GAP: ASSEMBLE REVISION 069 OF AGC PROGRAM LUMINARY BY NASA 2021112-011 19:02 NOV. 25,1968Note that the date is the date of the printout, not the date of the program revision.
Source Code
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These source-code files were transcribed from scans made from Don Eyles's personal
copy of Luminary 069. They were scanned at archive.org's Boston
facility, and the scanning was sponsored by Onno Hommes. The code was transcribed
from these scans by a team of volunteers who are referenced in the program
comments. Comments from the original source code are prefixed with a single '#' symbol,
whereas comments added later are prefixed by "##" or "###". In some cases, where
similar code blocks exist in previously-transcribed AGC programs (primarily
Luminary 99, from Apollo 11) those code blocks were used as a starting point and
then corrected to agree with the Luminary 69 scans. The full scans are available
at the Virtual AGC
project's collection at archive.org, while more-convenient reduced-size (but reduced-quality)
images are available at
the main Virtual AGC website. Report any errors noted by creating an
issue report at the Virtual AGC
project's GitHub repository. Notations on the program listing read, in part:GAP: ASSEMBLE REVISION 069 OF AGC PROGRAM LUMINARY BY NASA 2021112-011 19:02 NOV. 25,1968Note that the date is the date of the printout, not the date of the program revision. |
051954,000002: ## Copyright: Public domain.
051955,000003: ## Filename: INTEGRATION_INITIALIZATION.agc
051956,000004: ## Purpose: The main source file for Luminary revision 069.
051957,000005: ## It is part of the source code for the original release
051958,000006: ## of the flight software for the Lunar Module's (LM) Apollo
051959,000007: ## Guidance Computer (AGC) for Apollo 10. The actual flown
051960,000008: ## version was Luminary 69 revision 2, which included a
051961,000009: ## newer lunar gravity model and only affected module 2.
051962,000010: ## This file is intended to be a faithful transcription, except
051963,000011: ## that the code format has been changed to conform to the
051964,000012: ## requirements of the yaYUL assembler rather than the
051965,000013: ## original YUL assembler.
051966,000014: ## Reference: pp. 1200-1222
051967,000015: ## Assembler: yaYUL
051968,000016: ## Contact: Ron Burkey <info@sandroid.org>.
051969,000017: ## Website: www.ibiblio.org/apollo/index.html
051970,000018: ## Mod history: 2016-12-13 MAS Created from Luminary 99.
051971,000019: ## 2016-12-18 MAS Updated from comment-proofed Luminary 99 version.
051972,000020: ## 2017-01-22 MAS Updated for Luminary 69.
051973,000021: ## 2017-01-22 HG Add missing label ALLSTALL
051974,000022: ## Add missing operation INDEX L
051975,000023: ## Fix interpretive operator BOF -> BOFCLR
051976,000024: ## 2017-01-28 RSB Proofed comment text using octopus/prooferComments
051977,000025: ## but no errors found.
051978,000026: ## 2017-03-13 RSB Comment-text fixes noted in proofing Luminary 116.
051979,000027: ## 2017-03-15 RSB Comment-text fixes identified in 5-way
051980,000028: ## side-by-side diff of Luminary 69/99/116/131/210.
051981,000029: ## 2017-08-19 MAS Fixed comment errors found transcribing Zerlina 56.
051982,000030:
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Page 1200 |
051984,000032: # 1.0 INTRODUCTION
051985,000033: # ----------------
051986,000034:
051987,000035: # FROM A USERS POINT OF VIEW, ORBITAL INTEGRATION IS ESSENTIALLY THE SAME AS THE 278 INTEGRATION
051988,000036: # PROGRAM. THE SAME ENTRANCES TO THE PROGRAM WILL BE MAINTAINED, THE SAME STALLING ROUTINE WILL BE USED AND
051989,000037: # OUTPUT WILL STILL BE VIA THE PUSHLIST. THE PRIMARY DIFFERENCES TO A USER INVOLVE THE ADDED CAPABILITY OF
051990,000038: # TERMINATING INTEGRATION AT A SPECIFIC FINAL RADIUS AND THE DIFFERENCE IN STATE VECTOR SCALING INSIDE AND OUT-
051991,000039: # SIDE THE LUNAR SPHERE OF INFLUENCE.
051992,000040:
051993,000041: # IN ORDER TO MAKE THE CSM(LEM)PREC AND CSM(LEM)CONIC ENTRANCES SIMILAR TO FLIGHT 278, THE INTEGRATION PROGRAM
051994,000042: # WILL ITSELF SET THE FINAL RADIUS (RFINAL) TO 0 SO THAT REACHING THE DESIRED TIME ONLY WILL TERMINATE
051995,000043: # INTEGRATION. THE DP REGISTER RFINAL MUST BE SET BY USERS OF INTEGRVS AND INTEGRV, AND MUST BE DONE AFTER THE
051996,000044: # CALL TC INTSTALL.
051997,000045:
051998,000046: # WHEN THE LM IS ON THE LUNAR SURFACE (INDICATED BY LUNAR SURFACE FLAG SET) CALLS TO LEMCONIC, LEMPREC, AND
051999,000047: # INTEGRV WITH VINFLAG = 0 WILL RESULT IN THE USE OF THE PLANETARY INERTIAL ORIENTATION SUBROUTINES TO PROVIDE
052000,000048: # BOTH THE LMS POSITION AND VELOCITY IN THE REFERENCE COORDINATE SYSTEM.
052001,000049: # THE PROGRAM WILL PROVIDE OUTPUT AS IF INTEGRATION WAS USED. THAT IS, THE PUSHLIST WILL BE SET AS NOTED BELOW AND
052002,000050: # THE PERMANENT STATE VECTOR UPDATED WHEN SPECIFIED BY AN INTEGRV CALL.
052003,000051:
052004,000052: # USERS OF INTEGRVS DESIRING INTEGRATION (INTYPFLG = 0) SHOULD NOTE THAT THE OBLATENESS PERTURBATION COMPUTATION
052005,000053: # IN LUNAR ORBIT IS TIME DEPENDENT. THEREFORE, THE USER SHOULD SUPPLY AN INITIAL STATE VECTOR VALID AT SOME REAL
052006,000054: # TIME AND THE DESIRED TIME (TDEC1) ALSO AT SOME REAL TIME. FOR CONIC ,,INTEGRATION,, THE USER MAY STILL USE ZERO
052007,000055: # AS THE INITIAL TIME AND DELTA TIME AS THE DESIRED TIME.
052008,000056:
052009,000057: # 2.0 GENERAL DESCRIPTION
052010,000058: # -----------------------
052011,000059:
052012,000060: # THE INTEGRATION PROGRAM OPERATES AS A CLOSED INTERPRETIVE SUBROUTINE AND PERFORMS THESE FUNCTIONS---
052013,000061: # 1) INTEGRATES (PRECISION OR CONIC) EITHER CSM OR LM STATE VECTOR
052014,000062: # 2) INTEGRATES THE W-MATRIX
052015,000063: # 3) PERMANENT OR TEMPORARY UPDATE OF THE STATE VECTOR
052016,000064:
052017,000065: # THERE ARE SIX ENTRANCES TO THE INTEGRATION PROGRAM. FOUR OF THESE (CSMPREC, LEMPREC, CSMCONIC, LEMCONIC) SET
052018,000066: # ALL THE FLAGS REQUIRED IN THE INTEGRATION PROGRAM ITSELF TO CAUSE THE PRECISION OR CONIC INTEGRATION (KEPLER) OF
052019,000067: # THE LM OR CSM STATE VECTOR, AS THE NAMES SUGGEST. ONE ENTRANCE (INTEGRVS) PERMITS THE CALLING PROGRAM TO
052020,000068: # PROVIDE A STATE VECTOR TO BE INTEGRATED. THE CALLING PROGRAM MUST SET THE FLAGS INDICATING (1) PRECISION OR
052021,000069: # CONIC INTEGRATION, (2) IN OR OUT OF LUNAR SPHERE, (3) MIDCOURSE OR NOT, AND THE INTEGRATION PROGRAM COMPLETES
052022,000070: # THE FLAG SETTING TO BYPASS W-MATRIX INTEGRATION. THE LAST ENTRANCE (INTEGRV, USED IN GENERAL BY THE
052023,000071: # NAVIGATION PROGRAMS) PERMITS THE CALLER TO SET FIVE FLAGS (NOT MOONFLAG OR MIDFLAG) BUT NOT TO INPUT A STATE
052024,000072: # VECTOR. ANY PROGRAM WHICH CALLS INTEGRVS OR INTEGRV MUST CALL INTSTALL BEFORE IT SETS THE INTEGRATION FLAGS
052025,000073: # AND/OR STATE VECTOR.
052026,000074:
052027,000075: # THREE SETS OF 42 REGISTERS AND 2 FLAGS ARE USED FOR THE STATE VECTORS. TWO SETS, WHICH MAY NOT BE OVERLAYED, ARE
052028,000076: # USED FOR THE PERMANENT STATE VECTORS FOR THE CSM AND LM. THE THIRD SET, WHICH MAY BE OVERLAYED WHEN INTEGRATION
052029,000077: # IS NOT BEING DONE, IS USED IN THE COMPUTATIONS.
052030,000078:
052031,000079: # THE PERMANENT STATE VECTORS WILL BE PERIODICALLY UPDATED SO THAT THE VECTORS WILL NOT BE OLDER THAN 4 TIMESTEPS.
052032,000080: # THE PERMANENT STATE VECTORS WILL ALSO BE UPDATED WHENEVER THE W-MATRIX IS INTEGRATED OR WHEN A CALLER OF INTEGRV
052033,000081: # SETS STATEFLG (THE NAVIGATION PROGRAMS P20, P22.)
052034,000082:
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Page 1201 |
052036,000084: # APPENDIX B OF THE USERS GUIDE LISTS THE STATE VECTOR QUANTITIES.
052037,000085:
052038,000086: # 2.1 RESTARTS
052039,000087:
052040,000088: # PHASE CHANGES WILL BE MADE IN THE INTEGRATION PROGRAM ONLY FOR THE INTEGRV ENTRANCE (I.E., WHEN THE W-MATRIX IS
052041,000089: # INTEGRATED OR PERMANENT STATE VECTOR IS UPDATED.) THE GROUP NUMBER USED WILL BE THAT FOR THE P20-25 PROGRAMS
052042,000090: # (I.E., GROUP2) SINCE THE INTEGRV ENTRANCE WILL ONLY BE USED BY THESE PROGRAMS. IF A RESTART OCCURS DURING AN
052043,000091: # INTEGRATION OF THE STATE VECTOR ONLY, THE RECOVERY WILL BE TO THE LAST PHASE IN THE CALLING PROGRAM. CALLING
052044,000092: # PROGRAMS WHICH USE THE INTEGRV OR INTEGRVS ENTRANCE OF INTEGRATION SHOULD ENSURE THAT IF PHASE CHANGING IS DONE
052045,000093: # THAT IT IS PRIOR TO SETTING THE INTEGRATION INPUTS IN THE PUSHLIST.
052046,000094: # THIS IS BECAUSE THE PUSHLIST IS LOST DURING A RESTART.
052047,000095:
052048,000096: # 2.2 SCALING
052049,000097:
052050,000098: # THE INTEGRATION ROUTINE WILL MAINTAIN THE PERMANENT MEMORY STATE VECTORS IN THE SCALING AND UNITS DEFINED IN
052051,000099: # APPENDIX B OF THE USERS GUIDE. THE SCALING OF THE OUTPUT POSITION VECTORDEPENDS ON THE ORIGIN OF THE COORDINATE
052052,000100: # SYSTEM AT THE DESIRED INTEGRATION TIME. THE COORDINATE SYSTEM TRANSFORMATION WILL BE DONE AUTOMATICALLY ON
052053,000101: # MULTIPLE TIMESTEP ENCKE INTEGRATION ONLY. THUS IT IS POSSIBLE TO HAVE OUTPUT FROM SUCCESSIVE INTEGRATIONS IN
052054,000102: # DIFFERENT SCALING.
052055,000103: # HOWEVER, RATT, VATT WILL ALWAYS BE SCALED THE SAME.
052056,000104:
052057,000105: # 3.0 INPUT/OUTPUT
052058,000106: # ----------------
052059,000107:
052060,000108: # PROGRAM INPUTS ARE THE FLAGS DESCRIBED IN APPENDIX A AND THE PERMANENT STATE VECTOR QUANTITIES DESCRIBED IN AP-
052061,000109: # PENDIX B OF THE USERS GUIDE, PLUS THE DESIRED TIME TO INTEGRATE TO IN TDEC1 (A PUSH LIST LOCATION).
052062,000110: # FOR INTEGRVS, THE RCV,VCV, TET OF THE TEMPORARY STATE VECTOR MUST BE SET, PLUS MOONFLAG AND MIDFLAG
052063,000111:
052064,000112: # FOR SIMULATION THE FOLLOWING QUANTITIES MUST BE PRESET ---
052065,000113: # EARTH MOON
052066,000114: # 29 27
052067,000115: # RRECTCSM(LEM) - RECTIFIED POSITION VECTOR METERS 2 2
052068,000116:
052069,000117: # 7 5
052070,000118: # VRECTCSM(LEM) - RECTIFIED VELOCITY VECTOR M/CSEC 2 2
052071,000119:
052072,000120: # 28 28
052073,000121: # TETCSM(LEM) - TIME STATE VECTOR IS VALID CSEC 2 2
052074,000122: # CUSTOMARILY 0, BUT NOTE LUNAR
052075,000123: # ORBIT DEPENDENCE ON REAL TIME.
052076,000124:
052077,000125: # 22 18
052078,000126: # DELTAVCSM(LEM) - POSITION DEVIATION METERS 2 2
052079,000127: # 0 IF TCCSM(LEM) = 0
052080,000128:
052081,000129: # 3 -1
052082,000130: # NUVCSM(LEM) - VELOCITY DEVIATION M/CSEC 2 2
052083,000131: # 0 IF TCCSM(LEM) = 0
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Page 1202 |
052085,000133: # 29 27
052086,000134: # RCVCSM(LEM) - CONIC POSITION METERS 2 2
052087,000135: # EQUALS RRECTCSM(LEM) IF
052088,000136: # TCCSM(LEM) = 0
052089,000137:
052090,000138: # 7 5
052091,000139: # VCVCSM(LEM) - CONIC VELOCITY M/CSEC 2 2
052092,000140: # EQUALS VRECTCSM(LEM) IF
052093,000141: # TCCSM(LEM) = 0
052094,000142:
052095,000143: # 28 28
052096,000144: # TCCSM(LEM) - TIME SINCE RECTIFICATION CSECS 2 2
052097,000145: # CUSTOMARILY 0
052098,000146:
052099,000147: # 1/2 17 16
052100,000148: # XKEPCSM(LEM) - ROOT OF KEPLERS EQUATION M 2 2
052101,000149: # 0 IF TCCSM(LEM) = 0
052102,000150:
052103,000151: # CMOONFLG - PERMANENT FLAGS CORRESPONDING 0 0
052104,000152: # CMIDFLAG TO MOONFLAG AND MIDFLAG 0,1 0,1
052105,000153: # LMOONFLG C = CSM, L = LM 0 0
052106,000154: # LMIDFLG 0,1 0,1
052107,000155:
052108,000156: # SURFFLAG - LUNAR SURFACE FLAG 0,1 0,1
052109,000157:
052110,000158: # IN ADDITION, IF (L)CMIDFLAG IS SET, THE INITIAL INPUT VALUES FOR LUNAR
052111,000159: # SOLAR EPHEMERIDES SUBROUTINE AND PLANETARY INERTIAL ORIENTATION SUB-
052112,000160: # ROUTINE MUST BE PRESET.
052113,000161:
052114,000162: # OUTPUT
052115,000163: # AFTER EVERY CALL TO INTEGRATION
052116,000164: # EARTH MOON
052117,000165: # 29 29
052118,000166: # 0D RATT POSITION METERS 2 2
052119,000167: # 7 7
052120,000168: # 6D VATT VELOCITY M/CSEC 2 2
052121,000169: # 28 28
052122,000170: # 12D TAT TIME 2 2
052123,000171: # 29 27
052124,000172: # 14D RATT1 POSITION METERS 2 2
052125,000173: # 7 5
052126,000174: # 20D VATT1 VELOCITY M/CSEC 2 2
052127,000175: # 3 2 36 30
052128,000176: # 26D MU(P) MU M /CS 2 2
052129,000177:
052130,000178: # X1 MUTABLE ENTRY -2 -10D
052131,000179:
052132,000180: # X2 COORDINT
052133,000181: # X2 COORDINATE SYSTEM ORIGEN 0 2
052134,000182: # (THIS, NOT MOONFLAG, SHOULD BE
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Page 1203 |
052136,000184: # USED TO DETERMINE ORIGIN.)
052137,000185:
052138,000186: # IN ADDITION TO THE ABOVE, THE PERMANENT STATE VECTOR IS UPDATED WHENEVER
052139,000187: # STATEFLG WAS SET AND WHENEVER A W-MATRIX IS TO BE INTEGRATED. THE PUSH
052140,000188: # COUNTER IS SET TO 0 AND OVERFLOW IS CLEARED BEFORE RETURNING TO THE
052141,000189: # CALLING PROGRAM.
052142,000190:
052143,000191: # 4.0 CALLING SEQUENCES AND SAMPLE CODE
052144,000192: # -------------------------------------
052145,000193:
052146,000194: # A) PRECISION ORBITAL INTEGRATION. CSMPREC,LEMPREC ENTRANCES
052147,000195: # L-X STORE TIME TO 95T5791T5 T 95 PUS L9ST (T4531)
052148,000196: # L CALL
052149,000197: # L+1 CSMPREC (OR LEMPREC)
052150,000198: # L+2 RETURN
052151,000199: # INPUT 28
052152,000200: # TDEC1 (PD 32D) TIME TO INTEGRATE TO...CENTISECONDS SCALED 2
052153,000201: # OUTPUT
052154,000202: # THE DATA LISTED IN SECTION 3.0 PLUS
052155,000203: # RQVV POSITION VECTOR OF VEHICLE WITH RESPECT TO SECONDARY
052156,000204: # BODY... METERS B-29 ONLY IF MIDFLAG = DIMOFLAG = 1
052157,000205: # B) CONIC INTEGRATION. CSMCONIC, LEMCONIC ENTRANCES
052158,000206: # L-X STORE TIME IN PUSH LIST (TDEC1)
052159,000207: # L CALL
052160,000208: # L+1 CSMCONIC (OR LEMCONIC)
052161,000209: # INPUT/OUTPUT
052162,000210: # SAME AS PRECISION INTEGRATION, EXCEPT RQVV NOT SET
052163,000211: # C) INTEGRATE GIVEN STATE VECTOR. INTEGRVS ENTRANCE
052164,000212: # CALL
052165,000213: # INTSTALL
052166,000214: # VLOAD
052167,000215: # POSITION VECTOR
052168,000216: # STOVL RCV
052169,000217: # VELOCITY VECTOR
052170,000218: # STODL VCV
052171,000219: # TIME STATE VECTOR VALID
052172,000220: # STODL TET
052173,000221: # FINAL RADIUS
052174,000222: # STORE RFINAL
052175,000223: # SET(CLEAR) SET(CLEAR)
052176,000224: # INTYPFLAG
052177,000225: # MOONFLAG
052178,000226: # SET(CLEAR) DLOAD
052179,000227: # DESIRED TIME
052180,000228: # STCALL TDEC1
052181,000229: # INTEGRVS
052182,000230: # INPUT
052183,000231: # RCV POSITION VECTOR METERS
052184,000232: # VCV VELOCITY VECTOR M/CSEC
052185,000233: # TET TIME OF STATE VECTOR(MAY = 0) CSEC B-28
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Page 1204 |
052187,000235: # TDEC1 TIME TO INTEGRATE TO CSEC B-28 (PD 32D)
052188,000236: # (MAY BE INCREMENT IF TET=0)
052189,000237: # OUTPUT
052190,000238: # SAME AS FOR PRECISION OR CONIC INTEGRATION,
052191,000239: # DEPENDING ON INTYPFLG.
052192,000240: # D) INTEGRATE STATE VECTOR.INTGRV ENTRANCE
052193,000241: # L-X STORE TIME IN PUSH LIST (TDEC1) (MAY BE DONE AFTER CALL TO INTSTALL)
052194,000242: # L-8 CALL
052195,000243: # L-7
052196,000244: # L-6 SET(CLEAR) SET(CLEAR)
052197,000245: # L-5 VINTFLAG 1=CSM, 0=LM
052198,000246: # L-4 INTYPFLAG 1=CONIC, 0=PRECISION
052199,000247: # L-3 SET(CLEAR) SET(CLEAR)
052200,000248: # L-2 DIMOFLAG 1=W-MATRIX, 0=NO W-MATRIX
052201,000249: # L-1 D6OR9FLG 1=9X9, 0=6X6
052202,000250: # L SET DLOAD
052203,000251: # L+1 STATEFLG DESIRE PERMANENT UPDATE
052204,000252: # L+2 FINAL RAD. OF STATE VECTOR
052205,000253: # L+3 STCALL RFINAL
052206,000254: # L+4 INTEGRV
052207,000255: # L CALL NORMAL USE-- WILL UPDATE STATE
052208,000256: # L+1 INTEGRV VECTOR IF DIMOFLAG=1.(STATEFLG IS
052209,000257: # L+2 RETURN ALWAYS RESET IN INTEGRATION AFTER
052210,000258: # IT IS USED.)
052211,000259: # INPUT
052212,000260: # TDEC1 (PD 32D) TIME TO INTEGRATE TO CSEC B-28
052213,000261: # OUTPUT
052214,000262: # SAME AS FOR PRECISION OR CONIC INTEGRATION
052215,000263: # THE PROGRAM WILL SET MOONFLAG, MIDFLAG DEPENDING ON
052216,000264: # THE PERMANENT STATE VECTOR REPRESENTATION.
052217,000265:
052218,000266: 11,2311 BANK 11
052219,000267: 13,2000 SETLOC INTINIT
052220,000268: 13,2000 BANK
052221,000269: 13,2604 E3,1554 EBANK= RRECTCSM
052222,000270: 13,2604 COUNT* $$/INTIN
052223,000271: 13,2604 05353 STATEINT TC PHASCHNG
052224,000272: 13,2605 00052 OCT 00052
052225,000273: 13,2606 35017 CAF PRIO5
052226,000274: 13,2607 05105 TC FINDVAC
052227,000275: 13,2610 E3,1554 EBANK= RRECTCSM
052228,000276: 13,2610 02613 26063 2CADR STATINT1
052229,000277:
052230,000278: 13,2612 05261 TC TASKOVER
052231,000279: 13,2613 06036 STATINT1 TC INTPRET
052232,000280: 13,2614 47014 BON RTB
052233,000281: 13,2615 04712 QUITFLAG # KILL INTEGRATION UNTIL NEXT POO.
052234,000282: 13,2616 26653 NOINT
052235,000283: 13,2617 21462 LOADTIME
052236,000284: 13,2620 00041 STORE TDEC1
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Page 1205 |
052238,000286: 13,2621 77624 CALL
052239,000287: 13,2622 27412 INTSTALL
052240,000288: 13,2623 45014 SET CALL
052241,000289: 13,2624 01076 NODOFLAG
052242,000290: 13,2625 26644 SETIFLGS
052243,000291: 13,2626 77650 GOTO
052244,000292: 13,2627 26026 STATEUP
052245,000293: 13,2630 00003 25140 600SECS 2DEC 60000 B-28
052246,000294:
052247,000295: 13,2632 77414 ENDINT CLEAR EXIT
052248,000296: 13,2633 01672 STATEFLG
052249,000297: 13,2634 05353 TC PHASCHNG
052250,000298: 13,2635 20032 OCT 20032
052251,000299: 13,2636 00006 EXTEND
052252,000300: 13,2637 32631 DCA 600SECS
052253,000301: 13,2640 05277 TC LONGCALL
052254,000302: 13,2641 E3,1626 EBANK= RRECTHIS
052255,000303: 13,2641 02604 26063 2CADR STATEINT
052256,000304:
052257,000305: 13,2643 05155 TC ENDOFJOB
052258,000306: 13,2644 43014 SETIFLGS SET CLEAR
052259,000307: 13,2645 01472 STATEFLG
052260,000308: 13,2646 01673 INTYPFLG
052261,000309: 13,2647 43014 CLEAR CLEAR
052262,000310: 13,2650 01676 DIM0FLAG
052263,000311: 13,2651 01675 D6OR9FLG
052264,000312: 13,2652 77616 RVQ
052265,000313: 13,2653 77776 NOINT EXIT
052266,000314: 13,2654 05353 TC PHASCHNG
052267,000315: 13,2655 00002 OCT 00002
052268,000316:
052269,000317: 13,2656 05516 TC DOWNFLAG
052270,000318: 13,2657 00221 ADRES QUITFLAG
052271,000319: 13,2660 05155 TC ENDOFJOB
052272,000320:
052273,000321: # ATOPCSM TRANSFERS RRECT TO RRECT +41 TO RRECTCSM TO RRECTCSM +41
052274,000322:
052275,000323: # CALLING SEQUENCE
052276,000324: # L CALL
052277,000325: # L+1 ATOPCSM
052278,000326:
052279,000327: # NORMAL EXIT AT L+2
052280,000328:
052281,000329: 13,2661 47020 ATOPCSM STQ RTB
052282,000330: 13,2662 00051 S2
052283,000331: 13,2663 26674 MOVEACSM
052284,000332: 13,2664 45014 SET CALL
052285,000333: 13,2665 04063 CMOONFLG
052286,000334: 13,2666 26114 SVDWN1
052287,000335: 13,2667 43014 BON CLRGO
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Page 1206 |
052289,000337: 13,2670 00303 MOONFLAG
052290,000338: 13,2671 00051 S2
052291,000339: 13,2672 04223 CMOONFLG
052292,000340: 13,2673 00051 S2
052293,000341: 13,2674 03036 MOVEACSM TC SETBANK
052294,000342: 13,2675 55500 TS DIFEQCNT # INITIALIZE INDEX
052295,000343: 13,2676 51500 INDEX DIFEQCNT
052296,000344: 13,2677 31502 CA RRECT
052297,000345: 13,2700 51500 INDEX DIFEQCNT
052298,000346: 13,2701 55554 TS RRECTCSM
052299,000347: 13,2702 11500 CCS DIFEQCNT # IS TRANSFER COMPLETE
052300,000348: 13,2703 12675 TCF MOVEACSM +1 # NO-LOOP
052301,000349: 13,2704 06060 TC DANZIG # COMPLETE - RETURN
052302,000350:
052303,000351:
052304,000352: # PTOACSM TRANSFERS RRECTCSM TO RRECTCSM +41 TO RRECT TO RRECT +41
052305,000353:
052306,000354: # CALLING SEQUENCE
052307,000355: # L CALL
052308,000356: # PTOACSM
052309,000357:
052310,000358: # NORMAL EXIT AT L+2
052311,000359: 13,2705 43034 PTOACSM RTB BON
052312,000360: 13,2706 26723 MOVEPCSM
052313,000361: 13,2707 04303 CMOONFLG
052314,000362: 13,2710 26716 SETMOON
052315,000363: 13,2711 66214 CLRMOON CLEAR SSP
052316,000364: 13,2712 00263 MOONFLAG
052317,000365: 13,2713 02031 PBODY
052318,000366: 13,2714 00000 0
052319,000367: 13,2715 77616 RVQ
052320,000368: 13,2716 66214 SETMOON SET SSP
052321,000369: 13,2717 00063 MOONFLAG
052322,000370: 13,2720 02031 PBODY
052323,000371: 13,2721 00002 2
052324,000372: 13,2722 77616 RVQ
052325,000373: 13,2723 03036 MOVEPCSM TC SETBANK
052326,000374: 13,2724 55500 TS DIFEQCNT
052327,000375: 13,2725 51500 INDEX DIFEQCNT
052328,000376: 13,2726 31554 CA RRECTCSM
052329,000377: 13,2727 51500 INDEX DIFEQCNT
052330,000378: 13,2730 55502 TS RRECT
052331,000379: 13,2731 11500 CCS DIFEQCNT
052332,000380: 13,2732 12724 TCF MOVEPCSM +1
052333,000381: 13,2733 06060 TC DANZIG
052334,000382:
052335,000383:
052336,000384: # ATOPLEM TRANSFERS RRECT TO RRECT +41 TO RRECTLEM TO RRECTLEM +41
052337,000385:
052338,000386: 13,2734 47020 ATOPLEM STQ RTB
|
|
Page 1207 |
052340,000388: 13,2735 00051 S2
052341,000389: 13,2736 26747 MOVEALEM
052342,000390: 13,2737 45014 SET CALL
052343,000391: 13,2740 04064 LMOONFLG
052344,000392: 13,2741 26070 SVDWN2
052345,000393: 13,2742 43014 BON CLRGO
052346,000394: 13,2743 00303 MOONFLAG
052347,000395: 13,2744 00051 S2
052348,000396: 13,2745 04224 LMOONFLG
052349,000397: 13,2746 00051 S2
052350,000398: 13,2747 03036 MOVEALEM TC SETBANK
052351,000399: 13,2750 55500 TS DIFEQCNT
052352,000400: 13,2751 51500 INDEX DIFEQCNT
052353,000401: 13,2752 31502 CA RRECT
052354,000402: 13,2753 51500 INDEX DIFEQCNT
052355,000403: 13,2754 55626 TS RRECTLEM
052356,000404: 13,2755 11500 CCS DIFEQCNT
052357,000405: 13,2756 12750 TCF MOVEALEM +1
052358,000406: 13,2757 06060 TC DANZIG
052359,000407:
052360,000408:
052361,000409: # PTOALEM TRANSFERS RRECTLEM TO RRECTLEM +41 TO RRECT TO RRECT +41
052362,000410:
052363,000411: 13,2760 47014 PTOALEM BON RTB
052364,000412: 13,2761 04307 SURFFLAG
052365,000413: 13,2762 27001 USEPIOS
052366,000414: 13,2763 26770 MOVEPLEM
052367,000415: 13,2764 52014 BON GOTO
052368,000416: 13,2765 04304 LMOONFLG
052369,000417: 13,2766 26716 SETMOON
052370,000418: 13,2767 26711 CLRMOON
052371,000419: 13,2770 03036 MOVEPLEM TC SETBANK
052372,000420: 13,2771 55500 TS DIFEQCNT
052373,000421: 13,2772 51500 INDEX DIFEQCNT
052374,000422: 13,2773 31626 CA RRECTLEM
052375,000423: 13,2774 51500 INDEX DIFEQCNT
052376,000424: 13,2775 55502 TS RRECT
052377,000425: 13,2776 11500 CCS DIFEQCNT
052378,000426: 13,2777 12771 TCF MOVEPLEM +1
052379,000427: 13,3000 06060 TC DANZIG
052380,000428:
052381,000429:
052382,000430: 13,3001 77201 USEPIOS SETPD VLOAD
052383,000431: 13,3002 00001 0
052384,000432: 13,3003 02023 RLS
052385,000433: 13,3004 41525 PDDL PUSH
052386,000434: 13,3005 00041 TDEC1
052387,000435: 13,3006 15517 STODL TET
052388,000436: 13,3007 27736 5/8
052389,000437: 13,3010 77624 CALL
|
|
Page 1208 |
052391,000439: 13,3011 51504 RP-TO-R
052392,000440: 13,3012 25535 STOVL RCV
052393,000441: 13,3013 22267 ZUNIT
052394,000442: 13,3014 14001 STODL 0D
052395,000443: 13,3015 01517 TET
052396,000444: 13,3016 14007 STODL 6D
052397,000445: 13,3017 27736 5/8
052398,000446: 13,3020 45014 SET CALL # NEEDED FOR SETTING X1 ON EXIT
052399,000447: 13,3021 00063 MOONFLAG
052400,000448: 13,3022 51504 RP-TO-R
052401,000449: 13,3023 74235 VXV VXSC
052402,000450: 13,3024 01535 RCV
052403,000451: 13,3025 26001 OMEGMOON
052404,000452: 13,3026 25543 STOVL VCV
052405,000453: 13,3027 22275 ZEROVEC
052406,000454: 13,3030 01521 STORE TDELTAV
052407,000455: 13,3031 67174 AXT,2 SXA,2
052408,000456: 13,3032 00002 2
052409,000457: 13,3033 02030 PBODY
052410,000458: 13,3034 35527 STCALL TNUV
052411,000459: 13,3035 27157 A-PCHK
052412,000460: 13,3036 33042 SETBANK CAF INTBANK
052413,000461: 13,3037 54006 TS BBANK
052414,000462: 13,3040 33457 CAF FORTYONE
052415,000463: 13,3041 00002 TC Q
052416,000464: 13,3042 E3,1554 EBANK= RRECTCSM
052417,000465: 13,3042 26063 INTBANK BBCON INTEGRV
052418,000466:
052419,000467:
052420,000468: # SPECIAL PURPOSE ENTRIES TO ORBITAL INTEGRATION. THESE ROUTINES PROVIDE ENTRANCES TO INTEGRATION WITH
052421,000469: # APPROPRIATE SWITCHES SET OR CLEARED FOR THE DESIRED INTEGRATION.
052422,000470:
052423,000471: # CSMPREC AND LEMPREC PERFORM ORBIT INTEGRATION BY THE ENCKE METHOD TO THE TIME INDICATED IN TDEC1
052424,000472: # ACCELERATIONS DUE TO OBLATENESS ARE INCLUDED. NO W-MATRIX INT. IS DONE.
052425,000473: # THE PERMANENT STATE VECTOR IS NOT UPDATED.
052426,000474: # CSMCONIC AND LEMCONIC PERFORM ORBIT INTEG. BY KEPLERS METHOD TO THE TIME INDICATED IN TDEC1
052427,000475: # NO DISTURBING ACCELERATIONS ARE INCLUDED. IN THE PROGRAM FLOW THE GIVEN
052428,000476: # STATE VECTOR IS RECTIFIED BEFORE SOLUTION OF KEPLERS EQUATION
052429,000477:
052430,000478: # THE ROUTINES ASSUME THAT THE CSM (LEM) STATE VECTOR IN P-MEM IS VALID.
052431,000479: # SWITCHES SET PRIOR TO ENTRY TO THE MAIN INTEG. PROG ARE AS FOLLOWS
052432,000480: # CSMPREC CSMCONIC LEMPREC LEMCONIC
052433,000481: # VINTFLAG SET SET CLEAR CLEAR
052434,000482: # INTYPFLG CLEAR SET CLEAR SET
052435,000483: # DIM0FLAG CLEAR CLEAR CLEAR CLEAR
052436,000484:
052437,000485:
052438,000486: # CALLING SEQUENCE
052439,000487: # L-X STORE TDEC1
052440,000488: # L CALL (STCALL TDEC1)
|
|
Page 1209 |
052442,000490: # L+1 CSMPREC (CSMCONIC, LEMPREC, LEMCONIC)
052443,000491:
052444,000492: # NORMAL EXIT TO L+2
052445,000493:
052446,000494:
052447,000495: # SUBROUTINES CALLED
052448,000496: # INTEGRV1
052449,000497: # PRECOUT FOR CSMPREC AND LEMPREC
052450,000498: # CONICOUT FOR CSMCONIC AND LEMCONIC
052451,000499:
052452,000500:
052453,000501: # OUTPUT - SEE PAGE 2 OF THIS LOG SECTION
052454,000502: # INPUT
052455,000503: # TDEC1 TIME TO INTEGRATE TO . CSECS B-28
052456,000504: 13,3043 45020 CSMPREC STQ CALL
052457,000505: 13,3044 00046 X1
052458,000506: 13,3045 27412 INTSTALL
052459,000507: 13,3046 43130 SXA,1 SET
052460,000508: 13,3047 02102 IRETURN
052461,000509: 13,3050 01474 VINTFLAG
052462,000510:
052463,000511: 13,3051 43014 IFLAGP SET CLEAR
052464,000512: 13,3052 01467 PRECIFLG
052465,000513: 13,3053 01676 DIM0FLAG
052466,000514: 13,3054 77614 CLRGO
052467,000515: 13,3055 01633 INTYPFLG
052468,000516: 13,3056 27136 INTEGRV1
052469,000517: 13,3057 45020 LEMPREC STQ CALL
052470,000518: 13,3060 00046 X1
052471,000519: 13,3061 27412 INTSTALL
052472,000520: 13,3062 43130 SXA,1 CLRGO
052473,000521: 13,3063 02102 IRETURN
052474,000522: 13,3064 01634 VINTFLAG
052475,000523: 13,3065 27051 IFLAGP
052476,000524:
052477,000525: 13,3066 45020 CSMCONIC STQ CALL
052478,000526: 13,3067 00046 X1
052479,000527: 13,3070 27412 INTSTALL
052480,000528: 13,3071 43130 SXA,1 SET
052481,000529: 13,3072 02102 IRETURN
052482,000530: 13,3073 01474 VINTFLAG
052483,000531: 13,3074 43014 IFLAGC CLEAR SETGO
052484,000532: 13,3075 01676 DIM0FLAG
052485,000533: 13,3076 01433 INTYPFLG
052486,000534: 13,3077 27136 INTEGRV1
052487,000535: 13,3100 45020 LEMCONIC STQ CALL
052488,000536: 13,3101 00046 X1
052489,000537: 13,3102 27412 INTSTALL
052490,000538: 13,3103 43130 SXA,1 CLRGO
052491,000539: 13,3104 02102 IRETURN
|
|
Page 1210 |
052493,000541: 13,3105 01634 VINTFLAG
052494,000542: 13,3106 27074 IFLAGC
052495,000543:
052496,000544: 13,3107 66214 INTEGRVS SET SSP
052497,000545: 13,3110 01467 PRECIFLG
052498,000546: 13,3111 02031 PBODY
052499,000547: 13,3112 00000 0
052500,000548: 13,3113 66214 BOF SSP
052501,000549: 13,3114 00343 MOONFLAG
052502,000550: 13,3115 27120 +3
052503,000551: 13,3116 02031 PBODY
052504,000552: 13,3117 00002 2
052505,000553: 13,3120 77220 STQ VLOAD
052506,000554: 13,3121 02102 IRETURN
052507,000555: 13,3122 22275 ZEROVEC
052508,000556: 13,3123 01521 STORE TDELTAV
052509,000557: 13,3124 35527 STCALL TNUV
052510,000558: 13,3125 23345 RECTIFY
052511,000559: 13,3126 43014 CLEAR SET
052512,000560: 13,3127 01676 DIM0FLAG
052513,000561: 13,3130 04062 NEWIFLG
052514,000562: 13,3131 77614 SETGO
052515,000563: 13,3132 04020 RPQFLAG
052516,000564: 13,3133 27150 ALOADED
052517,000565: # INTEGRV IS AN ENTRY TO ORBIT INTEGRATION WHICH PERMITS THE CALLER ,
052518,000566: # NORMALLY THE NAVIGATION PROGRAM ,TO SET THE INTEG. FLAGS. THE ROUTINE
052519,000567: # IS ENTERED AT INTEGRV1 BY CSMPREC ET.AL. AND AT ALOADED BY INTEGRVS.
052520,000568: # THE ROUTINE SETS UP A-MEMORY IF ENTERED AT INTEGRV,1 AND SETS THE INTEG.
052521,000569: # PROGRAM FOR PRECISION OR CONIC
052522,000570:
052523,000571: # THE CALLER MUST FIRST CALL INTSTALL TO CHECK IF INTEG. IS IN USE BEFORE
052524,000572: # SETTING ANY FLAGS.
052525,000573: # THE FLAGS WHICH SHOULD BE SET OR CLEARED ARE
052526,000574: # VINTFLAG (IGNORED WHEN ENTERED FROM INTEGRVS)
052527,000575: # INTYPFLG
052528,000576: # DIM0FLAG
052529,000577: # D6OR9FLG
052530,000578: # CALLING SEQUENCE
052531,000579: # L-X CALL
052532,000580: # L-Y INTSTALL
052533,000581: # L-1 SET OR CLEAR ALL FOUR FLAGS. ALSO CAN SET STATEFLG IF DESIRED
052534,000582: # AND DIM0FLAG IS CLEAR.
052535,000583: # L CALL
052536,000584: # L+1 INTEGRV
052537,000585: # INITIALIZATION
052538,000586: # FLAGS AS ABOVE
052539,000587: # STORE TIME TO INTEGRATE TO IN TDEC1
052540,000588: # OUTPUT
052541,000589: # RATT AS
052542,000590: # VATT DEFINED
|
|
Page 1211 |
052544,000592: # TAT BEFORE
052545,000593:
052546,000594:
052547,000595: 13,3134 77620 INTEGRV STQ
052548,000596: 13,3135 02102 IRETURN
052549,000597: 13,3136 43014 INTEGRV1 SET SET
052550,000598: 13,3137 04060 RPQFLAG
052551,000599: 13,3140 04062 NEWIFLG
052552,000600: 13,3141 77731 INTEGRV2 SSP
052553,000601: 13,3142 00053 QPRET
052554,000602: 13,3143 27150 ALOADED
052555,000603: 13,3144 52014 BON GOTO
052556,000604: 13,3145 01714 VINTFLAG
052557,000605: 13,3146 26705 PTOACSM
052558,000606: 13,3147 26760 PTOALEM
052559,000607: 13,3150 77745 ALOADED DLOAD
052560,000608: 13,3151 00041 TDEC1
052561,000609: 13,3152 01116 STORE TDEC
052562,000610: 13,3153 52014 BOFF GOTO
052563,000611: 13,3154 01753 INTYPFLG
052564,000612: 13,3155 27255 TESTLOOP
052565,000613: 13,3156 27241 RVCON
052566,000614: 13,3157 77414 A-PCHK BOFCLR EXIT
052567,000615: 13,3160 01652 STATEFLG
052568,000616: 13,3161 27200 RECTOUT
052569,000617: 13,3162 05353 TC PHASCHNG
052570,000618: 13,3163 04022 OCT 04022
052571,000619: 13,3164 05504 TC UPFLAG # PHASE CHANGE HAS OCCURRED BETWEEN
052572,000620: 13,3165 00236 ADRES REINTFLG # INTSTALL AND INTWAKE
052573,000621: 13,3166 06036 TC INTPRET
052574,000622: 13,3167 77731 SSP
052575,000623: 13,3170 00053 QPRET
052576,000624: 13,3171 27176 PHEXIT
052577,000625: 13,3172 52014 BON GOTO
052578,000626: 13,3173 01714 VINTFLAG
052579,000627: 13,3174 26661 ATOPCSM
052580,000628: 13,3175 26734 ATOPLEM
052581,000629: 13,3176 77624 PHEXIT CALL
052582,000630: 13,3177 11165 GRP2PC
052583,000631: 13,3200 45001 RECTOUT SETPD CALL
052584,000632: 13,3201 00001 0
052585,000633: 13,3202 23345 RECTIFY
052586,000634: 13,3203 53775 VLOAD VSL*
052587,000635: 13,3204 01503 RRECT
052588,000636: 13,3205 57576 0,2
052589,000637: 13,3206 53715 PDVL VSL* # RATT TO PD0
052590,000638: 13,3207 01511 VRECT
052591,000639: 13,3210 57576 0,2
052592,000640: 13,3211 63325 PDDL PDVL # VATT TO PD6 TAT TO PD12
052593,000641: 13,3212 01517 TET
|
|
Page 1212 |
052595,000643: 13,3213 01503 RRECT
052596,000644: 13,3214 64715 PDVL PDDL*
052597,000645: 13,3215 01511 VRECT
052598,000646: 13,3216 51770 MUEARTH,2
052599,000647: 13,3217 76006 PUSH AXT,1
052600,000648: 13,3220 77765 DEC -10 B-14
052601,000649: 13,3221 76014 BON AXT,1
052602,000650: 13,3222 00303 MOONFLAG
052603,000651: 13,3223 27225 +2
052604,000652: 13,3224 77775 DEC -2 B-14
052605,000653: 13,3225 40001 INTEXIT SETPD BOV
052606,000654: 13,3226 00001 0
052607,000655: 13,3227 27230 +1
052608,000656: 13,3230 43014 CLEAR CLEAR
052609,000657: 13,3231 04676 AVEMIDSW # ALLOW UPDATE OF DOWNLINK STATE VECTOR
052610,000658: 13,3232 01667 PRECIFLG
052611,000659: 13,3233 77535 SLOAD EXIT
052612,000660: 13,3234 02103 IRETURN
052613,000661: 13,3235 30154 CA MPAC
052614,000662: 13,3236 50120 INDEX FIXLOC
052615,000663: 13,3237 54052 TS QPRET
052616,000664: 13,3240 03427 TC INTWAKE
052617,000665: # RVCON SETS UP ORBIT INTEGRATION TO DO A CONIC SOLUTION FOR POSITION AND
052618,000666: # VELOCITY FOR THE INTERVAL (TET-TDEC)
052619,000667:
052620,000668: 13,3241 45345 RVCON DLOAD DSU
052621,000669: 13,3242 01116 TDEC
052622,000670: 13,3243 01517 TET
052623,000671: 13,3244 36074 STCALL TAU.
052624,000672: 13,3245 23345 RECTIFY
052625,000673: 13,3246 77624 CALL
052626,000674: 13,3247 22311 KEPPREP
052627,000675: 13,3250 43345 DLOAD DAD
052628,000676: 13,3251 01551 TC
052629,000677: 13,3252 01517 TET
052630,000678: 13,3253 35517 STCALL TET
052631,000679: 13,3254 27200 RECTOUT
052632,000680:
|
|
Page 1213 |
052634,000682: # TESTLOOP
052635,000683:
052636,000684: 13,3255 43014 TESTLOOP BOF CLRGO
052637,000685: 13,3256 04752 QUITFLAG
052638,000686: 13,3257 27262 +3
052639,000687: 13,3260 01632 STATEFLG
052640,000688: 13,3261 27225 INTEXIT # STOP INTEGRATION
052641,000689: 13,3262 73001 +3 SETPD LXA,2
052642,000690: 13,3263 00013 10D
052643,000691: 13,3264 02030 PBODY
052644,000692: 13,3265 51575 VLOAD ABVAL
052645,000693: 13,3266 01535 RCV
052646,000694: 13,3267 43006 PUSH CLEAR # RC TO 10D
052647,000695: 13,3270 00262 MIDFLAG
052648,000696: 13,3271 50023 DSU* BMN # MIDFLAG=0 IF R G.T. RMP
052649,000697: 13,3272 55467 RME,2
052650,000698: 13,3273 27276 +3
052651,000699: 13,3274 77614 SET
052652,000700: 13,3275 00062 MIDFLAG
052653,000701: 13,3276 41345 NORFINAL DLOAD DMP
052654,000702: 13,3277 00013 10D
052655,000703: 13,3300 00043 34D
052656,000704: 13,3301 55762 SR1R DDV*
052657,000705: 13,3302 51770 MUEARTH,2
052658,000706: 13,3303 41366 SQRT DMP
052659,000707: 13,3304 23676 .3D
052660,000708: 13,3305 40442 SR3 SR4 # DT IS TRUNCATED TO A MULTIPLE
052661,000709: 13,3306 54345 DLOAD SL
052662,000710: 13,3307 00155 MPAC
052663,000711: 13,3310 20220 15D # OF 128 CSECS.
052664,000712: 13,3311 40006 PUSH BOV
052665,000713: 13,3312 27337 MAXDT
052666,000714: 13,3313 50021 BDSU BMN
052667,000715: 13,3314 27411 DT/2MAX
052668,000716: 13,3315 27337 MAXDT
052669,000717: 13,3316 45345 DT/2COMP DLOAD DSU
052670,000718: 13,3317 01116 TDEC
052671,000719: 13,3320 01517 TET
052672,000720: 13,3321 54234 RTB SL
052673,000721: 13,3322 21516 SGNAGREE
052674,000722: 13,3323 20211 8D
052675,000723: 13,3324 02076 STORE DT/2 # B-19
052676,000724: 13,3325 51400 BOV ABS
052677,000725: 13,3326 27343 GETMAXDT
052678,000726: 13,3327 50025 DSU BMN # IS TIME TO INTEG. TO GR THAN MAXTIME
052679,000727: 13,3330 00015 12D
052680,000728: 13,3331 27347 P00HCHK
052681,000729: 13,3332 75345 USEMAXDT DLOAD SIGN
052682,000730: 13,3333 00015 12D
052683,000731: 13,3334 02076 DT/2
|
|
Page 1214 |
052685,000733: 13,3335 36076 STCALL DT/2
052686,000734: 13,3336 27347 P00HCHK
052687,000735: 13,3337 65345 MAXDT DLOAD PDDL # EXCHANGE DT/2MAX WITH COMPUTED MAX.
052688,000736: 13,3340 27411 DT/2MAX
052689,000737: 13,3341 77650 GOTO
052690,000738: 13,3342 27316 DT/2COMP
052691,000739: 13,3343 77634 GETMAXDT RTB
052692,000740: 13,3344 21664 SIGNMPAC
052693,000741: 13,3345 36076 STCALL DT/2
052694,000742: 13,3346 27332 USEMAXDT
052695,000743: 13,3347 51545 P00HCHK DLOAD ABS
052696,000744: 13,3350 02076 DT/2
052697,000745: 13,3351 50025 DSU BMN
052698,000746: 13,3352 27407 DT/2MIN
052699,000747: 13,3353 27157 A-PCHK
052700,000748: 13,3354 46135 SLOAD BHIZ
052701,000749: 13,3355 01012 MODREG
052702,000750: 13,3356 27361 +3
052703,000751: 13,3357 77650 GOTO
052704,000752: 13,3360 23156 TIMESTEP
052705,000753: 13,3361 77614 BON # WAS THIS CALL VIA CSM(LEM)PREC
052706,000754: 13,3362 01707 PRECIFLG
052707,000755: 13,3363 23156 TIMESTEP # YES
052708,000756: 13,3364 45345 DLOAD DSU
052709,000757: 13,3365 02076 DT/2
052710,000758: 13,3366 00015 12D
052711,000759: 13,3367 43040 BMN BOFCLR
052712,000760: 13,3370 27157 A-PCHK
052713,000761: 13,3371 04242 NEWIFLG
052714,000762: 13,3372 23156 TIMESTEP
052715,000763: 13,3373 45345 DLOAD DSU
052716,000764: 13,3374 01116 TDEC
052717,000765: 13,3375 01517 TET
052718,000766: 13,3376 77640 BMN # NO BACKWARD INTEGRATION
052719,000767: 13,3377 27225 INTEXIT
052720,000768: 13,3400 40525 PDDL SR4
052721,000769: 13,3401 02076 DT/2 # IS 4(DT) LS (TDEC - TET)
052722,000770: 13,3402 44322 SR2R BDSU # NO
052723,000771: 13,3403 52040 BMN GOTO
052724,000772: 13,3404 27225 INTEXIT
052725,000773: 13,3405 23156 TIMESTEP
052726,000774: 13,3406 00000 01400 DT/2MIN 2DEC 3 B-20
052727,000775:
052728,000776: 13,3410 14152 00000 DT/2MAX 2DEC 4000 E2 B-20
052729,000777:
052730,000778: 13,3412 77776 INTSTALL EXIT
052731,000779: 13,3413 34755 CAF ZERO
052732,000780: 13,3414 54001 ALLSTALL TS L
052733,000781: 13,3415 30106 CA RASFLAG
052734,000782: 13,3416 50001 INDEX L
|
|
Page 1215 |
052736,000784: 13,3417 73510 MASK INTBITAB # IS THIS STALL AREA FREE
052737,000785: 13,3420 00006 EXTEND
052738,000786: 13,3421 13466 BZF OKTOGRAB # YES
052739,000787: 13,3422 50001 INDEX L
052740,000788: 13,3423 33505 CAF WAKESTAL
052741,000789: 13,3424 05133 TC JOBSLEEP
052742,000790: 13,3425 77776 INTWAKE0 EXIT
052743,000791: 13,3426 13447 TCF INTWAKE1
052744,000792:
052745,000793: 13,3427 40106 INTWAKE CS RASFLAG # IS THIS INTSTALLED ROUTINE TO BE
052746,000794: 13,3430 74745 MASK REINTBIT # RESTARTED
052747,000795: 13,3431 10000 CCS A
052748,000796: 13,3432 03447 TC INTWAKE1 # NO
052749,000797:
052750,000798: 13,3433 50120 INDEX FIXLOC
052751,000799: 13,3434 30052 CA QPRET
052752,000800: 13,3435 55055 TS TBASE2 # YES, DONT RESTART WITH SOMEONE ELSES Q
052753,000801:
052754,000802: 13,3436 05353 TC PHASCHNG
052755,000803: 13,3437 04022 OCT 04022
052756,000804:
052757,000805: 13,3440 31055 CA TBASE2
052758,000806: 13,3441 50120 INDEX FIXLOC
052759,000807: 13,3442 54052 TS QPRET
052760,000808:
052761,000809: 13,3443 34745 CAF REINTBIT
052762,000810: 13,3444 70106 MASK RASFLAG
052763,000811: 13,3445 00006 EXTEND
052764,000812: 13,3446 13471 BZF GOBAC # DONT INTWAKE IF WE CAME HERE VIA RESTART
052765,000813:
052766,000814: 13,3447 34755 INTWAKE1 CAF ZERO
052767,000815: 13,3450 54154 WAKE TS STALTEM # INDEX OF ANY STALL USER
052768,000816: 13,3451 50154 WAKE1 INDEX STALTEM
052769,000817: 13,3452 33505 CAF WAKESTAL
052770,000818: 13,3453 00004 INHINT
052771,000819: 13,3454 05137 TC JOBWAKE
052772,000820: 13,3455 10064 CCS LOCCTR
052773,000821: 13,3456 13451 TCF WAKE1 # MAY BE MORE TO WAKE UP
052774,000822: 13,3457 00051 FORTYONE DEC 41 B-14
052775,000823: 13,3460 50154 INDEX STALTEM
052776,000824: 13,3461 43510 CS INTBITAB
052777,000825: 13,3462 70106 MASK RASFLAG
052778,000826: 13,3463 54106 TS RASFLAG # RELEASE STALL AREA
052779,000827: 13,3464 00003 RELINT
052780,000828: 13,3465 13471 TCF GOBAC
052781,000829: 13,3466 50001 OKTOGRAB INDEX L # NO, WAIT UNTIL AVAILABLE
052782,000830: 13,3467 34736 CAF INTFLBIT
052783,000831: 13,3470 26106 ADS RASFLAG
052784,000832: 13,3471 06036 GOBAC TC INTPRET
052785,000833: 13,3472 77616 RVQ
|
|
Page 1216 |
052787,000835: 13,3473 77776 ERASTAL1 EXIT
052788,000836: 13,3474 34753 CAF ONE
052789,000837: 13,3475 13414 TCF ALLSTALL
052790,000838: 13,3476 77776 ERASTAL2 EXIT
052791,000839: 13,3477 34752 CAF TWO
052792,000840: 13,3500 13414 TCF ALLSTALL
052793,000841: 13,3501 34753 ERASWAK1 CAF ONE
052794,000842: 13,3502 13450 TCF WAKE
052795,000843: 13,3503 34752 ERASWAK2 CAF TWO
052796,000844: 13,3504 13450 TCF WAKE
052797,000845: 13,3505 27413 WAKESTAL CADR INTSTALL +1
052798,000846: 13,3506 27474 CADR ERASTAL1 +1
052799,000847: 13,3507 27477 CADR ERASTAL2 +1
052800,000848: 13,3510 0154 STALTEM EQUALS MPAC
052801,000849: 13,3510 20100 INTBITAB OCT 20100
052802,000850: 13,3511 10040 OCT 10040
052803,000851: 13,3512 04020 OCT 04020
052804,000852:
|
|
Page 1217 |
052806,000854: # AVETOMID
052807,000855:
052808,000856: # THIS ROUTINE PERFORMS THE TRANSITION FROM A THRUSTING PHASE TO THE COAST
052809,000857: # PHASE BY INITIALIZING THIS VEHICLES PERMANENT STATE VECTOR WITH THE
052810,000858: # VALUES LEFT BY THE AVERAGEG ROUTINE IN RN,VN,PIPTIME.
052811,000859:
052812,000860: # BEFORE THIS IS DONE THE W-MATRIX, IF ITS VALID (ORWFLAG OR RENDWFLG IS
052813,000861: # SET) IS INTEGRATED FORWARD TO PIPTIME WITH THE PRE-THRUST STATE VECTOR.
052814,000862:
052815,000863: # IN ADDITION, THE OTHER VEHICLE IS INTEGRATED (PERMANENT) TO PIPTIME.
052816,000864:
052817,000865: # FINALLY TRKMKCNT IS ZEROED
052818,000866:
052819,000867: 13,2000 SETLOC INTINIT
052820,000868: 13,2000 BANK
052821,000869:
052822,000870: 13,3513 COUNT* $$/INTIN
052823,000871: 13,3513 43020 AVETOMID STQ BON
052824,000872: 13,3514 02772 EGRESS
052825,000873: 13,3515 02716 RENDWFLG
052826,000874: 13,3516 27562 INT/W # W-MATRIX VALID ,GO INTEGRATE IT
052827,000875: 13,3517 77614 BON
052828,000876: 13,3520 01711 ORBWFLAG
052829,000877: 13,3521 27562 INT/W # W-MATRIX VALID ,GO INTEGRATE IT
052830,000878:
052831,000879: 13,3522 45145 OTHERS DLOAD CALL # GET SET FOR OTHER VEHICLE INTEGRATION
052832,000880: 13,3523 01235 PIPTIME # DESIRED TIME
052833,000881: 13,3524 27412 INTSTALL
052834,000882: 13,3525 45014 SET CALL
052835,000883: 13,3526 01474 VINTFLAG # CM
052836,000884: 13,3527 26644 SETIFLGS # SETS UP NONE W-MAT. PERMANENT INTEG.
052837,000885: 13,3530 34041 STCALL TDEC1
052838,000886: 13,3531 27134 INTEGRV
052839,000887:
052840,000888: 13,3532 45174 AXT,2 CALL # NOW MOVE PROPERLY SCALE RN,UN AS WELL AS
052841,000889: 13,3533 00002 2 # PIPTIME TO INTEGRATION ERASABLES.
052842,000890: 13,3534 27412 INTSTALL
052843,000891: 13,3535 77014 BON AXT,2
052844,000892: 13,3536 04304 MOONTHIS
052845,000893: 13,3537 27541 +2
052846,000894: 13,3540 00000 0
052847,000895: 13,3541 53775 VLOAD VSR*
052848,000896: 13,3542 01221 RN
052849,000897: 13,3543 57176 0,2
052850,000898: 13,3544 01503 STORE RRECT
052851,000899: 13,3545 15535 STODL RCV
052852,000900: 13,3546 01235 PIPTIME
052853,000901: 13,3547 25517 STOVL TET
052854,000902: 13,3550 01227 VN
|
|
Page 1218 |
052856,000904: 13,3551 45057 VSR* CALL
052857,000905: 13,3552 57176 0,2
052858,000906: 13,3553 23361 MINIRECT # FINISH SETTING UP STATE VECTOR
052859,000907: 13,3554 66234 RTB SSP
052860,000908: 13,3555 26747 MOVATHIS # PUT TEMP STATE VECTOR INTO PERMANENT
052861,000909: 13,3556 03461 TRKMKCNT
052862,000910: 13,3557 00000 0
052863,000911: 13,3560 77650 GOTO
052864,000912: 13,3561 47130 FAZAB5
052865,000913:
052866,000914: 13,3562 45145 INT/W DLOAD CALL
052867,000915: 13,3563 01235 PIPTIME # INTEGRATE W THRU BURN
052868,000916: 13,3564 27412 INTSTALL
052869,000917: 13,3565 43014 SET SET
052870,000918: 13,3566 01476 DIM0FLAG # DO W-MATRIX
052871,000919: 13,3567 04476 AVEMIDSW # SO WONT CLOBBER RN,VN,PIPTIME
052872,000920: 13,3570 43014 SET CLEAR
052873,000921: 13,3571 01475 D6OR9FLG # 9X9 FOR LM
052874,000922: 13,3572 01674 VINTFLAG # LM
052875,000923: 13,3573 34041 STCALL TDEC1
052876,000924: 13,3574 27134 INTEGRV
052877,000925: 13,3575 77650 GOTO
052878,000926: 13,3576 27522 OTHERS # NOW GO DO THE OTHER VEHICLE
052879,000927:
|
|
Page 1219 |
052881,000929: # MIDTOAV1
052882,000930:
052883,000931: # THIS ROUTINE INTEGRATES (PRECISION) TO THE TIME SPECIFIED IN TDEC1.
052884,000932: # IF, AT THE END OF AN INTEGRATION TIME STEP, CURRENT TIME PLUS A DELTA
052885,000933: # TIME (SEE TIMEDELT.....BASED ON THE COMPUTATUON TIME FOR ONE TIME STEP)
052886,000934: # IS GREATER THAN THE DESIRED TIME, ALARM 1703 IS SET AND THE INTEGRATION
052887,000935: # IS DONE TO THE CURRENT TIME.
052888,000936: # RETURN IS IN BASIC TO THE RETURN ADDRESS PLUS ONE.
052889,000937:
052890,000938: # IF THE INTEGRATION IS FINISHED TO THE DESIRED TIME, RETURN IS IN BASIC
052891,000939: # TO THE RETURN ADDRESS
052892,000940:
052893,000941: # IN EITHER CASE , BEFORE RETURNING, THE EXTRAPOLATED STATE VECTOR IS TRAN
052894,000942: # FERRED FROM R,VATT TO R,VN1-PIPTIME1 IS SET TO THE FINISHING INTEGRA-
052895,000943: # TION TIME AND MPAC IS SET TO THE DELTA TIME---
052896,000944: # TAT MINUS CURRENT TIME.
052897,000945:
052898,000946:
052899,000947: # MIDTOAV2
052900,000948:
052901,000949: # THIS ROUTINE INTEGRATES THIS VEHICLES STATE VECTOR TO THE CURRENT TIME.
052902,000950: # NO INPUTS ARE REQUIRED OF THE CALLER. RETURN IS IN BASIC TO THE RETURN
052903,000951: # ADDRESS WITH THE ABOVE TRANSFERS TO R,VN1-PIPTIME1-AND MPAC DONE
052904,000952:
052905,000953: 13,3577 E7,1743 EBANK= IRETURN1
052906,000954: 13,3577 43020 MIDTOAV2 STQ CLRGO # INTEGRATE TO PRESENT TIME PLUS TIMEDELT
052907,000955: 13,3600 03743 IRETURN1
052908,000956: 13,3601 04634 MID1FLAG
052909,000957: 13,3602 27616 ENTMID2
052910,000958:
052911,000959: 13,3603 43020 MIDTOAV1 STQ SET # INTEGRATE TO TDEC1
052912,000960: 13,3604 03743 IRETURN1
052913,000961: 13,3605 04474 MID1FLAG
052914,000962: 13,3606 43234 RTB DAD # INITIAL CHECK, IS TDEC1 IN THE FUTURE
052915,000963: 13,3607 21462 LOADTIME
052916,000964: 13,3610 27720 TIMEDELT
052917,000965: 13,3611 51021 BDSU BPL
052918,000966: 13,3612 00041 TDEC1
052919,000967: 13,3613 27622 ENTMID1 # Y5S
052920,000968: 13,3614 77624 CALL
052921,000969: 13,3615 27706 NOTIME # NO, SET ALARM, SWITCH TO MIDTOAV2
052922,000970:
052923,000971: 13,3616 43234 ENTMID2 RTB DAD
052924,000972: 13,3617 21462 LOADTIME
052925,000973: 13,3620 27720 TIMEDELT
052926,000974: 13,3621 00041 STORE TDEC1
052927,000975:
052928,000976: 13,3622 77624 ENTMID1 CALL
052929,000977: 13,3623 27412 INTSTALL
052930,000978: 13,3624 45014 CLEAR CALL
|
|
Page 1220 |
052932,000980: 13,3625 01676 DIM0FLAG # NO W-MATRIX
052933,000981: 13,3626 26066 THISVINT
052934,000982: 13,3627 43014 CLEAR SET
052935,000983: 13,3630 01673 INTYPFLG
052936,000984: 13,3631 04475 MIDAVFLG # LET INTEG. KNOW THE CALL IS FOR MIDTOAV.
052937,000985: 13,3632 77624 CALL
052938,000986: 13,3633 27134 INTEGRV # GO INTEGRATE
052939,000987: 13,3634 77214 CLEAR VLOAD
052940,000988: 13,3635 04675 MIDAVFLG
052941,000989: 13,3636 00001 RATT
052942,000990: 13,3637 27543 STOVL RN1
052943,000991: 13,3640 00007 VATT
052944,000992: 13,3641 17551 STODL VN1
052945,000993: 13,3642 00015 TAT
052946,000994: 13,3643 03557 STORE PIPTIME1
052947,000995: 13,3644 66134 SXA,2 SXA,1
052948,000996: 13,3645 03376 RTX2
052949,000997: 13,3646 03375 RTX1
052950,000998: 13,3647 77776 EXIT
052951,000999:
052952,001000: 13,3650 00004 INHINT
052953,001001: 13,3651 00006 EXTEND
052954,001002: 13,3652 40025 DCS TIME2
052955,001003: 13,3653 20155 DAS MPAC
052956,001004: 13,3654 07256 TC TPAGREE
052957,001005:
052958,001006: 13,3655 31743 CA IRETURN1
052959,001007: 13,3656 04640 TC BANKJUMP
052960,001008: 13,3657 47014 CKMID2 BOF RTB
052961,001009: 13,3660 04754 MID1FLAG
052962,001010: 13,3661 27676 MID2
052963,001011: 13,3662 21462 LOADTIME
052964,001012: 13,3663 44215 DAD BDSU
052965,001013: 13,3664 27720 TIMEDELT
052966,001014: 13,3665 01116 TDEC
052967,001015: 13,3666 45044 BPL CALL
052968,001016: 13,3667 27255 TESTLOOP # YES
052969,001017: 13,3670 27706 NOTIME
052970,001018:
052971,001019: 13,3671 43234 TIMEINC RTB DAD
052972,001020: 13,3672 21462 LOADTIME
052973,001021: 13,3673 27720 TIMEDELT
052974,001022: 13,3674 35116 STCALL TDEC
052975,001023: 13,3675 27255 TESTLOOP
052976,001024:
052977,001025: 13,3676 45345 MID2 DLOAD DSU
052978,001026: 13,3677 01116 TDEC
052979,001027: 13,3700 01517 TET
052980,001028: 13,3701 45246 ABS DSU
052981,001029: 13,3702 27716 3CSECS
052982,001030:
|
|
Page 1221 |
052984,001032: 13,3703 52040 BMN GOTO
052985,001033: 13,3704 27157 A-PCHK
052986,001034: 13,3705 27671 TIMEINC
052987,001035:
052988,001036: 13,3706 77414 NOTIME CLEAR EXIT # TOO LATE
052989,001037: 13,3707 04674 MID1FLAG
052990,001038: 13,3710 25743 INCR IRETURN1 # SET ERROR EXIT (CALLOC +2)
052991,001039: 13,3711 05567 TC ALARM # INSUFFICIENT TIME FOR INTEGRATION --
052992,001040: 13,3712 01703 OCT 1703 # TIG WILL BE SLIPPED...
052993,001041: 13,3713 06036 TC INTPRET
052994,001042: 13,3714 77616 RVQ
052995,001043:
052996,001044: 13,3715 00000 00003 3CSECS 2DEC 3 B-28
052997,001045:
052998,001046: 13,3717 00000 01750 TIMEDELT 2DEC 1000 B-28
052999,001047:
053000,001048: 27,3332 BANK 27
053001,001049: 04,2000 SETLOC UPDATE2
053002,001050: 04,2000 BANK
053003,001051: 04,3106 1167 EBANK= INTWAKUQ
053004,001052:
053005,001053: 04,3106 COUNT* $$/INTIN
053006,001054:
053007,001055: 04,3106 1167 INTWAKUQ = INTWAK1Q # TEMPORARY UNTIL NAME OF INTWAK1Q IS CHNG
053008,001056:
053009,001057: 04,3106 00003 INTWAKEU RELINT
053010,001058: 04,3107 00006 EXTEND
053011,001059: 04,3110 23167 QXCH INTWAKUQ # SAVE Q FOR RETURN
053012,001060:
053013,001061: 04,3111 06036 TC INTPRET
053014,001062:
053015,001063: 04,3112 53135 SLOAD BZE # IS THIS A CSM/LEM STATE VECTOR UPDATE
053016,001064: 04,3113 01502 UPSVFLAG # REQUEST. IF NOT GO TO INTWAKUP.
053017,001065: 04,3114 11153 INTWAKUP
053018,001066:
053019,001067: 04,3115 77775 VLOAD # MOVE RRECT(6) AND VRECT(6) INTO
053020,001068: 04,3116 01503 RRECT # RCV(6) AND VCV(6) RESPECTIVELY.
053021,001069: 04,3117 25535 STOVL RCV
053022,001070: 04,3120 01511 VRECT # NOW GO TO 'RECTIFY +13D' TO
053023,001071: 04,3121 77624 CALL # STORE VRECT INTO VCV AND ZERO OUT
053024,001072: 04,3122 23362 RECTIFY +13D # TDELTAV(6),TNUV(6),TC(2) AND XKEP(2)
053025,001073: 04,3123 51535 SLOAD ABS # COMPARE ABSOLUTE VALUE OF 'UPSVFLAG'
053026,001074: 04,3124 01502 UPSVFLAG # TO 'UPDATE MOON STATE VECTOR CODE'
053027,001075: 04,3125 53025 DSU BZE # TO DETERMINE WHETHER THE STATE VECTOR TO
053028,001076: 04,3126 11164 UPMNSVCD # BE UPDATED IS IN THE EARTH OR LUNAR
053029,001077: 04,3127 11134 INTWAKEM # SPHERE OF INFLUENCE.........
053030,001078: 04,3130 43174 AXT,2 CLRGO # EARTH SPHERE OF INFLUENCE.
053031,001079: 04,3131 00000 DEC 0 B-14
053032,001080: 04,3132 00223 MOONFLAG
|
|
Page 1222 |
053034,001082: 04,3133 11137 INTWAKEC
053035,001083: 04,3134 43174 INTWAKEM AXT,2 SET # LUNAR SPHERE OF INFLUENCE.
053036,001084: 04,3135 00002 DEC 2 B-14
053037,001085: 04,3136 00063 MOONFLAG
053038,001086: 04,3137 50135 INTWAKEC SLOAD BMN # COMMON CODING AFTER X2 INITIALIZED AND
053039,001087: # MOONFLAG SET (OR CLEARED).
053040,001088: 04,3140 01502 UPSVFLAG # IS THIS A REQUEST FOR A LEM OR CSM
053041,001089: 04,3141 11147 INTWAKLM # STATE VECTOR UPDATE......
053042,001090: 04,3142 77624 CALL # UPDATE CSM STATE VECTOR
053043,001091: 04,3143 26661 ATOPCSM
053044,001092:
053045,001093: 04,3144 52014 CLEAR GOTO
053046,001094: 04,3145 01671 ORBWFLAG
053047,001095: 04,3146 11151 INTWAKEX
053048,001096:
053049,001097: 04,3147 77624 INTWAKLM CALL # UPDATE LM STATE VECTOR
053050,001098: 04,3150 26734 ATOPLEM
053051,001099:
053052,001100: 04,3151 77614 INTWAKEX CLEAR
053053,001101: 04,3152 02676 RENDWFLG
053054,001102:
053055,001103: 04,3153 45131 INTWAKUP SSP CALL # REMOVE :UPDATE STATE VECTOR INDICATOR:
053056,001104: 04,3154 01502 UPSVFLAG
053057,001105: 04,3155 00000 0
053058,001106: 04,3156 27425 INTWAKE0 # RELEASE :GRAB: OF ORBIT INTEG
053059,001107: 04,3157 77776 EXIT
053060,001108:
053061,001109: 04,3160 05353 TC PHASCHNG
053062,001110: 04,3161 04026 OCT 04026
053063,001111: 04,3162 01167 TC INTWAKUQ
053064,001112:
053065,001113: 04,3163 00002 UPMNSVCD OCT 2
053066,001114: 04,3164 00000 OCT 0
053067,001115:
053068,001116:
053069,001117: 04,3165 77420 GRP2PC STQ EXIT
053070,001118: 04,3166 02711 GRP2SVQ
053071,001119: 04,3167 05353 TC PHASCHNG
053072,001120: 04,3170 04022 OCT 04022
053073,001121: 04,3171 06036 TC INTPRET
053074,001122: 04,3172 77650 GOTO
053075,001123: 04,3173 02711 GRP2SVQ
End of include-file INTEGRATION_INITIALIZATION.agc. Parent file is MAIN.agc