000802: # DISPLAY OR MONITOR BIT 1 = -.6278 FEET/SEC
000868,000803: # ONLY. CANNOT BE
000869,000804: # LOADED.
000870,000805: # BIAS OF 17000 COUNTS
000871,000806: # SUBTRACTED BEFORE
000872,000807: # DISPLAY.)
000873,000808:
000874,000809: # -W-
000875,000810: # LANDING RADAR XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000876,000811: # ALTITUDE WORD = 1.079 FEET
000877,000812:
000878,000813: # -X-
000879,000814: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000880,000815: # VELX WORD = -.6440 FEET/SEC
000881,000816:
000882,000817: # -Y-
000883,000818: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000884,000819: # VELY WORD = 1.212 FEET/SEC
000885,000820:
000886,000821: # -Z-
000887,000822: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000888,000823: # VELZ WORD = .8668 FEET/SEC
000889,000824:
000890,000825: # -AA-
000891,000826: # INITIAL/FINAL XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000892,000827: # ALTITUDE WORD = 2.345 FEET
000893,000828:
000894,000829: # -BB-
000895,000830: # ALTITUDE RATE XXXXX. FEET/SEC SP LOW ORDER BIT = .5
000896,000831: # (MAX 08191.) FEET/SEC
000897,000832:
000898,000833: # -CC-
000899,000834: # FORWARD/LATERAL XXXX.X FEET/SEC SP LOW ORDER BIT = .5571
000900,000835: # VELOCITY (MAX 09126.) FEET/SEC
000901,000836:
000902,000837: # -DD-
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|
Page 21 |
000904,000839: # ROTATIONAL HAND XXXXX. DEG/SEC SP FRACTIONAL PART OF PI RAD
000905,000840: # CONTROLLER ANGULAR (MAX 00044.) 4 SEC
000906,000841: # RATES
000907,000842:
000908,000843: # -EE-
000909,000844: # OPTICAL TRACKER XXX.XX DEG. DP LOW ORDER BIT OF LOW ORDER
000910,000845: # AZIMUTH ANGLE 15
000911,000846: # WORD = 360/2 DEGREES
000912,000847:
000913,000848: # -JJ-
000914,000849: # POSITION5 XXX.XX NAUT MI DP BIT 1 OF LOW REGISTER =
000915,000850: # 2 METERS
000916,000851:
000917,000852: # -KK- 16
000918,000853: # WEIGHT2 XXXXX. LBS SP FRACTIONAL PART OF 2 KG
000919,000854:
000920,000855: # -NN-
000921,000856: # TRIM DEGREES 2 XXX.XX DEG SP BIT 1=.01SEC(TIME)
000922,000857: # (MAX 032.76)
000923,000858:
000924,000859: # -PP-
000925,000860: # 2 INTEGERS +XXBYY DP BIT 1 OF HIGH REGISTER =
000926,000861: # (B IS A BLANK 1 UNIT OF XX
000927,000862: # POSITION. DECIMAL BIT 1 OF LOW REGISTER =
000928,000863: # ONLY, DISPLAY OR 1 UNIT OF YY
000929,000864: # MONITOR ONLY. CANNOT (EACH REGISTER MUST
000930,000865: # BE LOADED.) CONTAIN A POSITIVE INTEGER
000931,000866: # (MAX 99B99) LESS THAN 100)
000932,000867:
000933,000868: # -QQ-
000934,000869: # POSITION7 XXXX.X NAUT MI DP BIT 1 OF LOW REGISTER =
000935,000870: # (MAX 9058.9) -4
000936,000871: # 2 METERS
000937,000872:
000938,000873: # -RR-
000939,000874: # COMPUTED ALTITUDE XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000940,000875: # -4
000941,000876: # 2 METERS
000942,000877:
000943,000878: # -SS-
000944,000879: # DP DEGREES XXXX.X DEGREES DP BIT 1 OF HIGH REGISTER =
000945,000880: # 1 DEGREE
000946,000881:
000947,000882: # -TT-
000948,000883: # LANDING RADAR +0000X CHANNEL 33,BIT 6=NOT POSIT. 1
000949,000884: # POSITION (DECIMAL ONLY. CHANNEL 33,BIT 7=NOT POSIT. 2
000950,000885: # DISPLAY OR MONITOR X = 1 FOR LR POSITION 1
000951,000886: # ONLY. CANNOT BE X = 2 FOR LR POSITION 2
000952,000887: # LOADED.)
000953,000888:
000954,000889: # -WW- 15
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|
Page 22 |
000956,000891: # 360-CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360 - (360/2 )
000957,000892: # (MAX 359.99) DEGREES
000958,000893: # (USES 15 BITS FOR MAGNI-
000959,000894: # TUDE AND 2-S COMP.)
000960,000895:
000961,000896: # -XX-
000962,000897: # POSITION 9 XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000963,000898: # -9
000964,000899: # 2 METERS
000965,000900:
000966,000901: # -YY-
000967,000902: # VELOCITY 4 XXXX.X FEET/SEC DP FRACTIONAL PART OF
000968,000903: # (MAX 328.0) METERS/CENTI-SEC
000969,000904:
000970,000905: # -ZZ-
000971,000906: # VELOCITY5 XXXX.X FT/SEC DP BIT 1 OF HIGH REGISTER =
000972,000907: # -9
000973,000908: # 2 METERS/CENTI-SEC
000974,000909:
000975,000910: # -AAA-
000976,000911: # RADIANS XX.XXX RADIANS DP BIT 1 OF HIGH REGISTER =
000977,000912: # (MAX 31.999) -9
000978,000913: # 2 RADIANS
000979,000914:
000980,000915: # -BBB-
000981,000916: # COMPUTED ALTITUDE 2 XXXXX. FEET DP BIT 1 OF HIGH REGISTER =
000982,000917: # 2 METERS
000983,000918:
000984,000919: # THAT-S ALL ON THE NOUNS.
000985,000920:
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000987,000922: # ALARM CODES FOR LUMINARY
000988,000923:
000989,000924: # *9 *18 *60 COLUMN
000990,000925:
000991,000926: # CODE * TYPE SET BY
000992,000927:
000993,000928: # 00107 MORE THAN 5 MARK PAIRS AOTMARK
000994,000929: # 00111 MARK MISSING AOTMARK
000995,000930: # 00112 MARK OR MARK REJECT NOT BEING ACCEPTED AOTMARK
000996,000931: # 00113 NO INBITS AOTMARK
000997,000932: # 00114 MARK MADE BUT NOT DESIRED AOTMARK
000998,000933: # 00115 NO MARKS IN LAST PAIR TO REJECT AOTMARK
000999,000934: # 00206 ZERO ENCODE NOT ALLOWED WITH COARSE ALIGN IMU MODE SWITCHING
001000,000935: # 00206 + GIMBAL LOCK.
001001,000936: # 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT
001002,000937: # 00210 IMU NOT OPERATING IMU MODE SWITCH, IMU-2, R02, P51, P57
001003,000938: # 00211 COARSE ALIGN ERROR IMU MODE SWITCH
001004,000939: # 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH,T4RPT
001005,000940: # 00213 IMU NOT OPERATING WITH TURN-ON REQUEST T4RUPT
001006,000941: # 00214 PROGRAM USING IMU WHEN TURNED OFF T4RUPT
001007,000942: # 00217 BAD RETURN FROM IMUSTALL P51,P52,P57
001008,000943: # 00220 IMU NOT ALIGNED - NO REFSMMAT R02,R47
001009,000944: # 00401 DESIRED GIMBAL ANGLE YIELDS GIMBAL LOCK INF ALIGN, IMU-2,
001010,000945: # FINDCDUW
001011,000946: # 00402 FINDCDUW NOT CONTROLLING ATTITUDE FINDCDUW
001012,000947: # 00404 TWO STARS NOT AVAILABLE IN ANY DETENT R59, LUNAR SURFACE
001013,000948: # 00405 TWO STARS NOT AVAILABLE P52
001014,000949: # 00421 W-MATRIX OVERFLOW INTEGRV
001015,000950: # 00501 P RADAR ANTENNA OUT OF LIMITS R23
001016,000951: # 00502 BAD RADAR GIMBAL ANGLE INPUT V41N72
001017,000952: # 00503 P RADAR ANTENNA DESIGNATE FAIL R21, NON-P IN V41N72
001018,000953: # 00510 RADAR AUTO DESCRETE NOT PRESENT R25
001019,000954: # 00511 LR ANTENNA MOVED AND NOT REPOSITIONED SERVICER
001020,000955: # 00514 P RR GOES OUT OF AUTO MODE WHILE IN USE P20
001021,000956: # 00515 RR CDU FAIL DISCRETE PRESENT R25
001022,000957: # 00520 RADAR RUPT NOT EXPECTED AT THIS TIME RADAR READ
001023,000958: # 00522 LANDING RADAR POSITION CHANGE R04
001024,000959: # 00523 LR ANTENNA DIDN'T ACHIEVE POSITION 2 V59 IN V60)
001025,000960: # 00525 P DELTA THETA GREATER THAN 3 DEGREES R22
001026,000961: # 00526 RANGE GREATER THAN 400 NAUTICAL MILES P20
001027,000962: # 00527 P LOS NOT IN MODE II COVERAGE WHILE ON R21,R24
001028,000963: # LUNAR SURFACE
001029,000964: # OR VEHICLE MANEUVER REQUIRED R24 (20)
001030,000965: # 00530 P LOS NOT IN MODE2 COVERAGE R21
001031,000966: # ON LUNAR SURFACE AFTER 600 SECS.
001032,000967: # 00555 SERVICER LOOP EXCEEDED 4 SECONDS SERVICER
001033,000968: # 00600 IMAGINARY ROOTS ON FIRST ITERATION P32, P72
001034,000969: # 00601 PERIGEE ALTITUDE CSI LT PMIN1 P32,P72,
001035,000970: # 00602 PERIGEE ALTITUDE CDH LT PMIN2 P32,P72,
001036,000971: # 00603 CSI TO CDH TIME LT TMIN12 P32,P72,P33,P73
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001038,000973: # 00604 CDH TO TPI TIME LT TMIN23 P32,P72,
001039,000974: # OR COMPUTED CDH TIME GREATER THAN INPUT TP1 TIME
001040,000975: # 00605 NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM P32, P72
001041,000976: # 00606 DV EXCEEDS MAXIMUM P32,P72,
001042,000977: # 00611 NO TIG FOR GIVEN ELEV ANGLE P34,P74
001043,000978: # 00701 ILLEGAL OPTION CODE SELECTED P57
001044,000979: # 00777 PIPA FAIL CAUSED THE ISS WARNING T4RUPT
001045,000980: # 01102 AGC SELF TEST ERROR SELF CHECK
001046,000981: # 01105 DOWNLINK TOO FAST T4RUPT
001047,000982: # 01106 UPLINK TOO FAST T4RUPT
001048,000983: # 01107 PHASE TABLE FAILURE. ASSUME RESTART
001049,000984: # ERASABLE MEMORY IS SUSPECT. RESTART
001050,000985: # 01301 ARCSIN-ARCCOS ARGUMENT TOO LARGE INTERPRETER
001051,000986: # 01406 BAD RETURN FROM ROOTPSRS DESCENT GUIDANCE EQS.
001052,000987: # 01407 VG INCREASING (DELTA-V ACCUMULATED S40.8
001053,000988: # .GT. 90 DEGREES AWAY FROM DESIRED THRUST S40.8
001054,000989: # VECTOR.) S40.8
001055,000990: # 01410 UNINTENTIONAL OVERFLOW IN GUIDANCE DESCENT GUIDANCE EQS.
001056,000991: # 01412 DESCENT IGNALG NOT CONVERGING P63
001057,000992: # 01520 V37 REQUEST NOT PERMITTED AT THIS TIME V37
001058,000993: # 01600 OVERFLOW IN DRIFT TEST IMU 4
001059,000994: # 01601 BAD IMU TORQUE OPT PRE ALIGN CALIB
001060,000995: # 01601 IMU 4 (LEM)
001061,000996: # 01703 IGNITION TIME SLIPPED MIDTOAVE
001062,000997: # 01706 INCORRECT PROGRAM REQUESTED FOR VEHICLE
001063,000998: # CONFIGURATION P40, P42
001064,000999: # 02001 JET FAILURES HAVE DISABLED Y-Z TRANS. DAP
001065,001000: # 02002 JET FAILURES HAVE DISABLED X TRANSLATION DAP
001066,001001: # 02003 JET FAILURES HAVE DISABLED P-ROTATION DAP
001067,001002: # 02004 JET FAILURES HAVE DISABLED U-V ROTATION DAP
001068,001003: # 03777 ICDU FAIL CAUSED THE ISS WARNING T4RUPT
001069,001004: # 04777 ICDU , PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001070,001005: # 07777 IMU FAIL CAUSED THE ISS WARNING T4RUPT
001071,001006: # 10777 IMU , PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001072,001007: # 13777 IMU , ICDU FAILS CAUSED THE ISS WARNING T4RUPT
001073,001008: # 14777 IMU,ICDU,PIPA FAILS CAUSED ISS WARNING T4RUPT
001074,001009:
001075,001010: # THE FOLLOWING CODES INDICATE THE MORE SERIOUS POODOO ABORTS THAT RESULT
001076,001011: # IN THE PROGRAM GOING TO ROO.
001077,001012:
001078,001013: # 20105 AOTMARK SYSTEM IN USE AOTMARK
001079,001014: # 20430 ACCELERATION OVERFLOW IN INTEGRATION ORBITAL INTEGRATION
001080,001015: # 20607 NO SOLN FROM TIME-THETA OR TIME-RADIUS TIMETHET, TIMERAD
001081,001016: # 21103 UNUSED CCS BRANCH EXECUTED ABORT
001082,001017: # 21204 WAITLIST, VARDELAY, FIXDELAY, OR LONGCALL WAITLIST ROUTINES
001083,001018: # CALLED WITH ZERO OR NEGATIVE DELTA-TIME
001084,001019: # 21302 SQRT CALLED WITH NEGATIVE ARGUMENT INTERPRETER
001085,001020: # 21406 BAD RETURN FROM ROOTPSRS IGNITION ALGORITHMN
001086,001021: # 21501 KEYBOARD AND DISPLAY ALARM DURING PINBALL
001087,001022: # INTERNAL USE(NVSUB).ABORT
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001089,001024: # THE FOLLOWING CODES INDICATE A BAILOUT ABORT THAT RESULTS IN A SOFTWARE
001090,001025: # RESTART
001091,001026: # 31104 DELAY ROUTINE BUSY EXEC
001092,001027: # 31201 EXECUTIVE OVERFLOW-NO VAC AREAS EXEC
001093,001028: # 31202 EXECUTIVE OVERFLOW-NO CORE SETS EXEC
001094,001029: # 31203 WAITLIST OVERFLOW-TOO MANY TASKS WAITLIST
001095,001030: # 31206 SECOND JOB ATTEMPTS TO GO TO SLEEP VIA PINBALL
001096,001031: # KEYBOARD AND DISPLAY PROGRAM
001097,001032: # 31207 NO VAC AREAS FOR MARKS AOTMARK
001098,001033: # 31210 TWO PROGRAMS USING DEVICE AT SAME TIME MODE SWITCHING
001099,001034: # 31211 ILLEGAL INTERRUPT OF EXTENDED VERB AOTMARK
001100,001035: # 31502 TWO PRIO DISPLAYS WAITING DSP INTRFCE
001101,001036: # 32000 DAP STILL IN PROGRESS AT NEXT TIME5 RUPT DAP
001102,001037:
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001104,001039: # CHECKLIST CODES FOR LUMINARY
001105,001040:
001106,001041: # *9 *17 *26 *9 COLUMN
001107,001042:
001108,001043: # R1CODE ACTION TO BE EFFECTED PROGRAM
001109,001044:
001110,001045: # 00013 KEY IN NORMAL OR GYRO TORQUE COARSE ALIGN P52
001111,001046: # 00014 PROCEED DO IMU FINE ALIGN ROUTINE P51,P63,P57
001112,001047: # 00014 ENTER DO LANDING SITE DETERMINATION(N89DISP) P57OPTION2
001113,001048: # 00015 PERFORM CELESTIAL BODY ACQUISITION R51,P51
001114,001049: # 00062 SWITCH AGC POWER DOWN P06
001115,001050: # 00201 SWITCH RR MODE TO AUTOMATIC P20,P22,R04
001116,001051: # 00203 SWITCH GUID CONTROL TO GNC, MODE TO AUTO... P12,P42,P71
001117,001052: # ALSO THR CONT TO AUTO P40,P63,P70
001118,001053: # 00205 PERFORM MANUAL ACQUISITION OF RR R23
001119,001054: # 00500 SWITCH LR ANTENNA TO POSITION 1 P63
001120,001055:
001121,001056: # SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
001122,001057: # PERFORM DENOTES START OR END OF A TASK
001123,001058: # KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
001124,001059:
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001126,001061: # OPTION CODES FOR LUMINARY
001127,001062:
001128,001063: # THE SPECIFIED OPTION CODES WILL BE FLASHED IN COMPONENT R1 IN
001129,001064: # CONJUNCTION WITH V04N06 OR V04N12 (FOR EXTENDED VERBS) TO REQUEST THE
001130,001065: # ASTRONAUT TO LOAD INTO COMPONENT R2 THE OPTION HE DESIRES.
001131,001066:
001132,001067: # *9 *17 *52 *11 *25 COLUMN
001133,001068:
001134,001069: # OPTION
001135,001070: # CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
001136,001071:
001137,001072: # 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P52 ALL
001138,001073: # 4=LAND SITE
001139,001074: # 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
001140,001075: # 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
001141,001076: # 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
001142,001077: # 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
001143,001078: # 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
001144,001079: # 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
001145,001080: # 2=TWO BODIES 3=ONE BODY + G
001146,001081: # 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
001147,001082: # ORBIT TO PASS OVER LM
End of include-file ASSEMBLY_AND_OPERATION_INFORMATION.agc. Parent file is MAIN.agc