Source Code
|
This is a reconstructed version of Luminary 130, the initial AGC program released
in November 1969 for the Apollo 13 LM. Three more releases
followed before the flown revision was finally manufactured in February 1970.
This reconstruction was created from a previous transcription of the original listing of
Luminary 131, combined with Luminary memo #129 which describes the small difference
between the Luminary 130 and 131. The reconstructed source code was verified by
matching memory-bank checksums to those listed for Luminary 130 in drawing 2021152G.
In this source code, program comments from the original (Luminary 131) code are
prefixed with '#', while those added later by the Virtual AGC project are prefixed
with '##'.
|
000096,000002: ## Copyright: Public domain.
000097,000003: ## Filename: ASSEMBLY_AND_OPERATION_INFORMATION.agc
000098,000004: ## Purpose: A section of the reconstructed source code for Luminary 130.
000099,000005: ## This was the original program released for the Apollo 13 LM,
000100,000006: ## although several more revisions would follow. It has been
000101,000007: ## reconstructed from a listing of Luminary 131, from which it
000102,000008: ## differs on only two lines in P70-P71. The difference is
000103,000009: ## described in detail in Luminary memo #129, which was used
000104,000010: ## to perform the reconstruction. This file is intended to be a
000105,000011: ## faithful reconstruction, except that the code format has been
000106,000012: ## changed to conform to the requirements of the yaYUL assembler
000107,000013: ## rather than the original YUL assembler.
000108,000014: ## Reference: Pages 1-27
000109,000015: ## Contact: Ron Burkey <info@sandroid.org>.
000110,000016: ## Website: www.ibiblio.org/apollo/index.html
000111,000017: ## Mod history: 04/12/03 RSB. Began transcribing.
000112,000018: ## 04/23/03 RSB Finished draft.
000113,000019: ## 12/06/03 RSB Did some proofing.
000114,000020: ## 05/14/05 RSB Corrected website reference above.
000115,000021: ## 2010-08-24 JL FiXed a bunch of page number comments.
000116,000022: ## 2017-01-06 RSB Page numbers now agree with those on the
000117,000023: ## original harcopy, as opposed to the PDF page
000118,000024: ## numbers in 1701.pdf.
000119,000025: ## 2017-01-25 RSB Back-ported a typo-fix found while proofing Luminary 69.
000120,000026: ## 2017-02-12 RSB Proofed comment text using octopus/ProoferComments.
000121,000027: ## 2017-02-18 MAS Backported some typo fixes from Luminary 116.
000122,000028: ## 2017-02-28 RSB Lingering typos repaired.
000123,000029: ## 2017-03-14 RSB Comment-text fixes identified in 5-way
000124,000030: ## side-by-side diff of Luminary 69/99/116/131/210.
000125,000031: ## 2017-03-15 RSB More of the same.
000126,000032: ## 2018-09-04 MAS Copied from Luminary 131 for Luminary 130.
000127,000033:
|
|
Page 1
|
000129,000035:
000130,000036: # THIS LGC PROGRAM IS INTENDED FOR USE IN THE LM DURING THE MANNED LUNAR LANDING MISSION OR ANY SUBSET THEREOF.
000131,000037: # THE DETAILS OF IMPLEMENTATION ARE SPECIFIED IN REPORT R-567, AS AMENDED.
000132,000038:
000133,000039: # GUIDANCE SYSTEM OPERATIONS PLAN
000134,000040: # FOR MANNED LM EARTH ORBITAL AND LUNAR MISSIONS
000135,000041: # USING PROGRAM LUMINARY
000136,000042:
000137,000043: # THIS PROGRAM AND R-567 HAVE BEEN PREPARED BY THE INSTRUMENTATION LABORATORY, MASSACHUSETTS INSTITUTE OF
000138,000044: # TECHNOLOGY 75 CAMBRIDGE PARKWAY, CAMBRIDGE, MASSACHUSETTS UNDER PROJECT 55-238-70, SPONSORED BY THE MANNED
000139,000045: # SPACECRAFT CENTER OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, CONTRACT NAS 9-4065.
000140,000046:
000141,000047: # THIS PROGRAM IS REFERRED TO AS LUMINARY 1C
000142,000048:
|
|
Page 2
|
000144,000050: # TABLE OF LOG CARDS
000145,000051: # ABSOLUTE ADDRESSES FOR UPDATE PROGRAM
000146,000052: # ASSEMBLY AND OPERATION INFORMATION
000147,000053: # TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
000148,000054: # CONTROLLED CONSTANTS
000149,000055: # INPUT/OUTPUT CHANNEL BIT DESCRIPTIONS
000150,000056: # FLAGWORD ASSIGNMENTS
000151,000057: # SUBROUTINE CALLS
000152,000058:
000153,000059: # TABLE OF SUBROUTINE LOG SECTIONS
000154,000060: # LUMERASE
000155,000061: # ERASABLE ASSIGNMENTS
000156,000062: # LEMONAID
000157,000063: # INTERRUPT LEAD INS
000158,000064: # T4RUPT PROGRAM
000159,000065: # RCS FAILURE MONITOR
000160,000066: # DOWNLINK LISTS
000161,000067: # AGS INITIALIZATION
000162,000068: # FRESH START AND RESTART
000163,000069: # RESTART TABLES
000164,000070: # AOTMARK
000165,000071: # EXTENDED VERBS
000166,000072: # PINBALL NOUN TABLES
000167,000073: # LEM GEOMETRY
000168,000074: # IMU COMPENSATION PACKAGE
000169,000075: # R63
000170,000076: # ATTITUDE MANEUVER ROUTINE
000171,000077: # GIMBAL LOCK AVOIDANCE
000172,000078: # KALCMANU STEERING
000173,000079: # SYSTEM TEST STANDARD LEAD INS
000174,000080: # IMU PERFORMANCE TESTS 2
000175,000081: # IMU PERFORMANCE TESTS 4
000176,000082: # PINBALL GAMES BUTTONS AND LIGHTS
000177,000083: # R60,R62
000178,000084: # S-BAND ANTENNA FOR LM
000179,000085: # LEMP20S
000180,000086: # RADAR LEADIN ROUTINES
000181,000087: # P20-P25
000182,000088: # LEMP30S
000183,000089: # P30,P37
000184,000090: # P32-P35, P72-P75
000185,000091: # KISSING
000186,000092: # GROUND TRACKING DETERMINATION PROGRAM - P21
000187,000093: # P34-P35, P74-P75
000188,000094: # R31
000189,000095: # P76
000190,000096: # R30
000191,000097: # FLY
|
|
Page 3
|
000193,000099: # BURN, BABY, BURN -- MASTER IGNITION ROUTINE
000194,000100: # P40-P47
000195,000101: # THE LUNAR LANDING
000196,000102: # THROTTLE CONTROL ROUTINES
000197,000103: # LUNAR LANDING GUIDANCE EQUATIONS
000198,000104: # P70-P71
000199,000105: # P12
000200,000106: # ASCENT GUIDANCE
000201,000107: # SERVICER
000202,000108: # LANDING ANALOG DISPLAYS
000203,000109: # FINDCDUW - GUIDAP INTERFACE
000204,000110: # LEMP50S
000205,000111: # P51-P53
000206,000112: # LUNAR AND SOLAR EPHEMERIDES SUBROUTINES
000207,000113: # SKIPPER
000208,000114: # DOWN-TELEMETRY PROGRAM
000209,000115: # INTER-BANK COMMUNICATION
000210,000116: # INTERPRETER
000211,000117: # FIXED-FIXED CONSTANT POOL
000212,000118: # INTERPRETIVE CONSTANTS
000213,000119: # SINGLE PRECISION SUBROUTINES
000214,000120: # EXECUTIVE
000215,000121: # WAITLIST
000216,000122: # LATITUDE LONGITUDE SUBROUTINES
000217,000123: # PLANETARY INERTIAL ORIENTATION
000218,000124: # MEASUREMENT INCORPORATION
000219,000125: # CONIC SUBROUTINES
000220,000126: # INTEGRATION INITIALIZATION
000221,000127: # ORBITAL INTEGRATION
000222,000128: # INFLIGHT ALIGNMENT ROUTINES
000223,000129: # POWERED FLIGHT SUBROUTINES
000224,000130: # TIME OF FREE FALL
000225,000131: # AGC BLOCK TWO SELF-CHECK
000226,000132: # PHASE TABLE MAINTENANCE
000227,000133: # RESTARTS ROUTINE
000228,000134: # IMU MODE SWITCHING ROUTINES
000229,000135: # KEYRUPT, UPRUPT
000230,000136: # DISPLAY INTERFACE ROUTINES
000231,000137: # SERVICE ROUTINES
000232,000138: # ALARM AND ABORT
000233,000139: # UPDATE PROGRAM
000234,000140: # RTB OP CODES
000235,000141: # LMDAP
000236,000142: # T6-RUPT PROGRAMS
000237,000143: # DAP INTERFACE SUBROUTINES
000238,000144: # DAPIDLER PROGRAM
000239,000145: # P-AXIS RCS AUTOPILOT
000240,000146: # Q,R-AXIS RCS AUTOPILOT
000241,000147: # TJET LAW
000242,000148: # KALMAN FILTER
|
|
Page 4
|
000244,000150: # TRIM GIMBAL CONTROL SYSTEM
000245,000151: # AOSTASK AND AOSJOB
000246,000152: # SPS BACK-UP RCS CONTROL
000247,000153:
000248,000154: # SYMBOL TABLE LISTING
000249,000155: # UNREFERENCED SYMBOL LISTING
000250,000156: # ERASABLE & EQUALS CROSS-REFERENCE TABLE
000251,000157: # SUMMARY OF SYMBOL TABLE LISTINGS
000252,000158: # MEMORY TYPE & AVAILABLITY DISPLAY
000253,000159: # COUNT TABLE
000254,000160: # PARAGRAPHS GENERATED FOR THIS ASSEMBLY
000255,000161: # OCTAL LISTING
000256,000162: # OCCUPIED LOCATIONS TABLE
000257,000163: # SUBROS CALLED & PROGRAM STATUS
000258,000164:
|
|
Page 5
|
000260,000166: # VERB LIST FOR LUMINARY
000261,000167:
000262,000168: # REGULAR VERBS
000263,000169:
000264,000170: # 00 NOT IN USE
000265,000171: # 01 DISPLAY OCTAL COMP 1 IN R1
000266,000172: # 02 DISPLAY OCTAL COMP 2 IN R1
000267,000173: # 03 DISPLAY OCTAL COMP 3 IN R1
000268,000174: # 04 DISPLAY OCTAL COMP 1,2 IN R1,R2
000269,000175: # 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3
000270,000176: # 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000271,000177: # 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY)
000272,000178: # 08
000273,000179: # 09
000274,000180: # 10
000275,000181: # 11 MONITOR OCTAL COMP 1 IN R1
000276,000182: # 12 MONITOR OCTAL COMP 2 IN R1
000277,000183: # 13 MONITOR OCTAL COMP 3 IN R1
000278,000184: # 14 MONITOR OCTAL COMP 1,2 IN R1,R2
000279,000185: # 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3
000280,000186: # 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000281,000187: # 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY)
000282,000188: # 18
000283,000189: # 19
000284,000190: # 20
000285,000191: # 21 LOAD COMPONENT 1 INTO R1
000286,000192: # 22 LOAD COMPONENT 2 INTO R2
000287,000193: # 23 LOAD COMPONENT 3 INTO R3
000288,000194: # 24 LOAD COMPONENT 1,2 INTO R1,R2
000289,000195: # 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3
000290,000196: # 26
000291,000197: # 27 DISPLAY FIXED MEMORY
000292,000198: # 28
000293,000199: # 29
000294,000200: # 30 REQUEST EXECUTIVE
000295,000201: # 31 REQUEST WAITLIST
000296,000202: # 32 RECYCLE PROGRAM
000297,000203: # 33 PROCEED WITHOUT DSKY INPUTS
000298,000204: # 34 TERMINATE FUNCTION
000299,000205: # 35 TEST LIGHTS
000300,000206: # 36 REQUEST FRESH START
000301,000207: # 37 CHANGE PROGRAM (MAJOR MODE)
000302,000208: # 38
000303,000209: # 39
000304,000210:
|
|
Page 6
|
000306,000212: # EXTENDED VERBS
000307,000213:
000308,000214: # 40 ZERO CDU-S
000309,000215: # 41 COARSE ALIGN CDU-S
000310,000216: # 42 FINE ALIGN IMU
000311,000217: # 43 LOAD IMU ATT ERROR METERS
000312,000218: # 44 TERMINATE RR CONTINUOUS DESIGNATE (V41N72 OPTION 2)
000313,000219: # 45
000314,000220: # 46
000315,000221: # 47 INITIALIZE AGS (R47)
000316,000222: # 48 REQUEST DAP DATA LOAD ROUTINE (R03)
000317,000223: # 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
000318,000224: # 50 PLEASE PERFORM
000319,000225: # 51
000320,000226: # 52 MARK X-RETICLE
000321,000227: # 53 MARK Y-RETICLE
000322,000228: # 54 MARK X OR Y-RETICLE
000323,000229: # 55 INCREMENT AGC TIME (DECIMAL)
000324,000230: # 56 TERMINATE TRACKING (P20 + P25)
000325,000231: # 57 PERMIT LANDING RADAR UPDATES
000326,000232: # 58 INHIBIT LANDING RADAR UPDATES
000327,000233: # 59 COMMAND LR TO POSITION 2.
000328,000234: # 60 DISPLAY VEHICLE ATTITUDE RATES ON FDAI ERROR NEEDLES.
000329,000235: # 61 DISPLAY DAP FOLLOWING ATTITUDE ERRORS.
000330,000236: # 62 DISPLAY TOTAL ATTITUDE ERRORS WITH RESPECT TO NOUN 22.
000331,000237: # 63 SAMPLE RADAR ONCE PER SECOND (R04).
000332,000238: # 64 REQUEST S-BAND ANTENNA ROUTINE (R05)
000333,000239: # 65 DISABLE U AND V JET FIRINGS DURING DPS BURNS.
000334,000240: # 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
000335,000241: # 67 DISPLAY W MATRIX
000336,000242: # 68
000337,000243: # 69 CAUSE RESTART
000338,000244: # 70 UPDATE LIFTOFF TIME
000339,000245: # 71 UNIVERSAL UPDATE-BLOCK ADR
000340,000246: # 72 UNIVERSAL UPDATE-SINGLE ADR
000341,000247: # 73 UPDATE AGC TIME (OCTAL)
000342,000248: # 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK
000343,000249: # 75 ENABLE U AND V JET FIRINGS DURING DPS BURNS.
000344,000250: # 76 MINIMUM IMPULSE COMMAND MODE
000345,000251: # 77 RATE COMMAND AND ATTITUDE HOLD MODE
000346,000252: # 78 LR SPURIOUS RETURN TEST START (R77)
000347,000253: # 79 LR SPURIOUS RETURN TEST STOP
000348,000254: # 80 UPDATE LEM STATE VECTOR
000349,000255: # 81 UPDATE CSM STATE VECTOR
000350,000256: # 82 REQUEST ORBIT PARAM DISPLAY (R30)
000351,000257: # 83 REQUEST REND PARAM DISPLAY (R31)
000352,000258: # 84
000353,000259: # 85 DISPLAY RR LOS AZ AND ELEV
000354,000260: # 86
000355,000261: # 87
|
|
Page 7
|
000357,000263: # 88
000358,000264: # 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
000359,000265: # 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
000360,000266: # 91 DISPLAY BANK SUM
000361,000267: # 92 OPERATE IMU PERFORMANCE TEST (P07)
000362,000268: # 93 ENABLE W MATRIX INITIALIZATION
000363,000269: # 94
000364,000270: # 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
000365,000271: # 96 INTERRUPT INTEGRATION AND GO TO POO
000366,000272: # 97 PERFORM ENGINE FAIL PROCEDURE
000367,000273: # 98
000368,000274: # 99 PLEASE ENABLE ENGINE
000369,000275:
|
|
Page 8
|
000371,000277: # IN THE FOLLOWING NOUN LIST THE :NO LOAD: RESTRICTION MEANS THE NOUN
000372,000278: # CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
000373,000279: # SCALE TYPE L (MIN/SEC), PP (2 INTEGERS) OR TT (LANDING RADAR POSITION).
000374,000280: # IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22 OR 23
000375,000281: # MAY BE USED TO LOAD ANY OF THE NOUN:S COMPONENTS WHICH ARE NOT OF THE
000376,000282: # ABOVE SCALE TYPES.
000377,000283:
000378,000284: # THE :DEC ONLY: RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
000379,000285: # EVERY COMPONENT IN THE NOUN. (NOTE THAT :NO LOAD: IMPLIES :DEC ONLY:.)
000380,000286:
000381,000287: # NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000382,000288: # 00 NOT IN USE
000383,000289: # 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .XXXXX FOR EACH
000384,000290: # 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP XXXXX. FOR EACH
000385,000291: # 03 SPECIFY MACHINE ADDRESS (DEGREES) 3COMP XXX.XX DEG FOR EACH
000386,000292: # 04 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000387,000293: # 05 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000388,000294: # 06 OPTION CODE 3COMP OCTAL ONLY FOR EACH
000389,000295: # LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER
000390,000296: # 07 ECADR OF WORD TO BE MODIFIED 3COMP OCTAL ONLY FOR EACH
000391,000297: # ONES FOR BITS TO BE MODIFIED
000392,000298: # 1 TO SET OR 0 TO RESET SELECTED BITS
000393,000299: # 08 ALARM DATA 3COMP OCTAL ONLY FOR EACH
000394,000300: # 09 ALARM CODES 3COMP OCTAL ONLY FOR EACH
000395,000301: # 10 CHANNEL TO BE SPECIFIED 1COMP OCTAL ONLY
000396,000302: # 11 TIG OF CSI 3COMP 00XXX. HRS DEC ONLY
000397,000303: # 000XX. MIN MUST LOAD 3 COMPS
000398,000304: # 0XX.XX SEC
000399,000305: # 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH
000400,000306: # (USED BY EXTENDED VERBS ONLY)
000401,000307: # 13 TIG OF CDH 3COMP 00XXX. HRS DEC ONLY
000402,000308: # 000XX. MIN MUST LOAD 3 COMPS
000403,000309: # 0XX.XX SEC
000404,000310: # 14 CHECKLIST 3COMP XXXXX. FOR EACH
000405,000311: # (USED BY EXTENDED VERBS ONLY)
000406,000312: # (NOUN 25 IS PASTED AFTER DISPLAY)
000407,000313: # 15 INCREMENT MACHINE ADDRESS 1COMP OCTAL ONLY
000408,000314: # 16 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000409,000315: # (USED BY EXTENDED VERBS ONLY) 000XX. MIN MUST LOAD 3 COMPS
000410,000316: # 0XX.XX SEC
000411,000317: # 17 SPARE
000412,000318: # 18 AUTO MANEUVER BALL ANGLES 3COMP XXX.XX DEG FOR EACH
000413,000319: # 19 SPARE
000414,000320: # 20 ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000415,000321: # 21 PIPAS 3COMP XXXXX. PULSES FOR EACH
000416,000322: # 22 NEW ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000417,000323: # 23 SPARE
000418,000324: # 24 DELTA TIME FOR AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000419,000325: # 000XX. MIN MUST LOAD 3 COMPS
000420,000326: # 0XX.XX SEC
|
|
Page 9
|
000422,000328: # 25 CHECKLIST 3COMP XXXXX. FOR EACH
000423,000329: # (USED WITH PLEASE PERFORM ONLY)
000424,000330: # 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH
000425,000331: # 27 SELF TEST ON/OFF SWITCH 1COMP XXXXX.
000426,000332: # 28 SPARE
000427,000333: # 29 SPARE
000428,000334: # 30 SPARE
000429,000335: # 31 SPARE
000430,000336: # 32 TIME FROM PERIGEE 3COMP 00XXX. HRS DEC ONLY
000431,000337: # 000XX. MIN MUST LOAD 3 COMPS
000432,000338: # 0XX.XX SEC
000433,000339: # 33 TIME OF IGNITION 3COMP 00XXX. HRS DEC ONLY
000434,000340: # 000XX. MIN MUST LOAD 3 COMPS
000435,000341: # 0XX.XX SEC
000436,000342: # 34 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000437,000343: # 000XX. MIN MUST LOAD 3 COMPS
000438,000344: # 0XX.XX SEC
000439,000345: # 35 TIME FROM EVENT 3COMP 00XXX. HRS DEC ONLY
000440,000346: # 000XX. MIN MUST LOAD 3 COMPS
000441,000347: # 0XX.XX SEC
000442,000348: # 36 TIME OF AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000443,000349: # 000XX. MIN MUST LOAD 3 COMPS
000444,000350: # 0XX.XX SEC
000445,000351: # 37 TIG OF TPI 3COMP 00XXX. HRS DEC ONLY
000446,000352: # 000XX. MIN MUST LOAD 3 COMPS
000447,000353: # 0XX.XX SEC
000448,000354: # 38 TIME OF STATE BEING INTEGRATED 3COMP 00XXX. HRS DEC ONLY
000449,000355: # 000XX. MIN MUST LOAD 3 COMPS
000450,000356: # 0XX.XX SEC
000451,000357: # 39 SPARE
000452,000358:
|
|
Page 10
|
000454,000360: # MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000455,000361: # 40 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000456,000362: # VG, XXXX.X FT/SEC
000457,000363: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000458,000364: # 41 TARGET AZIMUTH , 2COMP XXX.XX DEG (FOR SYSTEM TEST)
000459,000365: # ELEVATION XX.XXX DEG
000460,000366: # 42 APOGEE, 3COMP XXXX.X NAUT MI DEC ONLY
000461,000367: # PERIGEE, XXXX.X NAUT MI
000462,000368: # DELTA V (REQUIRED) XXXX.X FT/SEC
000463,000369: # 43 LATITUDE, 3COMP XXX.XX DEG DEC ONLY
000464,000370: # LONGITUDE, XXX.XX DEG
000465,000371: # ALTITUDE XXXX.X NAUT MI
000466,000372: # 44 APOGEE, 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000467,000373: # PERIGEE, XXXX.X NAUT MI
000468,000374: # TFF XXBXX MIN/SEC
000469,000375: # 45 MARKS, 3COMP XXXXX. NO LOAD, DEC ONLY
000470,000376: # TFI OF NEXT BURN XXBXX MIN/SEC
000471,000377: # MGA XXX.XX DEG
000472,000378: # 46 AUTOPILOT CONFIGURATION 1COMP OCTAL ONLY
000473,000379: # 47 LEM WEIGHT, 2COMP XXXXX. LBS DEC ONLY
000474,000380: # CSM WEIGHT XXXXX. LBS
000475,000381: # 48 GIMBAL PITCH TRIM, 2COMP XXX.XX DEG DEC ONLY
000476,000382: # GIMBAL ROLL TRIM XXX.XX DEG
000477,000383: # 49 DELTA R, 3COMP XXXX.X NAUT MI DEC ONLY
000478,000384: # DELTA V, XXXX.X FT/SEC
000479,000385: # RADAR DATA SOURCE CODE XXXXX.
000480,000386: # 50 SPARE
000481,000387: # 51 S-BAND ANTENNA ANGLES PITCH 2COMP XXX.XX DEG DEC ONLY
000482,000388: # YAW XXX.XX DEG
000483,000389: # 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP XXX.XX DEG
000484,000390: # 53 SPARE
000485,000391: # 54 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY
000486,000392: # RANGE RATE, XXXX.X FT/SEC
000487,000393: # THETA XXX.XX DEG
000488,000394: # 55 NO. OF APSIDAL CROSSINGS 3COMP XXXXX. DEC ONLY
000489,000395: # ELEVATION ANGLE XXX.XX DEG
000490,000396: # CENTRAL ANGLE OF PASSIVE VEHICLE XXX.XX DEG
000491,000397: # 56 RR LOS AZIMUTH 2COMP XXX.XX DEG
000492,000398: # ELEVATION XXX.XX DEG
000493,000399: # 57 SPARE
000494,000400: # 58 PERIGEE ALT (POST TPI) 3COMP XXXX.X NAUT MI DEC ONLY
000495,000401: # DELTA V TPI XXXX.X FT/SEC
000496,000402: # DELTA V TPF XXXX.X FT/SEC
000497,000403: # 59 DELTA VELOCITY LOS 3COMP XXXX.X FT/SEC FOR EA. DEC ONLY
000498,000404: # 60 FORWARD VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000499,000405: # ALTITUDE RATE XXXX.X FT/SEC
000500,000406: # COMPUTED ALTITUDE XXXXX. FEET
000501,000407: # 61 TIME TO GO IN BRAKING PHASE 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000502,000408: # TIME FROM IGNITION XXBXX MIN/SEC
|
|
Page 11
|
000504,000410: # CROSS RANGE DISTANCE XXXX.X NAUT MI
000505,000411: # 62 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC NO LOAD, DEC ONLY
000506,000412: # TIME FROM IGNITION XXBXX MIN/SEC
000507,000413: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000508,000414: # 63 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000509,000415: # ALTITUDE RATE XXXX.X FT/SEC
000510,000416: # COMPUTED ALTITUDE XXXXX. FEET
000511,000417: # 64 TIME LEFT FOR REDESIGNATION- LPD ANGLE 3COMP XXBXX NO LOAD, DEC ONLY
000512,000418: # ALTITUDE RATE XXXX.X FT/SEC
000513,000419: # COMPUTED ALTITUDE XXXXX. FEET
000514,000420: # 65 SAMPLED AGC TIME 3COMP 00XXX. HRS DEC ONLY
000515,000421: # (FETCHED IN INTERRUPT) 000XX. MIN MUST LOAD 3 COMPS
000516,000422: # 0XX.XX SEC
000517,000423: # 66 LR RANGE 2COMP XXXXX. FEET NO LOAD, DEC ONLY
000518,000424: # POSITION +0000X
000519,000425: # 67 LRVX 3COMP XXXXX. FT/SEC
000520,000426: # LRVY XXXXX. FT/SEC
000521,000427: # LRVZ XXXXX. FT/SEC
000522,000428: # 68 SLANT RANGE TO LANDING SITE 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000523,000429: # TIME TO GO IN BRAKING PHASE XXBXX MIN/SEC
000524,000430: # LR ALTITUDE - COMPUTED ALTITUDE XXXXX. FEET
000525,000431: # 69 LANDING SITE CORRECTION, Z-COMPONENT 3COMP XXXXX. FEET DEC ONLY
000526,000432: # LANDING SITE CORRECTION, Y-COMPONENT XXXXX. FEET
000527,000433: # LANDING SITE CORRECTION, X-COMPONENT XXXXX. FEET
000528,000434: # 70 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000529,000435: # 71 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000530,000436: # 72 RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000531,000437: # SHAFT ANGLE XXX.XX DEG
000532,000438: # 73 NEW RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000533,000439: # SHAFT ANGLE XXX.XX DEG
000534,000440: # 74 TIME FROM IGNITION 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000535,000441: # YAW AFTER VEHICLE RISE XXX.XX DEG
000536,000442: # PITCH AFTER VEHICLE RISE XXX.XX DEG
000537,000443: # 75 DELTA ALTITUDE CDH 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000538,000444: # DELTA TIME (CDH-CSI OR TPI-CDH) XXBXX MIN/SEC
000539,000445: # DELTA TIME (TPI-CDH OR TPI-NONTPI) XXBXX MIN/SEC
000540,000446: # 76 DESIRED HORIZONTAL VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000541,000447: # DESIRED RADIAL VELOCITY XXXX.X FT/SEC
000542,000448: # CROSS-RANGE DISTANCE XXXX.X NAUT MI
000543,000449: # 77 TIME TO ENGINE CUTOFF 2COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000544,000450: # VELOCITY NORMAL TO CSM PLANE XXXX.X FT/SEC
000545,000451: # 78 RR RANGE 3COMP XXX.XX NAUT MI NO LOAD, DEC ONLY
000546,000452: # RANGE RATE XXXXX. FT/SEC
000547,000453: # TIME FROM IGNITION XXBXX MIN/SEC
000548,000454: # 79 CURSOR ANGLE 3COMP XXX.XX DEG DEC ONLY
000549,000455: # SPIRAL ANGLE XXX.XX DEG
000550,000456: # POSITION CODE XXXXX.
000551,000457: # 80 DATA INDICATOR, 2COMP XXXXX.
000552,000458: # OMEGA XXX.XX DEG
000553,000459: # 81 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
|
|
Page 12
|
000555,000461: # 82 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000556,000462: # 83 DELTA V (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000557,000463: # 84 DELTA V (OTHER VEHICLE) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000558,000464: # 85 VG (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000559,000465: # 86 VG (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000560,000466: # 87 BACKUP OPTICS LOS AZIMUTH 2COMP XXX.XX DEG
000561,000467: # ELEVATION XXX.XX DEG
000562,000468: # 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .XXXXX FOR EACH DEC ONLY
000563,000469: # 89 LANDMARK LATITUDE 3COMP XX.XXX DEG DEC ONLY
000564,000470: # LONGITUDE/2 XX.XXX DEC
000565,000471: # ALTITUDE XXX.XX NAUT MI
000566,000472: # 90 Y 3COMP XXX.XX NM DEC ONLY
000567,000473: # Y DOT XXXX.X FPS
000568,000474: # PSI XXX.XX DEG
000569,000475: # 91 ALTITUDE 3COMP XXXXXB. NAUT MI
000570,000476: # VELOCITY XXXXX. FT/SEC
000571,000477: # FLIGHT PATH ANGLE XXX.XX DEG
000572,000478: # 92 PCT FTP (10,5K LB) AT PRESENT THRUST 3COMP XXXXX.
000573,000479: # ALTITUDE RATE XXXX.X FT/SEC
000574,000480: # COMPUTED ALTITUDE XXXXX. FEET
000575,000481: # 93 DELTA GYRO ANGLES 3COMP XX.XXX DEG FOR EACH
000576,000482: # 94 SPARE
000577,000483: # 95 SPARE
000578,000484: # 96 SPARE
000579,000485: # 97 SYSTEM TEST INPUTS 3COMP XXXXX. FOR EACH
000580,000486: # 98 SYSTEM TEST RESULTS AND INPUTS 3COMP XXXXX.
000581,000487: # .XXXXX
000582,000488: # XXXXX.
000583,000489: # 99 RMS IN POSITION 3COMP XXXXX. FT DEC ONLY
000584,000490: # RMS IN VELOCITY XXXX.X FT/SEC
000585,000491: # RMS IN BIAS XX.XXX RADIANS
000586,000492:
|
|
Page 13
|
000588,000494: # REGISTERS AND SCALING FOR NORMAL NOUNS
000589,000495:
000590,000496: # NOUN REGISTER SCALE TYPE
000591,000497: # 00 NOT IN USE
000592,000498: # 01 SPECIFY ADDRESS B
000593,000499: # 02 SPECIFY ADDRESS C
000594,000500: # 03 SPECIFY ADDRESS D
000595,000501: # 04 DSPTEM1 H
000596,000502: # 05 DSPTEM1 H
000597,000503: # 06 OPTION1 A
000598,000504: # 07 XREG A
000599,000505: # 08 ALMCADR A
000600,000506: # 09 FAILREG A
000601,000507: # 10 SPECIFY CHANNEL A
000602,000508: # 11 TCSI K
000603,000509: # 12 OPTIONX A
000604,000510: # 13 TCDH K
000605,000511: # 14 DSPTEMX C
000606,000512: # 15 INCREMENT ADDRESS A
000607,000513: # 16 DSPTEMX K
000608,000514: # 17 SPARE
000609,000515: # 18 FDAIX D
000610,000516: # 19 SPARE
000611,000517: # 20 CDUX D
000612,000518: # 21 PIPAX C
000613,000519: # 22 THETAD D
000614,000520: # 23 SPARE
000615,000521: # 24 DSPTEM2 +1 K
000616,000522: # 25 DSPTEM1 C
000617,000523: # 26 DSPTEM1 A
000618,000524: # 27 SMODE C
000619,000525: # 28 SPARE
000620,000526: # 29 SPARE
000621,000527: # 30 SPARE
000622,000528: # 31 SPARE
000623,000529: # 32 -TPER K
000624,000530: # 33 TIG K
000625,000531: # 34 DSPTEM1 K
000626,000532: # 35 TTOGO K
000627,000533: # 36 TIME2 K
000628,000534: # 37 TTPI K
000629,000535: # 38 TET K
000630,000536: # 39 SPARE
000631,000537:
|
|
Page 14
|
000633,000539: # REGISTERS AND SCALING FOR MIXED NOUNS
000634,000540:
000635,000541: # NOUN COMP REGISTER SCALE TYPE
000636,000542: # 40 1 TTOGO L
000637,000543: # 2 VGDISP S
000638,000544: # 3 DVTOTAL S
000639,000545: # 41 1 DSPTEM1 D
000640,000546: # 2 DSPTEM1 +1 E
000641,000547: # 42 1 HAPO Q
000642,000548: # 2 HPER Q
000643,000549: # 3 VGDISP S
000644,000550: # 43 1 LAT H
000645,000551: # 2 LONG H
000646,000552: # 3 ALT Q
000647,000553: # 44 1 HAPOX Q
000648,000554: # 2 HPERX Q
000649,000555: # 3 TFF L
000650,000556: # 45 1 TRKMKCNT C
000651,000557: # 2 TTOGO L
000652,000558: # 3 +MGA H
000653,000559: # 46 1 DAPDATR1 A
000654,000560: # 47 1 LEMMASS KK
000655,000561: # 2 CSMMASS KK
000656,000562: # 48 1 PITTIME NN
000657,000563: # 2 ROLLTIME NN
000658,000564: # 49 1 R22DISP Q
000659,000565: # 2 R22DISP +2 S
000660,000566: # 3 WHCHREAD C
000661,000567: # 50 SPARE
000662,000568: # 51 1 ALPHASB H
000663,000569: # 2 BETASB H
000664,000570: # 52 1 ACTCENT H
000665,000571: # 53 SPARE
000666,000572: # 54 1 RANGE JJ
000667,000573: # 2 RRATE S
000668,000574: # 3 RTHETA H
000669,000575: # 55 1 NN C
000670,000576: # 2 ELEV H
000671,000577: # 3 CENTANG H
000672,000578: # 56 1 RR-AZ H
000673,000579: # 2 RR-ELEV H
000674,000580: # 57 SPARE
000675,000581: # 58 1 POSTTPI Q
000676,000582: # 2 DELVTPI S
000677,000583: # 3 DELVTPF S
000678,000584: # 59 1 DVLOS S
000679,000585: # 2 DVLOS +2 S
000680,000586: # 3 DVLOS +4 S
000681,000587: # 60 1 FORVEL CC
|
|
Page 15
|
000683,000589: # 2 HDOTDISP S
000684,000590: # 3 HCALC1 RR
000685,000591: # 61 1 TTFDISP L
000686,000592: # 2 TTOGO L
000687,000593: # 3 OUTOFPLN QQ
000688,000594: # 62 1 ABVEL S
000689,000595: # 2 TTOGO L
000690,000596: # 3 DVTOTAL S
000691,000597: # 63 1 ABVEL S
000692,000598: # 2 HDOTDISP S
000693,000599: # 3 HCALC1 RR
000694,000600: # 64 1 FUNNYDSP PP
000695,000601: # 2 HDOTDISP S
000696,000602: # 3 HCALC RR
000697,000603: # 65 1 SAMPTIME K
000698,000604: # 2 SAMPTIME K
000699,000605: # 3 SAMPTIME K
000700,000606: # 66 1 RSTACK +6 W
000701,000607: # 2 CHANNEL 33 TT
000702,000608: # 67 1 RSTACK X
000703,000609: # 2 RSTACK +2 Y
000704,000610: # 3 RSTACK +4 Z
000705,000611: # 68 1 RANGEDSP QQ
000706,000612: # 2 TTFDISP L
000707,000613: # 3 DELTAH RR
000708,000614: # 69 1 DLANDZ RR
000709,000615: # 2 DLANDY RR
000710,000616: # 3 DLANDX RR
000711,000617: # 70 1 AOTCODE A
000712,000618: # 2 AOTCODE +1 A
000713,000619: # 3 AOTCODE +2 A
000714,000620: # 71 1 AOTCODE A
000715,000621: # 2 AOTCODE +1 A
000716,000622: # 3 AOTCODE +2 A
000717,000623: # 72 1 CDUT WW
000718,000624: # 2 CDUS D
000719,000625: # 73 1 TANG WW
000720,000626: # 2 TANG +1 D
000721,000627: # 74 1 TTOGO L
000722,000628: # 2 YAW H
000723,000629: # 3 PITCH H
000724,000630: # 75 1 DIFFALT Q
000725,000631: # 2 T1TOT2 L
000726,000632: # 3 T2TOT3 L
000727,000633: # 76 1 ZDOTD S
000728,000634: # 2 RDOTD S
000729,000635: # 3 XRANGE Q
000730,000636: # 77 1 TTOGO L
000731,000637: # 2 YDOT S
000732,000638: # 78 1 DNRRANGE U
|
|
Page 16
|
000734,000640: # 2 DNRRDOT V
000735,000641: # 3 TTOTIG L
000736,000642: # 79 1 CURSOR D
000737,000643: # 2 SPIRAL D
000738,000644: # 3 POSCODE C
000739,000645: # 80 1 DATAGOOD C
000740,000646: # 2 OMEGAD H
000741,000647: # 81 1 DELVLVC S
000742,000648: # 2 DELVLVC +2 S
000743,000649: # 3 DELVLVC +4 S
000744,000650: # 82 1 DELVLVC S
000745,000651: # 2 DELVLVC +2 S
000746,000652: # 3 DELVLVC +4 S
000747,000653: # 83 1 DELVIMU S
000748,000654: # 2 DELVIMU +2 S
000749,000655: # 3 DELVIMU +4 S
000750,000656: # 84 1 DELVOV S
000751,000657: # 2 DELVOV +2 S
000752,000658: # 3 DELVOV +4 S
000753,000659: # 85 1 VGBODY S
000754,000660: # 2 VGBODY +2 S
000755,000661: # 3 VGBODY +4 S
000756,000662: # 86 1 DELVLVC S
000757,000663: # 2 DELVLVC +2 S
000758,000664: # 3 DELVLVC +4 S
000759,000665: # 87 1 AZ D
000760,000666: # 2 EL D
000761,000667: # 88 1 STARAD B
000762,000668: # 2 STARAD +2 B
000763,000669: # 3 STARAD +4 B
000764,000670: # 89 1 LANDLAT G
000765,000671: # 2 LANDLONG G
000766,000672: # 3 LANDALT JJ
000767,000673: # 90 1 RANGE JJ
000768,000674: # 2 RRATE S
000769,000675: # 3 RTHETA H
000770,000676: # 91 1 P21ALT Q (MEMORY/100 TO DIPLAY TENS N.M.)
000771,000677: # 2 P21VEL P
000772,000678: # 3 P21GAM H
000773,000679: # 92 1 THRDISP C
000774,000680: # 2 HDOTDISP S
000775,000681: # 3 HCALC1 RR
000776,000682: # 93 1 OGC G
000777,000683: # 2 OGC +2 G
000778,000684: # 3 OGC +4 G
000779,000685: # 94 SPARE
000780,000686: # 95 SPARE
000781,000687: # 96 SPARE
000782,000688: # 97 1 DSPTEM1 C
000783,000689: # 2 DSPTEM1 +1 C
|
|
Page 17
|
000785,000691: # 3 DSPTEM1 +2 C
000786,000692: # 98 1 DSPTEM2 C
000787,000693: # 2 DSPTEM2 +1 B
000788,000694: # 3 DSPTEM2 +2 C
000789,000695: # 99 1 WWPOS XX
000790,000696: # 2 WWVEL YY
000791,000697: # 3 WWBIAS AAA
|
|
Page 18
|
000793,000699: # NOUN SCALES AND FORMATS
000794,000700:
000795,000701: # -SCALE TYPE- PRECISION
000796,000702: # UNITS DECIMAL FORMAT -- AGC FORMAT
000797,000703: # ------------ -------------- -- ----------
000798,000704:
000799,000705: # -A-
000800,000706: # OCTAL XXXXX SP OCTAL
000801,000707:
000802,000708: # -B- -14
000803,000709: # FRACTIONAL .XXXXX SP BIT 1 = 2 UNITS
000804,000710: # (MAX .99996)
000805,000711:
000806,000712: # -C-
000807,000713: # WHOLE XXXXX. SP BIT 1 = 1 UNIT
000808,000714: # (MAX 16383.)
000809,000715:
000810,000716: # -D- 15
000811,000717: # CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360/2 DEGREES
000812,000718: # (MAX 359.99) (USES 15 BITS FOR MAGNI-
000813,000719: # TUDE AND 2-S COMP.)
000814,000720:
000815,000721: # -E- 14
000816,000722: # ELEVATION DEGREES XX.XXX DEGREES SP BIT 1 = 90/2 DEGREES
000817,000723: # (MAX 89.999)
000818,000724:
000819,000725: # -F- 14
000820,000726: # DEGREES (180) XXX.XX DEGREES SP BIT 1 = 180/2 DEGREES
000821,000727: # (MAX 179.99)
000822,000728:
000823,000729: # -G-
000824,000730: # DP DEGREES (90) XX.XXX DEGREES DP BIT 1 OF LOW REGISTER =
000825,000731: # 28
000826,000732: # 360/2 DEGREES
000827,000733:
000828,000734: # -H-
000829,000735: # DP DEGREES (360) XXX.XX DEGREES DP BIT 1 OF LOW REGISTER =
000830,000736: # 28
000831,000737: # (MAX 359.99) 360/2 DEGREES
000832,000738:
|
|
Page 19
|
000834,000740: # -K-
000835,000741: # TIME (HR, MIN, SEC) 00XXX. HR DP BIT 1 OF LOW REGISTER =
000836,000742: # 000XX. MIN -2
000837,000743: # 0XX.XX SEC 10 SEC
000838,000744: # (DECIMAL ONLY.
000839,000745: # MAX MIN COMP=59
000840,000746: # MAX SEC COMP=59.99
000841,000747: # MAX CAPACITY=745 HRS
000842,000748: # 39 MINS
000843,000749: # 14.55 SECS.
000844,000750: # WHEN LOADING, ALL 3
000845,000751: # COMPONENTS MUST BE
000846,000752: # SUPPLIED.)
000847,000753:
000848,000754: # -L-
000849,000755: # TIME (MIN/SEC) XXBXX MIN/SEC DP BIT 1 OF LOW REGISTER =
000850,000756: # (B IS A BLANK -2
000851,000757: # POSITION, DECIMAL 10 SEC
000852,000758: # ONLY, DISPLAY OR
000853,000759: # MONITOR ONLY. CANNOT
000854,000760: # BE LOADED.
000855,000761: # MAX MIN COMP=59
000856,000762: # MAX SEC COMP=59
000857,000763: # VALUES GREATER THAN
000858,000764: # 59 MIN 59 SEC
000859,000765: # ARE DISPLAYED AS
000860,000766: # 59 MIN 59 SEC.)
000861,000767:
000862,000768: # -M- -2
000863,000769: # TIME (SEC) XXX.XX SEC SP BIT 1 = 10 SEC
000864,000770: # (MAX 163.83)
000865,000771:
000866,000772: # -N-
000867,000773: # TIME(SEC) DP XXX.XX SEC DP BIT 1 OF LOW REGISTER =
000868,000774: # -2
000869,000775: # 10 SEC
000870,000776:
000871,000777: # -P-
000872,000778: # VELOCITY 2 XXXXX. FEET/SEC DP BIT 1 OF HIGH REGISTER =
000873,000779: # (MAX 41994.) -7
000874,000780: # 2 METERS/CENTI-SEC
000875,000781:
000876,000782: # -Q-
000877,000783: # POSITION 4 XXXX.X NAUTICAL MILES DP BIT 1 OF LOW REGISTER =
000878,000784: # 2 METERS
000879,000785:
000880,000786: # -S-
000881,000787: # VELOCITY 3 XXXX.X FT/SEC DP BIT 1 OF HIGH REGISTER =
000882,000788: # -7
000883,000789: # 2 METERS/CENTI-SEC
000884,000790:
|
|
Page 20
|
000886,000792: # -T- -2
000887,000793: # G XXX.XX G SP BIT 1 = 10 G
000888,000794: # (MAX 163.83)
000889,000795:
000890,000796: # -U-
000891,000797: # RENDEZVOUS XXX.XX NAUT MI SP USES 15 BITS FOR UNSIGNED
000892,000798: # RADAR RANGE (DECIMAL ONLY. MAGNITUDE.
000893,000799: # DISPLAY OR MONITOR BIT 1 = 9.38 FEET
000894,000800: # ONLY. CANNOT BE
000895,000801: # LOADED.)
000896,000802:
000897,000803: # -V-
000898,000804: # RENDEZVOUS XXXXX. FEET/SEC SP USES 15 BITS FOR UNSIGNED
000899,000805: # RADAR RANGE RATE (DECIMAL ONLY. MAGNITUDE.
000900,000806: # DISPLAY OR MONITOR BIT 1 = -.6278 FEET/SEC
000901,000807: # ONLY. CANNOT BE
000902,000808: # LOADED.
000903,000809: # BIAS OF 17000 COUNTS
000904,000810: # SUBTRACTED BEFORE
000905,000811: # DISPLAY.)
000906,000812:
000907,000813: # -W-
000908,000814: # LANDING RADAR XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000909,000815: # ALTITUDE WORD = 1.079 FEET
000910,000816:
000911,000817: # -X-
000912,000818: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000913,000819: # VELX WORD = -.6440 FEET/SEC
000914,000820:
000915,000821: # -Y-
000916,000822: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000917,000823: # VELY WORD = 1.212 FEET/SEC
000918,000824:
000919,000825: # -Z-
000920,000826: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000921,000827: # VELZ WORD = .8668 FEET/SEC
000922,000828:
000923,000829: # -AA-
000924,000830: # INITIAL/FINAL XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000925,000831: # ALTITUDE WORD = 2.345 FEET
000926,000832:
000927,000833: # -BB-
000928,000834: # ALTITUDE RATE XXXXX. FEET/SEC SP LOW ORDER BIT = .5
000929,000835: # (MAX 08191.) FEET/SEC
000930,000836:
000931,000837: # -CC-
000932,000838: # FORWARD/LATERAL XXXX.X FEET/SEC SP LOW ORDER BIT = .5571
000933,000839: # VELOCITY (MAX 09126.) FEET/SEC
000934,000840:
000935,000841: # -DD-
|
|
Page 21
|
000937,000843: # ROTATIONAL HAND XXXXX. DEG/SEC SP FRACTIONAL PART OF PI RAD
000938,000844: # CONTROLLER ANGULAR (MAX 00044.) 4 SEC
000939,000845: # RATES
000940,000846:
000941,000847: # -EE-
000942,000848: # OPTICAL TRACKER XXX.XX DEG. DP LOW ORDER BIT OF LOW ORDER
000943,000849: # AZIMUTH ANGLE 15
000944,000850: # WORD = 360/2 DEGREES
000945,000851:
000946,000852: # -JJ-
000947,000853: # POSITION5 XXX.XX NAUT MI DP BIT 1 OF LOW REGISTER =
000948,000854: # 2 METERS
000949,000855:
000950,000856: # -KK- 16
000951,000857: # WEIGHT2 XXXXX. LBS SP FRACTIONAL PART OF 2 KG
000952,000858:
000953,000859: # -NN-
000954,000860: # TRIM DEGREES 2 XXX.XX DEG SP BIT 1=.01 SEC(TIME)
000955,000861: # (MAX 032.76)
000956,000862:
000957,000863: # -PP-
000958,000864: # 2 INTEGERS +XXBYY DP BIT 1 OF HIGH REGISTER =
000959,000865: # (B IS A BLANK 1 UNIT OF XX
000960,000866: # POSITION. DECIMAL BIT 1 OF LOW REGISTER =
000961,000867: # ONLY, DISPLAY OR 1 UNIT OF YY
000962,000868: # MONITOR ONLY. CANNOT (EACH REGISTER MUST
000963,000869: # BE LOADED.) CONTAIN A POSITIVE INTEGER
000964,000870: # (MAX 99B99) LESS THAN 100)
000965,000871:
000966,000872: # -QQ-
000967,000873: # POSITION7 XXXX.X NAUT MI DP BIT 1 OF LOW REGISTER =
000968,000874: # (MAX 9058.9) -4
000969,000875: # 2 METERS
000970,000876:
000971,000877: # -RR-
000972,000878: # COMPUTED ALTITUDE XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000973,000879: # -4
000974,000880: # 2 METERS
000975,000881:
000976,000882: # -SS-
000977,000883: # DP DEGREES XXXX.X DEGREES DP BIT 1 OF HIGH REGISTER =
000978,000884: # 1 DEGREE
000979,000885:
000980,000886: # -TT-
000981,000887: # LANDING RADAR +0000X CHANNEL 33, BIT 6 = NOT POSIT. 1
000982,000888: # POSITION (DECIMAL ONLY. CHANNEL 33, BIT 7 = NOT POSIT. 2
000983,000889: # DISPLAY OR MONITOR X = 1 FOR LR POSITION 1
000984,000890: # ONLY. CANNOT BE X = 2 FOR LR POSITION 2
000985,000891: # LOADED.)
000986,000892:
000987,000893: # -WW- 15
|
|
Page 22
|
000989,000895: # 360-CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360 - (360/2 )
000990,000896: # (MAX 359.99) DEGREES
000991,000897: # (USES 15 BITS FOR MAGNI-
000992,000898: # TUDE AND 2-S COMP.)
000993,000899:
000994,000900: # -XX-
000995,000901: # POSITION 9 XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000996,000902: # -9
000997,000903: # 2 METERS
000998,000904:
000999,000905: # -YY-
001000,000906: # VELOCITY 4 XXXX.X FEET/SEC DP FRACTIONAL PART OF
001001,000907: # (MAX 328.0) METERS/CENTI-SEC
001002,000908:
001003,000909: # -AAA-
001004,000910: # RADIANS XX.XXX RADIANS DP BIT 1 OF HIGH REGISTER =
001005,000911: # (MAX 31.999) -9
001006,000912: # 2 RADIANS
001007,000913:
001008,000914:
001009,000915: # THAT-S ALL ON THE NOUNS.
001010,000916:
|
|
Page 23
|
001012,000918: # ALARM CODES FOR LUMINARY
001013,000919:
001014,000920: # *9 *18 *60 COLUMN
001015,000921:
001016,000922: # CODE * TYPE SET BY
001017,000923:
001018,000924: # 00107 MORE THAN 5 MARK PAIRS AOTMARK
001019,000925: # 00111 MARK MISSING AOTMARK
001020,000926: # 00112 MARK OR MARK REJECT NOT BEING ACCEPTED AOTMARK
001021,000927: # 00113 NO INBITS AOTMARK
001022,000928: # 00114 MARK MADE BUT NOT DESIRED AOTMARK
001023,000929: # 00115 NO MARKS IN LAST PAIR TO REJECT AOTMARK
001024,000930: # 00206 ZERO ENCODE NOT ALLOWED WITH COARSE ALIGN IMU MODE SWITCHING
001025,000931: # 00206 + GIMBAL LOCK.
001026,000932: # 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT
001027,000933: # 00210 IMU NOT OPERATING IMU MODE SWITCH, IMU-2, R02, P51, P57
001028,000934: # 00211 COARSE ALIGN ERROR IMU MODE SWITCH
001029,000935: # 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH, T4RPT
001030,000936: # 00213 IMU NOT OPERATING WITH TURN-ON REQUEST T4RUPT
001031,000937: # 00214 PROGRAM USING IMU WHEN TURNED OFF T4RUPT
001032,000938: # 00217 BAD RETURN FROM IMUSTALL P51, P52, P57
001033,000939: # 00220 IMU NOT ALIGNED - NO REFSMMAT R02, R47
001034,000940: # 00401 DESIRED GIMBAL ANGLE YIELDS GIMBAL LOCK INF ALIGN, IMU-2,
001035,000941: # FINDCDUW
001036,000942: # 00402 FINDCDUW NOT CONTROLLING ATTITUDE FINDCDUW
001037,000943: # 00404 TWO STARS NOT AVAILABLE IN ANY DETENT R59, LUNAR SURFACE
001038,000944: # 00405 TWO STARS NOT AVAILABLE P52
001039,000945: # 00421 W-MATRIX OVERFLOW INTEGRV
001040,000946: # 00501 P RADAR ANTENNA OUT OF LIMITS R23
001041,000947: # 00502 BAD RADAR GIMBAL ANGLE INPUT V41N72
001042,000948: # 00503 P RADAR ANTENNA DESIGNATE FAIL R21, NON-P IN V41N72
001043,000949: # 00510 RADAR AUTO DESCRETE NOT PRESENT R25
001044,000950: # 00511 L4 NOT IN POSITION 2 OR REPOSITIONING SERVICER
001045,000951: # 00514 P RR GOES OUT OF AUTO MODE WHILE IN USE P20
001046,000952: # 00515 RR CDU FAIL DISCRETE PRESENT R25
001047,000953: # 00520 RADAR RUPT NOT EXPECTED AT THIS TIME RADAR READ
001048,000954: # 00521 COULD NOT READ RADAR P20
001049,000955: # 00522 LANDING RADAR POSITION CHANGE RADAR READ
001050,000956: # 00523 P LR ANTENNA DIDN'T ACHIEVE POSITION 2 SERVICER, V60 (NON-P IN V60)
001051,000957: # 00525 P DELTA THETA GREATER THAN 3 DEGREES R22
001052,000958: # 00526 P RANGE GREATER THAN 400 NAUT. MILES P20, P22
001053,000959: # 00527 P LOS NOT IN MODE II COVERAGE WHILE ON R21, R24
001054,000960: # LUNAR SURFACE
001055,000961: # OR VEHICLE MANEUVER REQUIRED R24 (20)
001056,000962: # 00530 P LOS NOT IN MODE2 COVERAGE R21
001057,000963: # ON LUNAR SURFACE AFTER 600 SECS.
001058,000964: # 00600 IMAGINARY ROOTS ON FIRST ITERATION P32, P72
001059,000965: # 00601 PERIGEE ALTITUDE CSI LT PMIN1 P32, P72,
001060,000966: # 00602 PERIGEE ALTITUDE CDH LT PMIN2 P32, P72,
001061,000967: # 00603 CSI TO CDH TIME LT TMIN12 P32, P72, P33, P73
|
|
Page 24
|
001063,000969: # 00604 CDH TO TPI TIME LT TMIN23 P32, P72,
001064,000970: # OR COMPUTED CDH TIME GREATER THAN INPUT TP1 TIME
001065,000971: # 00605 NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM P32, P72
001066,000972: # 00606 DV EXCEEDS MAXIMUM P32, P72,
001067,000973: # 00611 NO TIG FOR GIVEN ELEV ANGLE P34, P74
001068,000974: # 00701 ILLEGAL OPTION CODE SELECTED P57
001069,000975: # 00777 PIPA FAIL CAUSED THE ISS WARNING T4RUPT
001070,000976: # 01102 AGC SELF TEST ERROR SELF CHECK
001071,000977: # 01105 DOWNLINK TOO FAST T4RUPT
001072,000978: # 01106 UPLINK TOO FAST T4RUPT
001073,000979: # 01107 PHASE TABLE FAILURE. ASSUME RESTART
001074,000980: # ERASABLE MEMORY IS SUSPECT. RESTART
001075,000981: # 01301 ARCSIN-ARCCOS ARGUMENT TOO LARGE INTERPRETER
001076,000982: # 01406 BAD RETURN FROM ROOTPSRS DESCENT GUIDANCE EQS.
001077,000983: # 01407 VG INCREASING (DELTA-V ACCUMULATED S40.8
001078,000984: # .GT. 90 DEGREES AWAY FROM DESIRED THRUST S40.8
001079,000985: # VECTOR.) S40.8
001080,000986: # 01410 UNINTENTIONAL OVERFLOW IN GUIDANCE DESCENT GUIDANCE EQS.
001081,000987: # 01412 DESCENT IGNALG NOT CONVERGING P63
001082,000988: # 01520 V37 REQUEST NOT PERMITTED AT THIS TIME V37
001083,000989: # 01600 OVERFLOW IN DRIFT TEST IMU 4
001084,000990: # 01601 BAD IMU TORQUE OPT PRE ALIGN CALIB
001085,000991: # 01601 IMU 4 (LEM)
001086,000992: # 01703 IGNITION TIME SLIPPED MIDTOAVE
001087,000993: # 01706 INCORRECT PROGRAM REQUESTED FOR VEHICLE
001088,000994: # CONFIGURATION P40, P42
001089,000995: # 02001 JET FAILURES HAVE DISABLED Y-Z TRANS. DAP
001090,000996: # 02002 JET FAILURES HAVE DISABLED X TRANSLATION DAP
001091,000997: # 02003 JET FAILURES HAVE DISABLED P-ROTATION DAP
001092,000998: # 02004 JET FAILURES HAVE DISABLED U-V ROTATION DAP
001093,000999: # 03777 ICDU FAIL CAUSED THE ISS WARNING T4RUPT
001094,001000: # 04777 ICDU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001095,001001: # 07777 IMU FAIL CAUSED THE ISS WARNING T4RUPT
001096,001002: # 10777 IMU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001097,001003: # 13777 IMU, ICDU FAILS CAUSED THE ISS WARNING T4RUPT
001098,001004: # 14777 IMU, ICDU, PIPA FAILS CAUSED ISS WARNING T4RUPT
001099,001005:
001100,001006: # THE FOLLOWING CODES INDICATE THE MORE SERIOUS POODOO ABORTS THAT RESULT
001101,001007: # IN THE PROGRAM GOING TO ROO.
001102,001008:
001103,001009: # 20105 AOTMARK SYSTEM IN USE AOTMARK
001104,001010: # 20430 ACCELERATION OVERFLOW IN INTEGRATION ORBITAL INTEGRATION
001105,001011: # 20607 NO SOLN FROM TIME-THETA OR TIME-RADIUS TIMETHET, TIMERAD
001106,001012: # 21103 UNUSED CCS BRANCH EXECUTED ABORT
001107,001013: # 21204 WAITLIST, VARDELAY, FIXDELAY, OR LONGCALL WAITLIST ROUTINES
001108,001014: # CALLED WITH ZERO OR NEGATIVE DELTA-TIME
001109,001015: # 21302 SQRT CALLED WITH NEGATIVE ARGUMENT INTERPRETER
001110,001016: # 21406 BAD RETURN FROM ROOTPSRS IGNITION ALGORITHMN
001111,001017: # 21501 KEYBOARD AND DISPLAY ALARM DURING PINBALL
001112,001018: # INTERNAL USE(NVSUB).ABORT
001113,001019:
|
|
Page 25
|
001115,001021: # THE FOLLOWING CODES INDICATE A BAILOUT ABORT THAT RESULTS IN A SOFTWARE
001116,001022: # RESTART
001117,001023:
001118,001024: # 31104 DELAY ROUTINE BUSY EXEC
001119,001025: # 31201 EXECUTIVE OVERFLOW-NO VAC AREAS EXEC
001120,001026: # 31202 EXECUTIVE OVERFLOW-NO CORE SETS EXEC
001121,001027: # 31203 WAITLIST OVERFLOW-TOO MANY TASKS WAITLIST
001122,001028: # 31206 SECOND JOB ATTEMPTS TO GO TO SLEEP VIA PINBALL
001123,001029: # KEYBOARD AND DISPLAY PROGRAM
001124,001030: # 31207 NO VAC AREAS FOR MARKS AOTMARK
001125,001031: # 31210 TWO PROGRAMS USING DEVICE AT SAME TIME MODE SWITCHING
001126,001032: # 31211 ILLEGAL INTERRUPT OF EXTENDED VERB AOTMARK
001127,001033: # 31502 TWO PRIO DISPLAYS WAITING DSP INTRFCE
001128,001034: # 32000 DAP STILL IN PROGRESS AT NEXT TIME5 RUPT DAP
001129,001035:
|
|
Page 26
|
001131,001037: # CHECKLIST CODES FOR LUMINARY
001132,001038:
001133,001039: # *9 *17 *26 *9 COLUMN
001134,001040:
001135,001041: # R1CODE ACTION TO BE EFFECTED PROGRAM
001136,001042:
001137,001043: # 00013 KEY IN NORMAL OR GYRO TORQUE COARSE ALIGN P52
001138,001044: # 00014 PROCEED DO IMU FINE ALIGN ROUTINE P51, P63, P57
001139,001045: # 00014 ENTER DO LANDING SITE DETERMINATION(N89DISP) P57OPTION2
001140,001046: # 00015 PERFORM CELESTIAL BODY ACQUISITION R51, P51
001141,001047: # 00062 SWITCH AGC POWER DOWN P06
001142,001048: # 00201 SWITCH RR MODE TO AUTOMATIC P20, P22, R04
001143,001049: # 00203 SWITCH GUID CONTROL TO GNC, MODE TO AUTO... P12, P42, P71
001144,001050: # ALSO THR CONT TO AUTO P40, P63, P70
001145,001051: # 00205 PERFORM MANUAL ACQUISITION OF RR R23
001146,001052: # 00500 SWITCH LR ANTENNA TO POSITION 1 P63
001147,001053:
001148,001054: # SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
001149,001055: # PERFORM DENOTES START OR END OF A TASK
001150,001056: # KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
001151,001057:
|
|
Page 27
|
001153,001059: # OPTION CODES FOR LUMINARY
001154,001060:
001155,001061: # THE SPECIFIED OPTION CODES WILL BE FLASHED IN COMPONENT R1 IN
001156,001062: # CONJUNCTION WITH V04N06 OR V04N12 (FOR EXTENDED VERBS) TO REQUEST THE
001157,001063: # ASTRONAUT TO LOAD INTO COMPONENT R2 THE OPTION HE DESIRES.
001158,001064:
001159,001065: # *9 *17 *52 *11 *25 COLUMN
001160,001066:
001161,001067: # OPTION
001162,001068: # CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
001163,001069:
001164,001070: # 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P52 ALL
001165,001071: # 4=LAND SITE
001166,001072: # 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
001167,001073: # 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
001168,001074: # 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
001169,001075: # 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
001170,001076: # 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
001171,001077: # 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
001172,001078: # 2=TWO BODIES 3=ONE BODY + G
001173,001079: # 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
001174,001080: # ORBIT TO PASS OVER LM
001175,001081:
End of include-file ASSEMBLY_AND_OPERATION_INFORMATION.agc. Parent file is MAIN.agc