Source Code
000069,000001: # Copyright: Public domain.
000070,000002: # Filename: ASSEMBLY_AND_OPERATION_INFORMATION.agc
000071,000003: # Purpose: Header information for Luminary 1C, revision 131.
000072,000004: # It is part of the source code for the Lunar Module's (LM)
000073,000005: # Apollo Guidance Computer (AGC) for Apollo 13 and Apollo 14.
000074,000006: # This file is intended to be a faithful transcription, except
000075,000007: # that the code format has been changed to conform to the
000076,000008: # requirements of the yaYUL assembler rather than the
000077,000009: # original YUL assembler.
000078,000010: # Reference: Pages 6-32 of 1729.pdf.
000079,000011: # Contact: Ron Burkey <info@sandroid.org>.
000080,000012: # Website: www.ibiblio.org/apollo/index.html
000081,000013: # Mod history: 04/12/03 RSB. Began transcribing.
000082,000014: # 04/23/03 RSB Finished draft.
000083,000015: # 12/06/03 RSB Did some proofing.
000084,000016: # 05/14/05 RSB Corrected website reference above.
000085,000017:
000086,000018: # The contents of this file, and all associated "Luminary131" files, are
000087,000019: # transcribed from a scanned document obtained from MIT's website,
000088,000020: # http://hrst.mit.edu/hrs/apollo/public/archive/1729.pdf. Notations on this
000089,000021: # document read, in part:
000090,000022:
000091,000023: # NASA Apollo LUMINARY 131 (1C) Program Source Code Listing.
000092,000024: # MIT Instrumentation/Draper Laboratory -- 19 December 1969, 1742 pages.
000093,000025: # This listing contains the flight program for the Lunar Module
000094,000026: # as created by MIT's Draper Lab for the Apollo 13/14 moon missions.
000095,000027:
000096,000028: # Refer directly to the online document mentioned above for further information.
000097,000029: # Please report any errors in this listing (relative to 1729.pdf) to info@sandroid.org.
000098,000030:
000099,000031: # Source code starts on Page 6 of the listing. Any pages with the notation "A" are proofed.
000100,000032: # However, proofing is hard, so even though a lot of errors were fixed in proofing, it should
000101,000033: # be assumed that lots of errors are still left. Also, I somehow got file corruption while proofing,
000102,000034: # so some of the changes I made in proofing got lost anyhow. :-(
000103,000035:
000104,000036: # Page 6, A
000105,000037:
000106,000038: # THIS LGC PROGRAM IS INTENDED FOR USE IN THE LM DURING THE MANNED LUNAR LANDING MISSION OR ANY SUBSET THEREOF.
000107,000039: # THE DETAILS OF IMPLEMENTATION ARE SPECIFIED IN REPORT R-567, AS AMENDED.
000108,000040:
000109,000041: # GUIDANCE SYSTEM OPERATIONS PLAN
000110,000042: # FOR MANNED LM EARTH ORBITAL AND LUNAR MISSIONS
000111,000043: # USING PROGRAM LUMINARY
000112,000044:
000113,000045: # THIS PROGRAM AND R-567 HAVE BEEN PREPARED BY THE INSTRUMENTATION LABORATORY, MASSACHUSETTS INSTITUTE OF
000114,000046: # TECHNOLOGY, 75 CAMBRIDGE PARKWAY, CAMBRIDGE, MASSACHUSETTS, UNDER PROJECT 55-238-70, SPONSORED BY THE MANNED
000115,000047: # SPACECRAFT CENTER OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, CONTRACT NAS 9-4065.
000116,000048:
000117,000049: # THIS PROGRAM IS REFERRED TO AS LUMINARY 1C
000118,000050:
000119,000051: # Page 7, A
000120,000052: # TABLE OF LOG CARDS
000121,000053: # ABSOLUTE ADDRESSES FOR UPDATE PROGRAM
000122,000054: # ASSEMBLY AND OPERATION INFORMATION
000123,000055: # TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
000124,000056: # CONTROLLED CONSTANTS
000125,000057: # INPUT/OUTPUT CHANNEL BIT DESCRIPTIONS
000126,000058: # FLAGWORD ASSIGNMENTS
000127,000059: # SUBROUTINE CALLS
000128,000060:
000129,000061: # TABLE OF SUBROUTINE LOG SECTIONS
000130,000062: # LUMERASE
000131,000063: # ERASABLE ASSIGNMENTS
000132,000064: # LEMONAID
000133,000065: # INTERRUPT LEAD INS
000134,000066: # T4RUPT PROGRAM
000135,000067: # RCS FAILURE MONITOR
000136,000068: # DOWNLINK LISTS
000137,000069: # AGS INITIALIZATION
000138,000070: # FRESH START AND RESTART
000139,000071: # RESTART TABLES
000140,000072: # AOTMARK
000141,000073: # EXTENDED VERBS
000142,000074: # PINBALL NOUN TABLES
000143,000075: # LEM GEOMETRY
000144,000076: # IMU COMPENSATION PACKAGE
000145,000077: # R63
000146,000078: # ATTITUDE MANEUVER ROUTINE
000147,000079: # GIMBAL LOCK AVOIDANCE
000148,000080: # KALCMANU STEERING
000149,000081: # SYSTEM TEST STANDARD LEAD INS
000150,000082: # IMU PERFORMANCE TESTS 2
000151,000083: # IMU PERFORMANCE TESTS 4
000152,000084: # PINBALL GAMES BUTTONS AND LIGHTS
000153,000085: # R60,R62
000154,000086: # S-BAND ANTENNA FOR LM
000155,000087: # LEMP20S
000156,000088: # RADAR LEADIN ROUTINES
000157,000089: # P20-P25
000158,000090: # LEMP30S
000159,000091: # P30,P37
000160,000092: # P32-P35, P72-P75
000161,000093: # KISSING
000162,000094: # GROUND TRACKING DETERMINATION PROGRAM -- P21
000163,000095: # P34-P35, P72-P75
000164,000096: # R31
000165,000097: # P76
000166,000098: # R30
000167,000099: # FLY
000168,000100: # Page 8, A
000169,000101: # BURN, BABY, BURN -- MASTER IGNITION ROUTINE
000170,000102: # P40-P47
000171,000103: # THE LUNAR LANDING
000172,000104: # THROTTLE CONTROL ROUTINES
000173,000105: # LUNAR LANDING GUIDANCE EQUATIONS
000174,000106: # P70-P71
000175,000107: # P12
000176,000108: # ASCENT GUIDANCE
000177,000109: # SERVICER
000178,000110: # LANDING ANALOG DISPLAYS
000179,000111: # FINDCDUW -- GUIDAP INTERFACE
000180,000112: # LEMP50S
000181,000113: # P51-P53
000182,000114: # LUNAR AND SOLAR EPHEMERIDES SUBROUTINES
000183,000115: # SKIPPER
000184,000116: # DOWN-TELEMETRY PROGRAM
000185,000117: # INTER-BANK COMMUNICATION
000186,000118: # INTEPRETER
000187,000119: # FIXED-FIXED CONSTANT POOL
000188,000120: # INTERPRETIVE CONSTANTS
000189,000121: # SINGLE PRECISION SUBROUTINES
000190,000122: # EXECUTIVE
000191,000123: # WAITLIST
000192,000124: # LATITUDE LONGITUDE SUBROUTINES
000193,000125: # PLANETARY INERTIAL ORIENTATION
000194,000126: # MEASUREMENT INCORPORATION
000195,000127: # CONIC SUBROUTINES
000196,000128: # INTEGRATION INITIALIZATION
000197,000129: # ORBITAL INTEGRATION
000198,000130: # INFLIGHT ALIGNMENT ROUTINES
000199,000131: # POWERED FLIGHT SUBROUTINES
000200,000132: # TIME OF FREE FALL
000201,000133: # AGC BLOCK TWO SELF-CHECK
000202,000134: # PHASE TABLE MAINTENANCE
000203,000135: # RESTARTS ROUTINE
000204,000136: # IMU MODE SWITCHING ROUTINES
000205,000137: # KEYRUPT, UPRUPT
000206,000138: # DISPLAY INTERFACE ROUTINES
000207,000139: # SERVICE ROUTINES
000208,000140: # ALARM AND ABORT
000209,000141: # UPDATE PROGRAM
000210,000142: # RT8 OP CODES
000211,000143: # LMDAP
000212,000144: # T6-RUPT PROGRAMS
000213,000145: # DAP INTERFACE SUBROUTINES
000214,000146: # CAPIDLER PROGRAM
000215,000147: # P-AXIS RCS AUTOPILOT
000216,000148: # Q,R-AXIS RCS AUTOPILOT
000217,000149: # TJET LAW
000218,000150: # KALMAN FILTER
000219,000151: # Page 9, A
000220,000152: # TRIM GIMBAL CNTROL SYSTEM
000221,000153: # AOSTASK AND ACSJOB
000222,000154: # SPS BACK-UP RCS CONTROL
000223,000155:
000224,000156: # Page 10, A
000225,000157: # VERB LIST FOR LUMINARY
000226,000158:
000227,000159: # REGULAR VERBS
000228,000160:
000229,000161: # 00 NOT IN USE
000230,000162: # 01 DISPLAY OCTAL COMP 1 IN R1
000231,000163: # 02 DISPLAY OCTAL COMP 2 IN R1
000232,000164: # 03 DISPLAY OCTAL COMP 3 IN R1
000233,000165: # 04 DISPLAY OCTAL COMP 1,2 IN R1,R2
000234,000166: # 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3
000235,000167: # 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000236,000168: # 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY)
000237,000169: # 08
000238,000170: # 09
000239,000171: # 10
000240,000172: # 11 MONITOR OCTAL COMP 1 IN R1
000241,000173: # 12 MONITOR OCTAL COMP 2 IN R1
000242,000174: # 13 MONITOR OCTAL COMP 3 IN R1
000243,000175: # 14 MONITOR OCTAL COMP 1,2 IN R1,R2
000244,000176: # 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3
000245,000177: # 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000246,000178: # 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY)
000247,000179: # 18
000248,000180: # 19
000249,000181: # 20
000250,000182: # 21 LOAD COMPONENT 1 INTO R1
000251,000183: # 22 LOAD COMPONENT 2 INTO R2
000252,000184: # 23 LOAD COMPONENT 3 INTO R3
000253,000185: # 24 LOAD COMPONENT 1,2, INTO R1,R2
000254,000186: # 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3
000255,000187: # 26
000256,000188: # 27 DISPLAY FIXED MEMORY
000257,000189: # 28
000258,000190: # 29
000259,000191: # 30 REQUEST EXECUTIVE
000260,000192: # 31 REQUEST WAITLIST
000261,000193: # 32 RECYCLE PROGRAM
000262,000194: # 33 PROCEED WITHOUT DSKY INPUTS
000263,000195: # 34 TERMINATE FUNCTION
000264,000196: # 35 TEST LIGHTS
000265,000197: # 36 REQUEST FRESH START
000266,000198: # 37 CHANGE PROGRAM (MAJOR MODE)
000267,000199: # 38
000268,000200: # 39
000269,000201:
000270,000202: # Page 11, A
000271,000203: # EXTENDED VERBS
000272,000204:
000273,000205: # 40 XERO CDU'S
000274,000206: # 41 COARSE ALIGN CDU'S
000275,000207: # 42 FINE ALIGN IMU
000276,000208: # 43 LOAD IMU ATT ERROR METERS
000277,000209: # 44 TERMINATE RR CONTINUOUS DESIGNATE (V41N72 OPTION 2)
000278,000210: # 45
000279,000211: # 46
000280,000212: # 47 INITIALIZE AGS (R47)
000281,000213: # 48 REQUEST DAP DATA LOAD ROUTINE (R03)
000282,000214: # 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
000283,000215: # 50 PLEASE PERFORM
000284,000216: # 51
000285,000217: # 52 MARK X-RETICLE
000286,000218: # 53 MARK Y-RETICLE
000287,000219: # 54 MARK X OR Y-RETICLE
000288,000220: # 55 INCREMENT AGC TIME (DECIMAL)
000289,000221: # 56 TERMINATE TRACKING (P20 + P25)
000290,000222: # 57 PERMIT LANDING RADAR UPDATES
000291,000223: # 58 INHIBIT LANDING RADAR UPDATES
000292,000224: # 59 COMMAND LR TO POSITON 2.
000293,000225: # 60 DISPLAY VEHICLE ATTITUDE RATES ON FDAI ERROR NEEDLES.
000294,000226: # 61 DISPLAY DAP FOLLOWING ATTITUDE ERRORS.
000295,000227: # 62 DISPLAY TOTAL ATTITUDE ERRORS WITH RESPECT TO NOUN 22.
000296,000228: # 63 SAMPLE RADAR ONCE PER SECOND (R04).
000297,000229: # 64 REQUEST S-BAND ANTENNA ROUTINE (R05).
000298,000230: # 65 DISABLE U AND V JET FIRINGS DURING DPS BURNS.
000299,000231: # 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
000300,000232: # 67 DISPLAY W MATRIX
000301,000233: # 68
000302,000234: # 69 CAUSE RESTART
000303,000235: # 70 UPDATE LIFTOFF TIME
000304,000236: # 71 UNIVERSAL UPDATE-BLOCK ADR
000305,000237: # 72 UNIVERSAL UPDATE-SINGLE ADR
000306,000238: # 73 UPDATE AGC TIME (OCTAL)
000307,000239: # 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK
000308,000240: # 75 ENABLE U AND V JET FIRINGS DURING DPS BURNS.
000309,000241: # 76 MINIMUM IMPUSE COMMAND MODE.
000310,000242: # 77 RATE COMMAND AND ATTITUDE HOLD MODE
000311,000243: # 78 LR SPURIOUS RETURN TEST START (R77)
000312,000244: # 79 LR SPURIOUS RETURN TEST STOP
000313,000245: # 80 UPDATE LEM STATE VECTOR
000314,000246: # 81 UPDATE CSM STATE FECTOR
000315,000247: # 82 REQUEST ORBIT PARAM DISPLAY (R30)
000316,000248: # 83 REQUEST REND PARAM DISPLAY (R31)
000317,000249: # 84
000318,000250: # 85 DISPLAY RR LOS AZ AND ELEV
000319,000251: # 86
000320,000252: # 87
000321,000253: # Page 12, A
000322,000254: # 88
000323,000255: # 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
000324,000256: # 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
000325,000257: # 91 DISPLAY BANK SUM
000326,000258: # 92 OPERATE IMU PERFORMANCE TEST (P07)
000327,000259: # 93 ENABLE W MATRIX INITALIZATION
000328,000260: # 94
000329,000261: # 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
000330,000262: # 96 INTERRUPT INTEGRATION AND GO TO P00
000331,000263: # 97 PERFORM ENGINE FAIL PROCEDURE
000332,000264: # 98
000333,000265: # 99 PLEASE ENABLE ENGINE
000334,000266:
000335,000267: # Page 13, A
000336,000268: # IN THE FOLLOWING NOUN LIST THE "NO LOAD" RESTRICTION MEANS THE NOUN
000337,000269: # CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
000338,000270: # SCALE TYPE L (MIN/SEC), PP (2 INTEGERS) OR TT (LANDING RADAR POSITION).
000339,000271: # IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22, OR 23
000340,000272: # MAY BE USED TO LOAD ANY OF THE NOUN'S COMPONENTS WHICH ARE NOT OF THE
000341,000273: # ABOVE SCALE TYPES.
000342,000274:
000343,000275: # THE "DEC ONLY" RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
000344,000276: # EVERY COMPONENT IN THE NOUN. (NOTE THAT "NO LOAD" IMPLIES "DEC ONLY".)
000345,000277:
000346,000278: # NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000347,000279: # 00 NOT IN USE
000348,000280: # 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .xxxxx FOR EACH
000349,000281: # 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP xxxxx. FOR EACH
000350,000282: # 03 SPECIFY MACHINE ADDRESS (DEGREES) 3COMP xxx.xx DEG FOR EACH
000351,000283: # 04 ANGULAR ERROR/DIFFERENCE 1COMP xxx.xx DEG
000352,000284: # 05 ANGULAR ERROR/DIFFERENCE 1COMP xxx.xx DEG
000353,000285: # 06 OPTION CODE 3COMP OCTAL ONLY
000354,000286: # LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER
000355,000287: # 07 ECADR OF WORD TO BE MODIFIED 3COMP OCTAL ONLY FOR EACH
000356,000288: # ONES FOR BITS TO BE MODIFIED
000357,000289: # 1 TO SET OR 0 TO RESET SELECTED BITS
000358,000290: # 08 ALARM DATA 3COMP OCTAL ONLY FOR EACH
000359,000291: # 09 ALARM CODES 3COMP OCTAL ONLY FOR EACH
000360,000292: # 10 CHANNEL TO BE SPECIFIED 1COMP OCTAL ONLY
000361,000293: # 11 TIG OF CSI 3COMP 00xxx. HRS DEC ONLY
000362,000294: # 000xx. MIN MUST LOAD 3 COMPS
000363,000295: # 0xx.xx SEC
000364,000296: # 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH
000365,000297: # (USED BY EXTENDED VERBS ONLY)
000366,000298: # 13 TIG OF CDH 3COMP 00xxx. HRS DEC ONLY
000367,000299: # 000xx. MIN MUST LOAD 3 COMPS
000368,000300: # 0xx.xx SEC
000369,000301: # 14 CHECKLIST 3COMP xxxxx. FOR EACH
000370,000302: # (USED BY EXTENDED VERBS ONLY)
000371,000303: # (NOUN 25 IS PASTED AFTER DISPLAY)
000372,000304: # 15 INCREMENT MACHINE ADDRESS 1COMP OCTAL ONLY
000373,000305: # 16 TIME OF EVENT 3COMP 00xxx. HRS DEC ONLY
000374,000306: # (USED BY EXTENDED VERBS ONLY) 000xx. MIN MUST LOAD 3 COMPS
000375,000307: # 0xx.xx SEC
000376,000308: # 17 SPARE
000377,000309: # 18 AUTO MANEUVER BALL ANGLES 3COMP xxx.xx DEG FOR EACH
000378,000310: # 19 SPARE
000379,000311: # 20 ICDU ANGLES 3COMP xxx.xx DEG FOR EACH
000380,000312: # 21 PIPAS 3COMP xxxxx. PULSES FOR EACH
000381,000313: # 22 NEW ICDU ANGLES 3COMP xxx.xx DEG FOR EACH
000382,000314: # 23 SPARE
000383,000315: # 24 DELTA TIME FOR AGC CLOCK 3COMP 00xxx. HRS DEC ONLY
000384,000316: # 000xx. MIN MUST LOAD 3 COMPS
000385,000317: # 0xx.xx SEC
000386,000318: # Page 14, A
000387,000319: # 25 CHECKLIST 3COMP xxxxx. FOR EACH
000388,000320: # (USED WITH PLEASE PERFORM ONLY)
000389,000321: # 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH
000390,000322: # 27 SELF TEST ON/OFF SWITCH 1COMP xxxxx.
000391,000323: # 28 SPARE
000392,000324: # 29 SPARE
000393,000325: # 30 SPARE
000394,000326: # 31 SPARE
000395,000327: # 32 TIME FROM PERIGEE 3COMP 00xxx. HRS DEC ONLY
000396,000328: # 000xx. MIN MUST LOAD 3 COMPS
000397,000329: # 0xx.xx SEC
000398,000330: # 33 TIME OF IGNITION 3COMP 00xxx. HRS DEC ONLY
000399,000331: # 000xx. MIN MUST LOAD 3 COMPS
000400,000332: # 0xx.xx SEC
000401,000333: # 34 TIME OF EVENT 3COMP 00xxx. HRS DEC ONLY
000402,000334: # 000xx. MIN MUST LOAD 3 COMPS
000403,000335: # 0xx.xx SEC
000404,000336: # 35 TIME FROM EVENT 3COMP 00xxx. HRS DEC ONLY
000405,000337: # 000xx. MIN MUST LOAD 3 COMPS
000406,000338: # 0xx.xx SEC
000407,000339: # 36 TIME OF AGC CLOCK 3COMP 00xxx. HRS DEC ONLY
000408,000340: # 000xx. MIN MUST LOAD 3 COMPS
000409,000341: # 0xx.xx SEC
000410,000342: # 37 TIG OF TPI 3COMP 00xxx. HRS DEC ONLY
000411,000343: # 000xx. MIN MUST LOAD 3 COMPS
000412,000344: # 0xx.xx SEC
000413,000345: # 38 TIME OF STATE BEING INTEGRATED 3COMP 00xxx. HRS DEC ONLY
000414,000346: # 000xx. MIN MUST LOAD 3 COMPS
000415,000347: # 0xx.xx SEC
000416,000348: # 39 SPARE
000417,000349:
000418,000350: # Page 15, A
000419,000351: # MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000420,000352: # 40 TIME FROM IGNITION/CUTOFF 3COMP xxBxx MIN/SEC NO LOAD, DEC ONLY
000421,000353: # VG, xxxx.x FT/SEC
000422,000354: # DELTA V (ACCUMULATED) xxxx.x FT.SEC
000423,000355: # 41 TARGET AXIMUTH 2COMP xxx.xx DEG (FOR SYSTEM TEST)
000424,000356: # ELEVATION xx.xxx DEG
000425,000357: # 42 APOGEE, 3COMP xxxx.x NAUT MI DEC ONLY
000426,000358: # PERIGEE, xxxx.x NAUT MI
000427,000359: # DELTA V (REQUIRED) xxxx.x FT/SEC
000428,000360: # 43 LATITUDE, 3COMP xxx.xx DEG DEC ONLY
000429,000361: # LONGITUDE, xxx.xx DEG
000430,000362: # ALTITUDE xxxx.x NAUT MI
000431,000363: # 44 APOGEE, 3COMP xxxx.x NAUT MI NO LOAD, DEC ONLY
000432,000364: # PERIGEE, xxxx.x NAUT MI
000433,000365: # TFF xxBxx MIN/SEC
000434,000366: # 45 MARKS, 3COMP xxxxx. NO LOAD, DEC ONLY
000435,000367: # TFI OF NEXT BURN, xxBxx MIN/SEC
000436,000368: # MGA xxx.xx DEG
000437,000369: # 46 AUTOPILOT CONFIGURATION 1COMP OCTAL ONLY
000438,000370: # 47 LEM WEIGHT, 2COMP xxxxx. LBS DEC ONLY
000439,000371: # CSM WEIGHT xxxxx. LBS
000440,000372: # 48 GIMBAL PITCH TRIM, 2COMP xxx.xx DEG DEC ONLY
000441,000373: # GIMBAL ROLL TRIM xxx.xx DEG
000442,000374: # 49 DELTA R, 3COMP xxxx.x NAUT MI DEC ONLY
000443,000375: # DELTA V, xxxx.x FT/SEC
000444,000376: # RADAR DATA SOURCE CODE xxxxx.
000445,000377: # 50 SPARE
000446,000378: # 51 S-BAND ANTENNA ANGLES PITCH 2COMP xxx.xx DEG DEC ONLY
000447,000379: # YAW xxx.xx DEG
000448,000380: # 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP xxx.xx DEG
000449,000381: # 53 SPARE
000450,000382: # 54 RANGE, 3COMP xxx.xx NAUT MI DEC ONLY
000451,000383: # RANGE RATE, xxxx.x FT/SEC
000452,000384: # THETA xxx.xx DEG
000453,000385: # 55 NO. OF APSIDAL CROSSINGS 3COMP xxxxx. DEC ONLY
000454,000386: # ELEVATION ANGLE xxx.xx DEG
000455,000387: # CENTRAL ANGLE OF PASSIVE VEHICLE xxx.xx DEG
000456,000388: # 56 RR LOS AZIMUTH 2COMP xxx.xx DEG
000457,000389: # ELEVATION xxx.xx DEG
000458,000390: # 57 SPARE
000459,000391: # 58 PERIGEE ALT (POST TPI) 3COMP xxxx.x NAUT MI DEC ONLY
000460,000392: # DELTA V TPI xxxx.x FT/SEC
000461,000393: # DELTA V TPF xxxx.x FT/SEC
000462,000394: # 59 DELTA VELOCITY LOS 3COMP xxxx.x FT/SEC FOR EA. DEC ONLY
000463,000395: # 60 FORWARD VELOCITY 3COMP xxxx.x FT/SEC DEC ONLY
000464,000396: # ALTITUDE RATE xxxx.x FT/SEC
000465,000397: # COMPUTED ALTITUDE xxxxx. FEET
000466,000398: # 61 TIME TO GO IN BRAKING PHASE 3COMP xxBxx MIN/SEC NO LOAD, DEC ONLY
000467,000399: # TIME FROM IGNITION xxBxx MIN/SEC
000468,000400: # Page 16, A
000469,000401: # CROSS RANGE DISTANCE xxxx.x NAUT MI
000470,000402: # 62 ABSOLUTE VALUE OF VELOCITY 3COMP xxxx.x FT/SEC NO LOAD, DEC ONLY
000471,000403: # TIME FROM IGNITION xxBxx MIN/SEC
000472,000404: # DELTA V (ACCUMULATED) xxxx.x FT/SEC
000473,000405: # 63 ABSOLUTE VALUE OF VELOCITY 3COMP xxxx.x FT/SEC DEC ONLY
000474,000406: # ALTITUDE RATE xxxx.x FT/SEC
000475,000407: # COMPUTED ALTITUDE xxxxx. FEET
000476,000408: # 64 TIME LEFT FOR REDESIGNATION--LPD ANGLE 3COMP xxBxx NO LOAD, DEC ONLY
000477,000409: # ALTITUDE RATE xxxx.x FT/SEC
000478,000410: # COMPUTED ALTITUDE xxxxx. FEET
000479,000411: # 65 SAMPLED AGC TIME 3COMP 00xxx. HRS. DEC ONLY
000480,000412: # (FETCHED IN INTERRUPT) 000xx. MIN MUST LOAD 3 COMPS
000481,000413: # 0xx.xx SEC
000482,000414: # 66 LR RANGE 2COMP xxxxx. FEET NO LOAD, DEC ONLY
000483,000415: # POSITION +0000x
000484,000416: # 67 LRVX 3COMP xxxxx. FT/SEC
000485,000417: # LRVY xxxxx. FT/SEC
000486,000418: # LRVZ xxxxx. FT/SEC
000487,000419: # 68 SLANT RANGE TO LANDING SITE 3COMP xxxx.x NAUT MI NO LOAD, DEC ONLY
000488,000420: # TIME TO GO IN BRAKING PHASE xxBxx MIN/SEC
000489,000421: # LR ALTITUDE -- COMPUTED ALTITUDE xxxxx. FEET
000490,000422: # 69 LANDING SITE CORRECTION, Z-COMPONENT 3COMP xxxxx. FEET DEC ONLY
000491,000423: # LANDING SITE CORRECTION, Y-COMPONENT xxxxx. FEET
000492,000424: # LANDING SITE CORRECTION, X-COMPONENT xxxxx. FEET
000493,000425: # 70 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000494,000426: # 71 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000495,000427: # 72 RR 360 -- TRUNNION ANGLE 2COMP xxx.xx DEG
000496,000428: # SHAFT ANGLE xxx.xx DEG
000497,000429: # 73 NEW RR 360 -- TRUNNION ANGLE 2COMP xxx.xx DEG
000498,000430: # SHAFT ANGLE xxx.xx DEG
000499,000431: # 74 TIME FROM IGNITION 3COMP xxBxx MIN/SEC NO LOAD, DEC ONLY
000500,000432: # YAW AFTER VEHICLE RISE xxx.xx DEG
000501,000433: # PITCH AFTER VEHICLE RISE xxx.xx DEG
000502,000434: # 75 DELTA ALTITUDE CDH 3COMP xxxx.x NAUT MI NO LOAD, DEC ONLY
000503,000435: # DELTA TIME (CDH-CSI OR TPI-CDH) xxBxx MIN/SEC
000504,000436: # DELTA TIME (TPI-CDH OR TPI-NONTPI) xxBxx MIN/SEC
000505,000437: # 76 DESIRED HORIZONTAL VELOCITY 3COMP xxxx.x FT/SEC DEC ONLY
000506,000438: # DESIRED RADIAL VELOCITY xxxx.x FT/SEC
000507,000439: # CROSS-RANGE DISTANCE xxxx.x NAUT MI
000508,000440: # 77 TIME TO ENGINE CUTOFF 2COMP xxBxx MIN/SEC NO LOAD, DEC ONLY
000509,000441: # VELOCITY NORMAL TO CSM PLANE xxxx.x FT/SEC
000510,000442: # 78 RR RANGE 3COMP xxx.xx NAUT MI NO LOAD, DEC ONLY
000511,000443: # RANGE RATE xxxx. FT/SEC
000512,000444: # TIME FROM IGNITION xxBxx MIN/SEC
000513,000445: # 79 CURSOR ANGLE 3COMP xxx.xx DEG DEC ONLY
000514,000446: # SPIRAL ANGLE xxx.xx DEG
000515,000447: # POSITION CODE xxxxx.
000516,000448: # 80 DATA INDICATOR, 2COMP xxxxx.
000517,000449: # OMEGA xxx.xx DEG
000518,000450: # 81 DELTA V (LV) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
000519,000451: # Page 17, A
000520,000452: # 82 DELTA V (LV) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
000521,000453: # 83 DELTA V (BODY) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
000522,000454: # 84 DELTA V (OTHER VEHICLE) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
000523,000455: # 85 VG (BODY) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
000524,000456: # 86 VG (LV) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
000525,000457: # 87 BACKUP OPTICS LOS AZIMUTH 2COMP xxx.xx DEG
000526,000458: # ELEVATION xxx.xx DEG
000527,000459: # 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .xxxxx FOR EACH DEC ONLY
000528,000460: # 89 LANDMARK LATITUDE 3COMP xx.xxx DEG DEC ONLY
000529,000461: # LONGITUDE/2 xx.xxx DEG
000530,000462: # ALTITUDE xxx.xx NAUT MI
000531,000463: # 90 y 3COMP xxx.xx NM DEC ONLY
000532,000464: # Y DOT xxxx.x FPS
000533,000465: # PSI xxx.xx DEG
000534,000466: # 91 ALTITUDE 3COMP xxxxxB. NAUT MI
000535,000467: # VELOCITY xxxxx. FT/SEC
000536,000468: # FLIGHT PATH ANGLE xxx.xx DEG
000537,000469: # 92 PCT FTP (10.5K LB) AT PRESENT THRUST 3COMP xxxxx.
000538,000470: # ALTITUDE RATE xxxx.x FT/SEC
000539,000471: # COMPUTED ALTITUDE xxxxx. FEET
000540,000472: # 93 DELTA GYRO ANGLES 3COMP xx.xxx DEG FOR EACH
000541,000473: # 94 SPARE
000542,000474: # 95 SPARE
000543,000475: # 96 SPARE
000544,000476: # 97 SYSTEM TEST INPUTS 3COMP xxxxx. FOR EACH
000545,000477: # 98 SYSTEM TEST RESULTS AND INPUTS 3COMP xxxxx.
000546,000478: # .xxxxx
000547,000479: # xxxxx.
000548,000480: # 99 RMS IN POSITION 3COMP xxxxx. FT DEC ONLY
000549,000481: # RMS IN VELOCITY xxxx.x FT/SEC
000550,000482: # RMS IN BIAS xx.xxx RADIANS
000551,000483:
000552,000484: # Page 18, A
000553,000485: # REGISTERS AND SCALING FOR NORMAL NOUNS
000554,000486:
000555,000487: # NOUN REGISTER SCALE TYPE
000556,000488: # 00 NOT IN USE
000557,000489: # 01 SPECIFY ADDRESS B
000558,000490: # 02 SPECIFY ADDRESS C
000559,000491: # 03 SPECIFY ADDRESS D
000560,000492: # 04 DSPTEM1 H
000561,000493: # 05 DSPTEM1 H
000562,000494: # 06 OPTION1 A
000563,000495: # 07 XREG A
000564,000496: # 08 ALMCADR A
000565,000497: # 09 FAILREG A
000566,000498: # 10 SPECIFY CHANNEL A
000567,000499: # 11 TCSI K
000568,000500: # 12 OPTIONX A
000569,000501: # 13 TCDH K
000570,000502: # 14 DSPTEMX C
000571,000503: # 15 INCREMENT ADDRESS A
000572,000504: # 16 DSPTEMX K
000573,000505: # 17 SPARE
000574,000506: # 18 FDAIX D
000575,000507: # 19 SPARE
000576,000508: # 20 CDUX D
000577,000509: # 21 PIPAX C
000578,000510: # 22 THETAD D
000579,000511: # 23 SPARE
000580,000512: # 24 DSPTEM2 +1 K
000581,000513: # 25 DSPTEM1 C
000582,000514: # 26 DSPTEM1 A
000583,000515: # 27 SMODE C
000584,000516: # 28 SPARE
000585,000517: # 29 SPARE
000586,000518: # 30 SPARE
000587,000519: # 31 SPARE
000588,000520: # 32 -TPER K
000589,000521: # 33 TIG K
000590,000522: # 34 DSPTEM1 K
000591,000523: # 35 TTOGO K
000592,000524: # 36 TIME2 K
000593,000525: # 37 TTPI K
000594,000526: # 38 TET K
000595,000527: # 39 SPARE
000596,000528:
000597,000529: # Page 19, A
000598,000530: # REGISTERS AND SCALING FOR MIXED NOUNS
000599,000531:
000600,000532: # NOUN COMP REGISTER SCALE TYPE
000601,000533: # 40 1 TTOGO L
000602,000534: # 2 VGDISP S
000603,000535: # 3 DVTOTAL S
000604,000536: # 41 1 DSPTEM1 D
000605,000537: # 2 DSPTEM1 +1 E
000606,000538: # 42 1 HAPO Q
000607,000539: # 2 HPER Q
000608,000540: # 3 VGDISP S
000609,000541: # 43 1 LAT H
000610,000542: # 2 LONG H
000611,000543: # 3 ALT Q
000612,000544: # 44 1 HAPOX Q
000613,000545: # 2 HPERX Q
000614,000546: # 3 TFF L
000615,000547: # 45 1 TRKMKCNT C
000616,000548: # 2 TTOGO L
000617,000549: # 3 +MGA H
000618,000550: # 46 1 DAPDATR1 A
000619,000551: # 47 1 LEMMASS KK
000620,000552: # 2 CSMMASS KK
000621,000553: # 48 1 PITTIME NN
000622,000554: # 2 ROLLTIME NN
000623,000555: # 49 1 R22DISP Q
000624,000556: # 2 R22DISP +2 S
000625,000557: # 3 WHCHREAD C
000626,000558: # 50 SPARE
000627,000559: # 51 1 ALPHASB H
000628,000560: # 2 BETASB H
000629,000561: # 52 1 ACTCENT H
000630,000562: # 53 SPARE
000631,000563: # 54 1 RANGE JJ
000632,000564: # 2 RRATE S
000633,000565: # 3 RTHETA H
000634,000566: # 55 1 NN C
000635,000567: # 2 ELEV H
000636,000568: # 3 CENTANG H
000637,000569: # 56 1 RR-AZ H
000638,000570: # 2 RR-ELEV H
000639,000571: # 57 SPARE
000640,000572: # 58 1 POSTTPI Q
000641,000573: # 2 DELVTPI S
000642,000574: # 3 DELVTPF S
000643,000575: # 59 1 DVLOS S
000644,000576: # 2 DVLOS +2 S
000645,000577: # 3 DVLOS +4 S
000646,000578: # 60 1 FORVEL CC
000647,000579: # Page 20, A
000648,000580: # 2 HDOTDISP S
000649,000581: # 3 HCALC1 RR
000650,000582: # 61 1 TTFDISP L
000651,000583: # 2 TTOGO L
000652,000584: # 3 OUTOFPLN QQ
000653,000585: # 62 1 ABVEL S
000654,000586: # 2 TTOGO L
000655,000587: # 3 DVTOTAL S
000656,000588: # 63 1 ABVEL S
000657,000589: # 2 HDOTDISP S
000658,000590: # 3 HCALC1 RR
000659,000591: # 64 1 FUNNYDSP PP
000660,000592: # 2 HDOTDISP S
000661,000593: # 3 HCALC RR
000662,000594: # 65 1 SAMPTIME K
000663,000595: # 2 SAMPTIME K
000664,000596: # 3 SAMPTIME K
000665,000597: # 66 1 RSTACK +6 W
000666,000598: # 2 CHANNEL 33 TT
000667,000599: # 67 1 RSTACK X
000668,000600: # 2 RSTACK +2 Y
000669,000601: # 3 RSTACK +4 Z
000670,000602: # 68 1 RANGEDSP QQ
000671,000603: # 2 TTFDISP L
000672,000604: # 3 DELTAH RR
000673,000605: # 69 1 DLANDZ RR
000674,000606: # 2 DLANDY RR
000675,000607: # 3 DLANDX RR
000676,000608: # 70 1 AOTCODE A
000677,000609: # 2 AOTCODE +1 A
000678,000610: # 3 AOTCODE +2 A
000679,000611: # 71 1 AOTCODE A
000680,000612: # 2 AOTCODE +1 A
000681,000613: # 3 AOTCODE +2 A
000682,000614: # 72 1 CDUT WW
000683,000615: # 2 CDUS D
000684,000616: # 73 1 TANG WW
000685,000617: # 2 TANG +1 D
000686,000618: # 74 1 TTOGO L
000687,000619: # 2 YAW H
000688,000620: # 3 PITCH H
000689,000621: # 75 1 DIFFALT Q
000690,000622: # 2 T1TOT2 L
000691,000623: # 3 T2TOT3 L
000692,000624: # 76 1 ZDOTD S
000693,000625: # 2 RDOTD S
000694,000626: # 3 XRANGE Q
000695,000627: # 77 1 TTOGO L
000696,000628: # 2 YDOT S
000697,000629: # 78 1 DNRRANGE U
000698,000630: # Page 21, A
000699,000631: # 2 DNRRDOT V
000700,000632: # 3 TTOTIG L
000701,000633: # 79 1 CURSOR D
000702,000634: # 2 SPIRAL D
000703,000635: # 3 POSCODE C
000704,000636: # 80 1 DATAGOOD C
000705,000637: # 2 OMEGAC H
000706,000638: # 81 1 DELVLVC S
000707,000639: # 2 DELVLVC +2 S
000708,000640: # 3 DELVLVC +4 S
000709,000641: # 82 1 DELVLVC S
000710,000642: # 2 DELVLVC +2 S
000711,000643: # 3 DELVLVC +4 S
000712,000644: # 83 1 DELVIMU S
000713,000645: # 2 DELVIMU +2 S
000714,000646: # 3 DELVIMU +4 S
000715,000647: # 84 1 DELVOV S
000716,000648: # 2 DELVOV +2 S
000717,000649: # 3 DELVOV +4 S
000718,000650: # 85 1 VGBODY S
000719,000651: # 2 VGBODY +2 S
000720,000652: # 3 VGBODY +4 S
000721,000653: # 86 1 DELVLVC S
000722,000654: # 2 DELVLVC +2 S
000723,000655: # 3 DELVLVC +4 S
000724,000656: # 87 1 AZ D
000725,000657: # 2 EL D
000726,000658: # 88 1 STARAD B
000727,000659: # 2 STARAD +2 B
000728,000660: # 3 STARAD +4 B
000729,000661: # 89 1 LANDLAT G
000730,000662: # 2 LANDLONG G
000731,000663: # 3 LANDALT JJ
000732,000664: # 90 1 RANGE JJ
000733,000665: # 2 RRATE S
000734,000666: # 3 RTHETA H
000735,000667: # 91 1 P21ALT Q (MEMORY/100 TO DISPLAY TENS N.M.)
000736,000668: # 2 P21VEL P
000737,000669: # 3 P21GAM H
000738,000670: # 92 1 THRDISP C
000739,000671: # 2 HDOTDISP S
000740,000672: # 3 HCALC1 RR
000741,000673: # 93 1 OGC G
000742,000674: # 2 OGC +2 G
000743,000675: # 3 OGC +4 G
000744,000676: # 94 SPARE
000745,000677: # 95 SPARE
000746,000678: # 96 SPARE
000747,000679: # 97 1 DSPTEM1 C
000748,000680: # 2 DSPTEM1 +1 C
000749,000681: # Page 22, A
000750,000682: # 3 DSPTEM1 +2 C
000751,000683: # 98 1 DSPTEM2 C
000752,000684: # 2 DSPTEM2 +1 B
000753,000685: # 3 DSPTEM2 +2 C
000754,000686: # 99 1 WWPOS XX
000755,000687: # 2 WWVEL YY
000756,000688: # 3 WWBIAS AAA
000757,000689: # Page 23
000758,000690: # NOUN SCALES AND FORMATS
000759,000691:
000760,000692: # -SCALE TYPE- PRECISION
000761,000693: # UNITS DECIMAL FORMAT -- AGC FORMAT
000762,000694: # ------------ -------------- -- ----------
000763,000695:
000764,000696: # -A-
000765,000697: # OCTAL xxxxx SP OCTAL
000766,000698:
000767,000699: # -B- -14
000768,000700: # FRACTIONAL .xxxxx SP BIT 1 = 2 UNITS
000769,000701: # (MAX .99996)
000770,000702:
000771,000703: # -C-
000772,000704: # WHOLE xxxxx. SP BIT 1 = 1 UNIT
000773,000705: # (MAX 16383.)
000774,000706:
000775,000707: # -D- 15
000776,000708: # CDU DEGREES xxx.xx DEGREES SP BIT 1 = 360/2 DEGREES
000777,000709: # (MAX 359.99) (USES 15 BITS FOR MAGNI-
000778,000710: # TUDE AND 2-S COMP.)
000779,000711:
000780,000712: # -E- 14
000781,000713: # ELEVATION DEGREES xx.xxx DEGREES SP BIT 1 = 90/2 DEGREES.
000782,000714: # (MAX 89.999)
000783,000715:
000784,000716: # -F- 14
000785,000717: # DEGREES (180) xxx.xx DEGREES SP BIT 1 = 180/2 DEGREES
000786,000718: # (MAX 179.99)
000787,000719:
000788,000720: # -G-
000789,000721: # DP DEGREES (90) xx.xxx DEGREES DP BIT 1 OF LOW REGISTER =
000790,000722: # 28
000791,000723: # 360/2 DEGREES
000792,000724:
000793,000725: # -H-
000794,000726: # DP DEGREES (360) xxx.xx DEGREES DP BIT 1 OF LOW REGISTER =
000795,000727: # 28
000796,000728: # (MAX 359.99) 360/2 DEGREES
000797,000729:
000798,000730: # Page 24
000799,000731: # -K-
000800,000732: # TIME (HR, MIN, SEC) 00xxx. HR DP BIT 1 OF LOW REGISTER =
000801,000733: # 000xx. MIN -2
000802,000734: # 0xx.xx SEC 10 SEC
000803,000735: # (DECIMAL ONLY.
000804,000736: # MAX MIN COMP=59
000805,000737: # MAX SEC COMP=59.99
000806,000738: # MAX CAPACITY=745 HRS
000807,000739: # 39 MINS
000808,000740: # 14.55 SECS.
000809,000741: # WHEN LOADING, ALL 3
000810,000742: # COMPONENTS MUST BE
000811,000743: # SUPPLIED.)
000812,000744:
000813,000745: # -L-
000814,000746: # TIME (MIN/SEC) xxBxx MIN/SEC DP BIT 1 OF LOW REGISTER =
000815,000747: # (B IS A BLANK -2
000816,000748: # POSITION, DECIMAL 10 SEC
000817,000749: # ONLY, DISPLAY OR
000818,000750: # MONITOR ONLY. CANNOT
000819,000751: # BE LOADED.
000820,000752: # MAX MIN COMP=59
000821,000753: # MAX SEC COMP=59
000822,000754: # VALUES GREATER THAN
000823,000755: # 59 MIN 59 SEC
000824,000756: # ARE DISPLAYED AS
000825,000757: # 59 MIN 59 SEC.)
000826,000758:
000827,000759: # -M- -2
000828,000760: # TIME (SEC) xxx.xx SEC SP BIT 1 = 10 SEC
000829,000761: # (MAX 163.83)
000830,000762:
000831,000763: # -N-
000832,000764: # TIME(SEC) DP xxx.xx SEC DP BIT 1 OF LOW REGISTER =
000833,000765: # -2
000834,000766: # 10 SEC.
000835,000767:
000836,000768: # -P-
000837,000769: # VELOCITY 2 xxxxx. FEET/SEC DP BIT 1 OF HIGH REGISTER =
000838,000770: # (MAX 41994.) -7
000839,000771: # 2 METERS/CENTI-SEC
000840,000772:
000841,000773: # -Q-
000842,000774: # POSITION 4 xxxx.x NAUTICAL MILES DP BIT 1 OF LOW REGISTER =
000843,000775: # 2 METERS
000844,000776:
000845,000777: # -S-
000846,000778: # VELOCITY 3 xxxx.x FT/SEC DP BIT 1 OF HIGH REGISTER =
000847,000779: # -7
000848,000780: # 2 METERS/CENTI-SEC
000849,000781:
000850,000782: # Page 25
000851,000783: # -T- -2
000852,000784: # G xxx.xx G SP BIT 1 = 10 G
000853,000785: # (MAX 163.83)
000854,000786:
000855,000787: # -U-
000856,000788: # RENDEZVOUS xxx.xx NAUT MI SP USES 15 BITS FR UNSIGNED
000857,000789: # RADAR RANGE (DECIMAL ONLY. MAGNITUDE.
000858,000790: # DISPLAY OR MONITOR BIT 1 = 9.38 FEET
000859,000791: # ONLY. CANNOT BE
000860,000792: # LOADED.)
000861,000793:
000862,000794: # -V-
000863,000795: # RENDEZVOUS xxxx. FEET/SEC SP USES 15 BITS FOR UNSIGNED
000864,000796: # RADAR RANGE RATE (DECIMAL ONLY. MAGNITUDE.
000865,000797: # DISPLAY OR MONITOR BIT 1 = -.6278 FEET/SEC
000866,000798: # ONLY. CANNOT BE
000867,000799: # LOADED.
000868,000800: # BIAS OF 17000 COUNTS
000869,000801: # SUBTRACTED BEFORE
000870,000802: # DISPLAY.)
000871,000803:
000872,000804: # -W-
000873,000805: # LANDING RADAR xxxxx. FEET DP LOW ORDER BIT OF LOW ORDER
000874,000806: # ALTITUDE WORD = 1.079 FEET
000875,000807:
000876,000808: # -X-
000877,000809: # LANDING RADAR xxxxx. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000878,000810: # VELX WORD = -.6440 FEET/SEC
000879,000811:
000880,000812: # -Y-
000881,000813: # LANDING RADAR xxxxx. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000882,000814: # VELY WORD = 1.212 FEET/SEC
000883,000815:
000884,000816: # -Z-
000885,000817: # LANDING RADAR xxxxx. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000886,000818: # VELZ WORD = .8668 FEET/SEC
000887,000819:
000888,000820: # -AA-
000889,000821: # INITIAL/FINAL xxxxx. FEET DP LOW ORDER BIT OF LOW ORDER
000890,000822: # ALTITUDE WORD = 2.345 FEET
000891,000823:
000892,000824: # -BB-
000893,000825: # ALTITUDE RATE xxxxx. FEET/SEC SP LOW ORDER BIT = .5
000894,000826: # (MAX 08191.) FEET/SEC
000895,000827:
000896,000828: # -CC-
000897,000829: # FORWARD/LATERAL xxxx.x FEET/SEC SP LOW ORDER BIT = .5571
000898,000830: # VELOCITY (MAX 09126.) FEET/SEC
000899,000831:
000900,000832: # -DD-
000901,000833: # Page 26
000902,000834: # ROTATIONAL HAND xxxxx. DEG/SEC SP FRACTIONAL PART OF PI RAD
000903,000835: # CONTROLLER ANGULAR (MAX 00044.) 4 SEC
000904,000836: # RATES
000905,000837:
000906,000838: # -EE-
000907,000839: # OPTICAL TRACKER xxx.xx DEG. DP LOW ORDER BIT OF LOW ORDER
000908,000840: # AZIMUTH ANGLE 15
000909,000841: # WORD = 360/2 DEGREES
000910,000842:
000911,000843: # -JJ-
000912,000844: # POSITION5 xxx.xx NAUT MI DP BIT 1 OF LOW REGISTER =
000913,000845: # 2 METERS
000914,000846:
000915,000847: # -KK- 16
000916,000848: # WEIGHT2 xxxxx. LBS SP FRACTIONAL PART OF 2 KG
000917,000849:
000918,000850: # -NN-
000919,000851: # TRIM DEGREES 2 xxx.xx DEG SP BIT 1=.01 SEC(TIME)
000920,000852: # (MAX 032.76) (garbled)
000921,000853:
000922,000854: # -PP-
000923,000855: # 2 INTEGERS +xxByy DP BIT 1 OF HIGH REGISTER =
000924,000856: # (B IS A BLANK 1 UNIT OF XX
000925,000857: # POSITION. DECIMAL BIT 1 OF LOW REGISTER =
000926,000858: # ONLY. DISPLAY OR 1 UNIT OF YY
000927,000859: # MONITOR ONLY. CANNOT (EACH REGISTER MUST
000928,000860: # BE LOADED.) CONTAIN A POSITIVE INTEGER
000929,000861: # (MAX 99B99) LESS THAN 100)
000930,000862:
000931,000863: # -QQ-
000932,000864: # POSITION7 xxxx.x NAUT MI DP BIT 1 OF LOW REGISTER =
000933,000865: # (MAX 9058.9) -4
000934,000866: # 2 METERS
000935,000867:
000936,000868: # -RR-
000937,000869: # COMPUTED ALTITUDE xxxxx. FEET DP BIT 1 OF LOW REGISTER =
000938,000870: # -4
000939,000871: # 2 METERS
000940,000872:
000941,000873: # -SS-
000942,000874: # DP DEGREES xxxx.x DEGREES DP BIT 1 OF HIGH REGISTER =
000943,000875: # 1 DEGREE
000944,000876:
000945,000877: # -TT-
000946,000878: # LANDING RADAR +0000x CHANNEL 33, BIT 6 = NOT POSIT. 1
000947,000879: # POSITION (DECIMAL ONLY. CHANNEL 33, BIT 7 = NOT POSIT. 2
000948,000880: # DISPLAY OR MONITOR X = 1 FOR LR POSITION 1
000949,000881: # ONLY. CANNOT BE X = 2 FOR LR POSITION 2
000950,000882: # LOADED.)
000951,000883:
000952,000884: # -WW-
000953,000885: # Page 27 15
000954,000886: # 360-CDU DEGREES xxx.xx DEGREES SP BIT 1 = 360 - (360/2 )
000955,000887: # (MAX 359.99) DEGREES
000956,000888: # (USES 15 BITS FOR MAGNI-
000957,000889: # TUDE AND 2-S COMP.)
000958,000890:
000959,000891: # -XX-
000960,000892: # POSITION 9 xxxxx. FEET DP BIT 1 OF LOW REGISTER =
000961,000893: # -9
000962,000894: # 2 METERS
000963,000895:
000964,000896: # -YY-
000965,000897: # VELOCITY 4 xxxx.x FEET/SEC DP FRACTIONAL PART
000966,000898: # (MAX 328.0) METERS/CENTI-SEC
000967,000899:
000968,000900: # -AAA-
000969,000901: # RADIANS xx.xxx RADIANS DP BIT 1 OF HIGH REGISTER -
000970,000902: # (MAX 31.999) -9
000971,000903: # 2 RADIANS.
000972,000904:
000973,000905:
000974,000906: # THAT-S ALL ON THE NOUNS.
000975,000907:
000976,000908: # Page 28
000977,000909: # ALARM CODES FOR LUMINARY
000978,000910:
000979,000911: # *9 *18 *60 COLUMN
000980,000912:
000981,000913: # CODE * TYPE SET BY
000982,000914:
000983,000915: # 00107 MORE THAN 5 MARK PAIRS AOTMARK
000984,000916: # 00111 MARK MISSING AOTMARK
000985,000917: # 00112 MARK OR MARK REJECT NOT BEING ACCEPTED AOTMARK
000986,000918: # 00113 NO INBITS AOTMARK
000987,000919: # 00114 MARK MADE BUT NOT DESIRED AOTMARK
000988,000920: # 00115 NO MARKS IN LAST PAIR TO REJECT AOTMARK
000989,000921: # 00206 ZERO ENCODE NOT ALLOWED WITH COARDS ALIGN IMU MODE SWITCHING
000990,000922: # 00206 + GIMBAL LOC
000991,000923: # 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT
000992,000924: # 00210 IMU NOT OPERATING IMU MODE SWITCH, IMU-2, R02, P51, P57
000993,000925: # 00211 COARSE ALIGN ERROR IMU MODE SWITCH
000994,000926: # 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH, T4RPT
000995,000927: # 00213 IMU NOT OPERATING WITH TURN-ON REQUEST T4RUPT
000996,000928: # 00214 PROGRAM USING IMU WHEN TURNED OFF T4RUPT
000997,000929: # 00217 BAD RETURN FROM IMUSTALL P51, P52, P57
000998,000930: # 00220 IMU NOT ALIGNED - NO REFSMMAT R02, R47
000999,000931: # 00401 DESIRED GIMBAL ANGLE YIELDS GIMBAL LOCK INF ALIGN, IMU-2,
001000,000932: # FINDCDUW
001001,000933: # 00402 FINDCDUW NOT CONTROLLING ATTITUDE FINDCDUW
001002,000934: # 00404 TWO STARS NOT AVAILABLE IN ANY DETENT R59, LUNAR SURFACE
001003,000935: # 00405 TWO STARS NOT AVAILABLE P52
001004,000936: # 00421 W-MATRIX OVERFLOW INTEGRV
001005,000937: # 00501 P RADAR ANTENNA OUT OF LIMITS R23
001006,000938: # 00502 BAD RADAR GIMBAL ANGLE INPUT V4IN72
001007,000939: # 00503 P RADAR ANTENNA DESIGNATE FAIL R21, NON-P IN V4IN72
001008,000940: # 00510 RADAR AUTO DESCRETE NOT PRESENT R25
001009,000941: # 00511 L4 NOT IN POSITION 2 OR REPOSITIONING SERVICER
001010,000942: # 00514 P RR GOES OUT OF AUTO MODE WHILE IN USE P20
001011,000943: # 00515 RR CDU FAIL DISCRETE PRESENT R25
001012,000944: # 00520 RADAR RUPT NOT EXPECTED AT THIS TIME RADAR READ
001013,000945: # 00521 COULD NOT READ RADAR P20
001014,000946: # 00522 LANDING RADAR POSITION CHANGE RADAR READ
001015,000947: # 00523 P LR ANTENNA DIDN'T ACHIEVE POSITION 2 SERVICER, V60 (NON-P IN V60)
001016,000948: # 00525 P DELTA THETA GREATER THAN 3 DEGREES R22
001017,000949: # 00526 P RANGE GREATER THAN 400 NAUT. MILES P20, P22
001018,000950: # 00527 P LOS NOT IN MODE II COVERAGE WHILE ON R21, R24
001019,000951: # LUNAR SURFACE
001020,000952: # OR VEHICLE MANEUVER REQUIRED R24 (20)
001021,000953: # 00530 P LOS NOT IN MODE2 COVERAGE R21
001022,000954: # ON LUNAR SURFACE AFTR 600 SECS.
001023,000955: # 00600 IMAGINARY ROOTS ON FIRST ITERATION P32, P72
001024,000956: # 00601 PERIGEE ALTITUDE CSI LT PMIN1 P32, P72.
001025,000957: # 00602 PERIGEE ALTITUDE CDH LT PMIN2 P32, P72.
001026,000958: # 00603 CSI TO CDH TIME LT TMIN12 P32, P72, P33, P73
001027,000959: # Page 29
001028,000960: # 00604 CDH TO TPI TIME LT TMIN23 P32, P72
001029,000961: # OR COMPUTED CDH TIME GREATER THAN INPUT TP1 TIME
001030,000962: # 00605 NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM P32, P72
001031,000963: # 00606 DV EXCEEDS MAXIMUM P32, P72
001032,000964: # 00611 NO TIG FOR GIVEN ELEV ANGLE P34, P74
001033,000965: # 00701 ILLEGAL OPTION CODE SELECTED P57
001034,000966: # 00777 PIPA FAIL CAUSED THE ISS WARNING T4RUPT
001035,000967: # 01102 AGC SELF TEST ERROR SELF CHECK
001036,000968: # 01105 DOWNLINK TOO FAST T4RUPT
001037,000969: # 01106 UPLINK TOO FAST T4RUPT
001038,000970: # 01107 PHASE TABLE FAILURE. ASSUME RESTART
001039,000971: # ERASABLE MEMORY IS SUSPECT. RESTART
001040,000972: # 01301 ARCSIN-ARCCOS ARGUMENT TOO LARGE INTERPRETER
001041,000973: # 01406 BAD RETURN FROM ROOTPSRS DESCENT GUIDANCE EQS.
001042,000974: # 01407 VG INCREASING (DELTA-V ACCUMULATED S40.8
001043,000975: # .GT. 90 DEGREES AWAY FROM DESIRED THRUST S40.8
001044,000976: # VECTOR.) S40.8
001045,000977: # 01410 UNINTENTIONAL OVERFLOW IN GUIDANCE DESCENT GUIDANCE EQS.
001046,000978: # 01412 DESCENT IGNALG NOT CONVERGING P63
001047,000979: # 01520 V37 REQUEST NOT PERMITTED AT THIS TIME V37
001048,000980: # 01600 OVERFLOW IN DRIFT TEST IMU 4
001049,000981: # 01601 BAD IMU TORQUE OPT PRE ALIGN CALIB
001050,000982: # IMU 4 (LEM)
001051,000983: # 01703 IGNITION TIME SLIPPED MIDTOAVE
001052,000984: # 01706 INCORRECT PROGRAM REQUESTED FOR VEHICLE
001053,000985: # CONFIGURATION P40, P42
001054,000986: # 02001 JET FAILURES HAVE DISABLED Y-Z TRANS. DAP
001055,000987: # 02002 JET FAILURES HAVE DISABLED X TRANSLATION DAP
001056,000988: # 02003 JET FAILURES HAVE DISABLED P-ROTATION DAP
001057,000989: # 02004 JET FAILURES HAVE DISABLED U-V ROTATION DAP
001058,000990: # 03777 ICDU FAIL CAUSED THE ISS WARNING T4RUPT
001059,000991: # 04777 ICDU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001060,000992: # 07777 IMU FAIL CAUSED THE ISS WARNING T4RUPT
001061,000993: # 10777 IMU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001062,000994: # 13777 IMU, ICDU FAILS CAUSED THE ISS WARNING T4RUPT
001063,000995: # 14777 IMU, ICDU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001064,000996:
001065,000997: # THE FOLLOWING CODES INDICATE THE MORE SERIOUS P00DOO ABORTS THAT RESULT
001066,000998: # IN THE PROGRAM GOING TO R00.
001067,000999:
001068,001000: # 20105 AOTMARK SYSTEM IN USE AOTMARK
001069,001001: # 20430 ACCELERATON OVERFLOW IN INTEGRATION ORBITAL INTEGRATION
001070,001002: # 20607 NO SOLN FROM TIME-THETA OR TIME-RADIUS TIMETHET, TIMERAD
001071,001003: # 21103 UNUSED CCS BRANCH EXECUTED ABORT
001072,001004: # 21204 WAITLIST, VARDELAY, FIXDELAY, OR LONGCALL WAITLIST ROUTINES
001073,001005: # CALLED WITH ZERO OR NEGATIVE DELTA-TIME
001074,001006: # 21302 SQRT CALLED WITH NEGATIVE ARGUMENT INTERPRETER
001075,001007: # 21406 BAD RETURN FROM ROOTRSRS IGNITION ALGORITHM
001076,001008: # 21501 KEYBOARD AND DISPLAY ALARM DURING PINBALL
001077,001009: # INTERNAL USE(NVSUB).ABORT
001078,001010:
001079,001011: # Page 30
001080,001012: # THE FOLLOWING CODE INDICATE A BAILOUT ABORT THAT RESULTS IN A SOFTWARE
001081,001013: # RESTART
001082,001014:
001083,001015: # 31104 DELAY ROUTINE BUSY EXEC
001084,001016: # 31201 EXECUTIVE OVERFLOW-NO VAC AREAS EXEC
001085,001017: # 31202 EXECUTIVE OVERFLOW-NO CORE SETS EXEC
001086,001018: # 31203 WAITLIST OVERFLOW-TOO MANY TASKS WAITLIST
001087,001019: # 31206 SECOND JOB ATTEMPTS TO GO TO SLEEP VIA PINBALL
001088,001020: # KEYBOARD AND DISPLAY PROGRAM
001089,001021: # 31207 NO VAC AREAS FOR MARKS AOTMARK
001090,001022: # 31210 TWO PROGRAMS USING DEVICE AT THE SAME TIME MODE-SWITCHING
001091,001023: # 31211 ILLEGAL INTERRUPT OF EXTENDED VERB AOTMARK
001092,001024: # 31502 TWO PRIO DISPLAYS WAITING DSP INTRFCE
001093,001025: # 32000 DAP STILL IN PROGRESS AT NEXT TIMES RUPT DAP
001094,001026:
001095,001027: # Page 31
001096,001028: # CHECKLIST CODES FOR LUMINARY
001097,001029:
001098,001030: # *9 *17 *26 *9 COLUMN
001099,001031:
001100,001032: # R1CODE ACTION TO BE EFFECTED PROGRAM
001101,001033:
001102,001034: # 00013 KEY IN NORMAL OR GYRO TORQUE COARSE ALIGN P52
001103,001035: # 00014 PROCEED DO IMU FINE ALIGN ROUTINE P51, P63, P57
001104,001036: # 00014 ENTER DO LANDING SITE DETERMINATION(N89DISP) P57OPTION2
001105,001037: # 00015 PERFORM CELESTIAL BODY ACQUISITION R51, P51
001106,001038: # 00062 SWITCH AGC POWER DOWN P06
001107,001039: # 00201 SWITCH RR MODE TO AUTOMATIC P20, P22, R04
001108,001040: # 00203 SWITCH GUID CONTROL TO GNC, MODE TO AUTO... P12, P42, P71
001109,001041: # ALSO THR CONT TO AUTO P40, P63, P70
001110,001042: # 00205 PERFORM MANUAL ACQUISITION OF RR R23
001111,001043: # 00500 SWITCH LR ANTENNA TO POSITION 1 P63
001112,001044:
001113,001045: # SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
001114,001046: # PERFORM DENOTES START OR END OF A TASK
001115,001047: # KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
001116,001048:
001117,001049: # Page 32
001118,001050: # OPTION CODES FOR LUMINARY
001119,001051:
001120,001052: # THE SPECIFIED OPTION CODES WIL BE FLASHED IN COMPONENT R1 IN
001121,001053: # CONJUNCTION WITH V04N06 OR V04N12 (FOR EXTENDED VERBS) TO REQUEST THE
001122,001054: # ASTRONAUT TO LOAD INTO COMPONENT R2 THE OPTION HE DESIRES.
001123,001055:
001124,001056: # *9 *17 *52 *11 *25 COLUMN
001125,001057:
001126,001058: # OPTION
001127,001059: # CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
001128,001060:
001129,001061: # 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P52 ALL
001130,001062: # 4=LAND SITE
001131,001063: # 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
001132,001064: # 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
001133,001065: # 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
001134,001066: # 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
001135,001067: # 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
001136,001068: # 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
001137,001069: # 2=TWO BODIES 3=ONE BODY + G
001138,001070: # 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
001139,001071: # ORBIT TO PASS OVER LM.
001140,001072:
End of include-file ASSEMBLY_AND_OPERATION_INFORMATION.agc. Parent file is MAIN.agc