Source Code
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These source-code files are part of a reconstructed copy of Comanche 45/2 (AKA Manche45 revision 2),
the final, flown mission release of the Apollo 10 Command Module (CM) Apollo Guidance
Computer (AGC) software. Comanche 45/2 was preceded by Comanche 44 and Comanche 45. The
reconstruction is believed to be exactly accurate, but in the absence of an actual Apollo-era
listing of Comanche 45/2, some explanation of the reconstruction process is needed
to insure confidence in that accuracy.
The starting point was the source code of Comanche 45 (itself previously accurately
reconstructed). Comanche 45 source code was then modified by incorporating changes
known from contemporary documentation to have been made between revisions 45 and 45/2.
The now-reconstructed Comanche 45/2 source code was
verified by assembling it and checking that the assembled code had
the expected known-correct memory-bank checksums.
Note that page numbers in the reconstructed code tend to match those in the Comanche 55, the
most-similar revision of Comanche for which we have access to an actual non-reconstructed hardcopy;
the source code would likely have different page numbers in a contemporary
Comanche 45 listing.
Annotations that were not present in the contemporary source code have been added to the reconstructed
code to justify each change relative to Comanche 44. Here's a guide to the Apollo documentation referenced
in those annotations:
Comments expected to have been present in the original source code are prefixed with a single '#' symbol,
whereas comments added later are prefixed by "##" or "###". Report any errors
noted by creating an
issue report at the Virtual AGC
Project's GitHub repository.
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055508,000002: ## Copyright: Public domain.
055509,000003: ## Filename: INTEGRATION_INITIALIZATION.agc
055510,000004: ## Purpose: A section of Manche45 revision 2.
055511,000005: ## It is part of the reconstructed source code for the
055512,000006: ## final, flown release of the flight software for the Command
055513,000007: ## Module's (CM) Apollo Guidance Computer (AGC) for Apollo 10.
055514,000008: ## The code has been recreated from a copy of Comanche 055. It
055515,000009: ## has been adapted such that the resulting bugger words
055516,000010: ## exactly match those specified for Manche 45/2 in NASA drawing
055517,000011: ## 2021153D, which gives relatively high confidence that the
055518,000012: ## reconstruction is correct.
055519,000013: ## Assembler: yaYUL
055520,000014: ## Contact: Ron Burkey <info@sandroid.org>.
055521,000015: ## Website: www.ibiblio.org/apollo/index.html
055522,000016: ## Mod history: 2020-12-24 MAS Created from Comanche 45.
055523,000017:
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Page 1309
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055525,000019: # 1.0 INTRODUCTION
055526,000020: # ----------------
055527,000021:
055528,000022: # FROM A USERS POINT OF VIEW, ORBITAL INTEGRATION IS ESSENTIALLY THE SAME AS THE 278 INTEGRATION
055529,000023: # PROGRAM. THE SAME ENTRANCES TO THE PROGRAM WILL BE MAINTAINED, THE SAME STALLING ROUTINE WILL BE USED AND
055530,000024: # OUTPUT WILL STILL BE VIA THE PUSHLIST. THE PRIMARY DIFFERENCES TO A USER INVOLVE THE ADDED CAPABILITY OF
055531,000025: # TERMINATING INTEGRATION AT A SPECIFIC FINAL RADIUS AND THE DIFFERENCE IN STATE VECTOR SCALING INSIDE AND OUT-
055532,000026: # SIDE THE LUNAR SPHERE OF INFLUENCE.
055533,000027:
055534,000028: # IN ORDER TO MAKE THE CSM(LEM)PREC AND CSM(LEM)CONIC ENTRANCES SIMILAR TO FLIGHT 278, THE INTEGRATION PROGRAM
055535,000029: # WILL ITSELF SET THE FINAL RADIUS (RFINAL) TO 0 SO THAT REACHING THE DESIRED TIME ONLY WILL TERMINATE
055536,000030: # INTEGRATION. THE DP REGISTER RFINAL MUST BE SET BY USERS OF INTEGRVS AND INTEGRV, AND MUST BE DONE AFTER THE
055537,000031: # CALL TC INTSTALL.
055538,000032:
055539,000033: # WHEN THE LM IS ON THE LUNAR SURFACE (INDICATED BY LUNAR SURFACE FLAG SET) CALLS TO LEMCONIC, LEMPREC, AND
055540,000034: # INTEGRV WITH VINFLAG = 0 WILL RESULT IN THE USE OF THE PLANETARY INERTIAL ORIENTATION SUBROUTINES TO PROVIDE
055541,000035: # BOTH THE LMS POSITION AND VELOCITY IN THE REFERENCE COORDINATE SYSTEM.
055542,000036: # THE PROGRAM WILL PROVIDE OUTPUT AS IF INTEGRATION WAS USED. THAT IS, THE PUSHLIST WILL BE SET AS NOTED BELOW AND
055543,000037: # THE PERMANENT STATE VECTOR UPDATED WHEN SPECIFIED BY AN INTEGRV CALL.
055544,000038:
055545,000039: # USERS OF INTEGRVS DESIRING INTEGRATION (INTYPFLG = 0) SHOULD NOTE THAT THE OBLATENESS PERTURBATION COMPUTATION
055546,000040: # IN LUNAR ORBIT IS TIME DEPENDENT. THEREFORE, THE USER SHOULD SUPPLY AN INITIAL STATE VECTOR VALID AT SOME REAL
055547,000041: # TIME AND THE DESIRED TIME (TDEC1) ALSO AT SOME REAL TIME. FOR CONIC ,,INTEGRATION,, THE USER MAY STILL USE ZERO
055548,000042: # AS THE INITIAL TIME AND DELTA TIME AS THE DESIRED TIME.
055549,000043:
055550,000044: # 2.0 GENERAL DESCRIPTION
055551,000045: # -----------------------
055552,000046:
055553,000047: # THE INTEGRATION PROGRAM OPERATES AS A CLOSED INTERPRETIVE SUBROUTINE AND PERFORMS THESE FUNCTIONS ---
055554,000048: # 1) INTEGRATES (PRECISION OR CONIC) EITHER CSM OR LM STATE VECTOR
055555,000049: # 2) INTEGRATES THE W-MATRIX
055556,000050: # 3) PERMANENT OR TEMPORARY UPDATE OF THE STATE VECTOR
055557,000051:
055558,000052: # THERE ARE SIX ENTRANCES TO THE INTEGRATION PROGRAM. FOUR OF THESE (CSMPREC, LEMPREC, CSMCONIC, LEMCONIC) SET
055559,000053: # ALL THE FLAGS REQUIRED IN THE INTEGRATION PROGRAM ITSELF TO CAUSE THE PRECISION OR CONIC INTEGRATION (KEPLER) OF
055560,000054: # THE LM OR CSM STATE VECTOR, AS THE NAMES SUGGEST. ONE ENTRANCE (INTEGRVS) PERMITS THE CALLING PROGRAM TO
055561,000055: # PROVIDE A STATE VECTOR TO BE INTEGRATED. THE CALLING PROGRAM MUST SET THE FLAGS INDICATING (1) PRECISION OR
055562,000056: # CONIC INTEGRATION, (2) IN OR OUT OF LUNAR SPHERE, (3) MIDCOURSE OR NOT, AND THE INTEGRATION PROGRAM COMPLETES
055563,000057: # THE FLAG SETTING TO BYPASS W-MATRIX INTEGRATION. THE LAST ENTRANCE (INTEGRV, USED IN GENERAL BY THE
055564,000058: # NAVIGATION PROGRAMS) PERMITS THE CALLER TO SET FIVE FLAGS (NOT MOONFLAG OR MIDFLAG) BUT NOT TO INPUT A STATE
055565,000059: # VECTOR. ANY PROGRAM WHICH CALLS INTEGRVS OR INTEGRV MUST CALL INTSTALL BEFORE IT SETS THE INTEGRATION FLAGS
055566,000060: # AND/OR STATE VECTOR.
055567,000061:
055568,000062: # THREE SETS OF 42 REGISTERS AND 2 FLAGS ARE USED FOR THE STATE VECTORS. TWO SETS, WHICH MAY NOT BE OVERLAYED, ARE
055569,000063: # USED FOR THE PERMANENT STATE VECTORS FOR THE CSM AND LM. THE THIRD SET, WHICH MAY BE OVERLAYED WHEN INTEGRATION
055570,000064: # IS NOT BEING DONE, IS USED IN THE COMPUTATIONS.
055571,000065:
055572,000066: # THE PERMANENT STATE VECTORS WILL BE PERIODICALLY UPDATED SO THAT THE VECTORS WILL NOT BE OLDER THAN 4 TIMESTEPS.
055573,000067: # THE PERMANENT STATE VECTORS WILL ALSO BE UPDATED WHENEVER THE W-MATRIX IS INTEGRATED OR WHEN A CALLER OF INTEGRV
055574,000068: # SETS STATEFLG (THE NAVIGATION PROGRAMS P20, P22.)
055575,000069:
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Page 1310
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055577,000071: # APPENDIX B OF THE USERS GUIDE LISTS THE STATE VECTOR QUANTITIES.
055578,000072:
055579,000073: # 2.1 RESTARTS
055580,000074:
055581,000075: # PHASE CHANGES WILL BE MADE IN THE INTEGRATION PROGRAM ONLY FOR THE INTEGRV ENTRANCE (I.E., WHEN THE W-MATRIX IS
055582,000076: # INTEGRATED OR PERMANENT STATE VECTOR IS UPDATED.) THE GROUP NUMBER USED WILL BE THAT FOR THE P20-25 PROGRAMS
055583,000077: # (I.E., GROUP2) SINCE THE INTEGRV ENTRANCE WILL ONLY BE USED BY THESE PROGRAMS. IF A RESTART OCCURS DURING AN
055584,000078: # INTEGRATION OF THE STATE VECTOR ONLY, THE RECOVERY WILL BE TO THE LAST PHASE IN THE CALLING PROGRAM. CALLING
055585,000079: # PROGRAMS WHICH USE THE INTEGRV OR INTEGRVS ENTRANCE OF INTEGRATION SHOULD ENSURE THAT IF PHASE CHANGING IS DONE
055586,000080: # THAT IT IS PRIOR TO SETTING THE INTEGRATION INPUTS IN THE PUSHLIST.
055587,000081: # THIS IS BECAUSE THE PUSHLIST IS LOST DURING A RESTART.
055588,000082:
055589,000083: # 2.2 SCALING
055590,000084:
055591,000085: # THE INTEGRATION ROUTINE WILL MAINTAIN THE PERMANENT MEMORY STATE VECTORS IN THE SCALING AND UNITS DEFINED IN
055592,000086: # APPENDIX B OF THE USERS GUIDE. THE SCALING OF THE OUTPUT POSITION VECTOR DEPENDS ON THE ORIGIN OF THE COORDINATE
055593,000087: # SYSTEM AT THE DESIRED INTEGRATION TIME. THE COORDINATE SYSTEM TRANSFORMATION WILL BE DONE AUTOMATICALLY ON
055594,000088: # MULTIPLE TIMESTEP ENCKE INTEGRATION ONLY. THUS IT IS POSSIBLE TO HAVE OUTPUT FROM SUCCESSIVE INTEGRATIONS IN
055595,000089: # DIFFERENT SCALING.
055596,000090: # HOWEVER, RATT, VATT WILL ALWAYS BE SCALED THE SAME.
055597,000091:
055598,000092: # 3.0 INPUT/OUTPUT
055599,000093: # ----------------
055600,000094:
055601,000095: # PROGRAM INPUTS ARE THE FLAGS DESCRIBED IN APPENDIX A AND THE PERMANENT STATE VECTOR QUANTITIES DESCRIBED IN AP-
055602,000096: # PENDIX B OF THE USERS GUIDE, PLUS THE DESIRED TIME TO INTEGRATE TO IN TDEC1 (A PUSH LIST LOCATION).
055603,000097: # FOR INTEGRVS, THE RCV,VCV,TET OF THE TEMPORARY STATE VECTOR MUST BE SET, PLUS MOONFLAG AND MIDFLAG
055604,000098:
055605,000099: # FOR SIMULATION THE FOLLOWING QUANTITIES MUST BE PRESET ---
055606,000100: # EARTH MOON
055607,000101: # 29 27
055608,000102: # RRECTCSM(LEM) - RECTIFIED POSITION VECTOR METERS 2 2
055609,000103:
055610,000104: # 7 5
055611,000105: # VRECTCSM(LEM) - RECTIFIED VELOCITY VECTOR M/CSEC 2 2
055612,000106:
055613,000107: # 28 28
055614,000108: # TETCSM(LEM) - TIME STATE VECTOR IS VALID CSEC 2 2
055615,000109: # CUSTOMARILY 0, BUT NOTE LUNAR
055616,000110: # ORBIT DEPENDENCE ON REAL TIME.
055617,000111:
055618,000112: # 22 18
055619,000113: # DELTAVCSM(LEM) - POSITION DEVIATION METERS 2 2
055620,000114: # 0 IF TCCSM(LEM) = 0
055621,000115:
055622,000116: # 3 -1
055623,000117: # NUVCSM(LEM) - VELOCITY DEVIATION M/CSEC 2 2
055624,000118: # 0 IF TCCSM(LEM) = 0
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Page 1311
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055626,000120: # 29 27
055627,000121: # RCVCSM(LEM) - CONIC POSITION METERS 2 2
055628,000122: # EQUALS RRECTCSM(LEM) IF
055629,000123: # TCCSM(LEM) = 0
055630,000124:
055631,000125: # 7 5
055632,000126: # VCVCSM(LEM) - CONIC VELOCITY M/CSEC 2 2
055633,000127: # EQUALS VRECTCSM(LEM) IF
055634,000128: # TCCSM(LEM) = 0
055635,000129:
055636,000130: # 28 28
055637,000131: # TCCSM(LEM) - TIME SINCE RECTIFICATION CSECS 2 2
055638,000132: # CUSTOMARILY 0
055639,000133:
055640,000134: # 1/2 17 16
055641,000135: # XKEPCSM(LEM) - ROOT OF KEPLERS EQUATION M 2 2
055642,000136: # 0 IF TCCSM(LEM) = 0
055643,000137:
055644,000138: # CMOONFLG - PERMANENT FLAGS CORRESPONDING 0 0
055645,000139: # CMIDFLAG TO MOONFLAG AND MIDFLAG 0,1 0,1
055646,000140: # LMOONFLG C = CSM, L = LM 0 0
055647,000141: # LMIDFLG 0,1 0,1
055648,000142:
055649,000143: # SURFFLAG - LUNAR SURFACE FLAG 0,1 0,1
055650,000144:
055651,000145: # IN ADDITION, IF (L)CMIDFLAG IS SET, THE INITIAL INPUT VALUES FOR LUNAR
055652,000146: # SOLAR EPHEMERIDES SUBROUTINE AND PLANETARY INERTIAL ORIENTATION SUB-
055653,000147: # ROUTINE MUST BE PRESET.
055654,000148:
055655,000149: # OUTPUT
055656,000150: # AFTER EVERY CALL TO INTEGRATION
055657,000151: # EARTH MOON
055658,000152: # 29 29
055659,000153: # 0D RATT POSITION METERS 2 2
055660,000154:
055661,000155: # 7 7
055662,000156: # 6D VATT VELOCITY M/CSEC 2 2
055663,000157:
055664,000158: # 28 28
055665,000159: # 12D TAT TIME 2 2
055666,000160:
055667,000161: # 29 27
055668,000162: # 14D RATT1 POSITION METERS 2 2
055669,000163:
055670,000164: # 7 5
055671,000165: # 20D VATT1 VELOCITY M/CSEC 2 2
055672,000166:
055673,000167: # 3 2 36 30
055674,000168: # 26D MU(P) MU M /CS 2 2
055675,000169:
055676,000170: # X1 MUTABLE ENTRY -2 -10D
055677,000171:
055678,000172: # X2 COORDINT
055679,000173: # X2 COORDINATE SYSTEM ORIGEN 0 2
055680,000174: # (THIS, NOT MOONFLAG, SHOULD BE
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Page 1312
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055682,000176: # USED TO DETERMINE ORIGIN.)
055683,000177:
055684,000178: # IN ADDITION TO THE ABOVE, THE PERMANENT STATE VECTOR IS UPDATED WHENEVER
055685,000179: # STATEFLG WAS SET AND WHENEVER A W-MATRIX IS TO BE INTEGRATED. THE PUSH
055686,000180: # COUNTER IS SET TO 0 AND OVERFLOW IS CLEARED BEFORE RETURNING TO THE
055687,000181: # CALLING PROGRAM.
055688,000182:
055689,000183: # 4.0 CALLING SEQUENCES AND SAMPLE CODE
055690,000184: # -------------------------------------
055691,000185:
055692,000186: # A) PRECISION ORBITAL INTEGRATION. CSMPREC, LEMPREC ENTRANCES
055693,000187: # L-X STORE TIME TO 95T5791T5 T 95 PUS L9ST (T4531)
055694,000188: # L CALL
055695,000189: # L+1 CSMPREC (OR LEMPREC)
055696,000190: # L+2 RETURN
055697,000191: # INPUT 28
055698,000192: # TDEC1 (PD 32D) TIME TO INTEGRATE TO...CENTISECONDS SCALED 2
055699,000193: # OUTPUT
055700,000194: # THE DATA LISTED IN SECTION 3.0 PLUS
055701,000195: # RQVV POSITION VECTOR OF VEHICLE WITH RESPECT TO SECONDARY
055702,000196: # BODY... METERS B-29 ONLY IF MIDFLAG = DIMOFLAG = 1
055703,000197: # B) CONIC INTEGRATION. CSMCONIC, LEMCONIC ENTRANCES
055704,000198: # L-X STORE TIME IN PUSH LIST (TDEC1)
055705,000199: # L CALL
055706,000200: # L+1 CSMCONIC (OR LEMCONIC)
055707,000201: # INPUT/OUTPUT
055708,000202: # SAME AS PRECISION INTEGRATION, EXCEPT RQVV NOT SET
055709,000203: # C) INTEGRATE GIVEN STATE VECTOR. INTEGRVS ENTRANCE
055710,000204: # CALL
055711,000205: # INTSTALL
055712,000206: # VLOAD
055713,000207: # POSITION VECTOR
055714,000208: # STOVL RCV
055715,000209: # VELOCITY VECTOR
055716,000210: # STODL VCV
055717,000211: # TIME STATE VECTOR VALID
055718,000212: # STODL TET
055719,000213: # FINAL RADIUS
055720,000214: # STORE RFINAL
055721,000215: # SET(CLEAR) SET(CLEAR)
055722,000216: # INTYPFLAG
055723,000217: # MOONFLAG
055724,000218: # SET(CLEAR) DLOAD
055725,000219: # DESIRED TIME
055726,000220: # STCALL TDEC1
055727,000221: # INTEGRVS
055728,000222: # INPUT
055729,000223: # RCV POSITION VECTOR METERS
055730,000224: # VCV VELOCITY VECTOR M/CSEC
055731,000225: # TET TIME OF STATE VECTOR (MAY = 0) CSEC B-28
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Page 1313
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055733,000227: # TDEC1 TIME TO INTEGRATE TO CSEC B-28 (PD 32D)
055734,000228: # (MAY BE INCREMENT IF TET=0)
055735,000229: # OUTPUT
055736,000230: # SAME AS FOR PRECISION OR CONIC INTEGRATION,
055737,000231: # DEPENDING ON INTYPFLG.
055738,000232: # D) INTEGRATE STATE VECTOR. INTGRV ENTRANCE
055739,000233: # L-X STORE TIME IN PUSH LIST (TDEC1) (MAY BE DONE AFTER CALL TO INTSTALL)
055740,000234: # L-8 CALL
055741,000235: # L-7
055742,000236: # L-6 SET(CLEAR) SET(CLEAR)
055743,000237: # L-5 VINTFLAG 1=CSM, 0=LM
055744,000238: # L-4 INTYPFLAG 1=CONIC, 0=PRECISION
055745,000239: # L-3 SET(CLEAR) SET(CLEAR)
055746,000240: # L-2 DIMOFLAG 1=W-MATRIX, 0=NO W-MATRIX
055747,000241: # L-1 D6OR9FLG 1=9X9, 0=6X6
055748,000242: # L SET DLOAD
055749,000243: # L+1 STATEFLG DESIRE PERMANENT UPDATE
055750,000244: # L+2 FINAL RAD. OF STATE VECTOR
055751,000245: # L+3 STCALL RFINAL
055752,000246: # L+4 INTEGRV
055753,000247: # L CALL NORMAL USE -- WILL UPDATE STATE
055754,000248: # L+1 INTEGRV VECTOR IF DIMOFLAG=1. (STATEFLG IS
055755,000249: # L+2 RETURN ALWAYS RESET IN INTEGRATION AFTER
055756,000250: # IT IS USED.)
055757,000251: # INPUT
055758,000252: # TDEC1 (PD 32D) TIME TO INTEGRATE TO CSEC B-28
055759,000253: # OUTPUT
055760,000254: # SAME AS FOR PRECISION OR CONIC INTEGRATION
055761,000255: # THE PROGRAM WILL SET MOONFLAG, MIDFLAG DEPENDING ON
055762,000256: # THE PERMANENT STATE VECTOR REPRESENTATION.
055763,000257:
055764,000258: 11,2363 BANK 11
055765,000259: 13,2000 SETLOC INTINIT
055766,000260: 13,2000 BANK
055767,000261: 13,2627 E3,1554 EBANK= RRECTCSM
055768,000262: 13,2627 COUNT 13/INTIN
055769,000263:
055770,000264: 13,2627 05412 STATEINT TC PHASCHNG
055771,000265: 13,2630 00052 OCT 00052
055772,000266: 13,2631 35061 CAF PRIO5
055773,000267: 13,2632 05147 TC FINDVAC
055774,000268: 13,2633 E3,1554 EBANK= RRECTCSM
055775,000269: 13,2633 02636 26063 2CADR STATINT1
055776,000270:
055777,000271: 13,2635 05324 TC TASKOVER
055778,000272: 13,2636 06006 STATINT1 TC INTPRET
055779,000273: 13,2637 47014 BON RTB
055780,000274: 13,2640 04712 QUITFLAG
055781,000275: 13,2641 26677 NOINT # NO STATEINT IF V96
055782,000276: 13,2642 45510 LOADTIME
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Page 1314
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055784,000278: 13,2643 00041 STORE TDEC1
055785,000279: 13,2644 45014 CLEAR CALL
055786,000280: 13,2645 04274 V96ONFLG
055787,000281: 13,2646 27442 INTSTALL
055788,000282: 13,2647 45014 SET CALL
055789,000283: 13,2650 01076 NODOFLAG
055790,000284: 13,2651 26670 SETIFLGS
055791,000285: 13,2652 77650 GOTO
055792,000286: 13,2653 26000 STATEUP
055793,000287: 13,2654 00003 25140 600SECS 2DEC 60000 B-28
055794,000288:
055795,000289: 13,2656 77414 ENDINT CLEAR EXIT
055796,000290: 13,2657 01672 STATEFLG
055797,000291: 13,2660 05412 TC PHASCHNG
055798,000292: 13,2661 20032 OCT 20032
055799,000293: 13,2662 00006 EXTEND
055800,000294: 13,2663 32655 DCA 600SECS
055801,000295: 13,2664 05342 TC LONGCALL
055802,000296: 13,2665 E3,1554 EBANK= RRECTHIS
055803,000297: 13,2665 02627 26063 2CADR STATEINT
055804,000298:
055805,000299: 13,2667 05217 TC ENDOFJOB
055806,000300: 13,2670 43014 SETIFLGS SET CLEAR
055807,000301: 13,2671 01472 STATEFLG
055808,000302: 13,2672 01673 INTYPFLG
055809,000303: 13,2673 43014 CLEAR CLEAR
055810,000304: 13,2674 01676 DIM0FLAG
055811,000305: 13,2675 01675 D6OR9FLG
055812,000306: 13,2676 77616 RVQ
055813,000307: 13,2677 77776 NOINT EXIT
055814,000308: 13,2700 05412 TC PHASCHNG
055815,000309: 13,2701 00002 OCT 2
055816,000310:
055817,000311: 13,2702 05560 TC DOWNFLAG
055818,000312: 13,2703 00221 ADRES QUITFLAG
055819,000313:
055820,000314: 13,2704 05217 TC ENDOFJOB
055821,000315:
055822,000316: # ATOPCSM TRANSFERS RRECT TO RRECT +41 TO RRECTCSM TO RRECTCSM +41
055823,000317:
055824,000318: # CALLING SEQUENCE
055825,000319: # L CALL
055826,000320: # L+1 ATOPCSM
055827,000321:
055828,000322: # NORMAL EXIT AT L+2
055829,000323:
055830,000324: 13,2705 47020 ATOPCSM STQ RTB
055831,000325: 13,2706 00051 S2
055832,000326: 13,2707 26720 MOVEACSM
055833,000327: 13,2710 45014 SET CALL
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Page 1315
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055835,000329: 13,2711 04063 CMOONFLG
055836,000330: 13,2712 20237 SVDWN1
055837,000331: 13,2713 43014 BON CLRGO
055838,000332: 13,2714 00303 MOONFLAG
055839,000333: 13,2715 00051 S2
055840,000334: 13,2716 04223 CMOONFLG
055841,000335: 13,2717 00051 S2
055842,000336: 13,2720 03064 MOVEACSM TC SETBANK
055843,000337: 13,2721 55500 TS DIFEQCNT # INITIALIZE INDEX
055844,000338: 13,2722 51500 INDEX DIFEQCNT
055845,000339: 13,2723 31502 CA RRECT
055846,000340: 13,2724 51500 INDEX DIFEQCNT
055847,000341: 13,2725 55554 TS RRECTCSM
055848,000342: 13,2726 11500 CCS DIFEQCNT # IS TRANSFER COMPLETE
055849,000343: 13,2727 12721 TCF MOVEACSM +1 # NO-LOOP
055850,000344: 13,2730 06030 TC DANZIG # COMPLETE - RETURN
055851,000345:
055852,000346: # PTOACSM TRANSFERS RRECTCSM TO RRECTCSM +41 TO RRECT TO RRECT +41
055853,000347:
055854,000348: # CALLING SEQUENCE
055855,000349: # L CALL
055856,000350: # PTOACSM
055857,000351:
055858,000352: # NORMAL EXIT AT L+2
055859,000353:
055860,000354: 13,2731 43034 PTOACSM RTB BON
055861,000355: 13,2732 26747 MOVEPCSM
055862,000356: 13,2733 04303 CMOONFLG
055863,000357: 13,2734 26742 SETMOON
055864,000358: 13,2735 66214 CLRMOON CLEAR SSP
055865,000359: 13,2736 00263 MOONFLAG
055866,000360: 13,2737 02151 PBODY
055867,000361: 13,2740 00000 0
055868,000362: 13,2741 77616 RVQ
055869,000363: 13,2742 66214 SETMOON SET SSP
055870,000364: 13,2743 00063 MOONFLAG
055871,000365: 13,2744 02151 PBODY
055872,000366: 13,2745 00002 2
055873,000367: 13,2746 77616 RVQ
055874,000368: 13,2747 03064 MOVEPCSM TC SETBANK
055875,000369: 13,2750 55500 TS DIFEQCNT
055876,000370: 13,2751 51500 INDEX DIFEQCNT
055877,000371: 13,2752 31554 CA RRECTCSM
055878,000372: 13,2753 51500 INDEX DIFEQCNT
055879,000373: 13,2754 55502 TS RRECT
055880,000374: 13,2755 11500 CCS DIFEQCNT
055881,000375: 13,2756 12750 TCF MOVEPCSM +1
055882,000376: 13,2757 06030 TC DANZIG
055883,000377:
|
|
Page 1316
|
055885,000379: # ATOPLEM TRANSFERS RRECT TO RRECT +41 TO RRECTLEM TO RRECTLEM +41
055886,000380: 13,2760 47020 ATOPLEM STQ RTB
055887,000381: 13,2761 00051 S2
055888,000382: 13,2762 26773 MOVEALEM
055889,000383: 13,2763 45014 SET CALL
055890,000384: 13,2764 04064 LMOONFLG
055891,000385: 13,2765 20263 SVDWN2
055892,000386: 13,2766 43014 BON CLRGO
055893,000387: 13,2767 00303 MOONFLAG
055894,000388: 13,2770 00051 S2
055895,000389: 13,2771 04224 LMOONFLG
055896,000390: 13,2772 00051 S2
055897,000391: 13,2773 03064 MOVEALEM TC SETBANK
055898,000392: 13,2774 55500 TS DIFEQCNT
055899,000393: 13,2775 51500 INDEX DIFEQCNT
055900,000394: 13,2776 31502 CA RRECT
055901,000395: 13,2777 51500 INDEX DIFEQCNT
055902,000396: 13,3000 55626 TS RRECTLEM
055903,000397: 13,3001 11500 CCS DIFEQCNT
055904,000398: 13,3002 12774 TCF MOVEALEM +1
055905,000399: 13,3003 06030 TC DANZIG
055906,000400:
055907,000401: # PTOALEM TRANSFERS RRECTLEM TO RRECTLEM +41 TO RRECT TO RRECT +41
055908,000402:
055909,000403: 13,3004 47014 PTOALEM BON RTB
055910,000404: 13,3005 04307 SURFFLAG
055911,000405: 13,3006 27025 USEPIOS
055912,000406: 13,3007 27014 MOVEPLEM
055913,000407: 13,3010 52014 BON GOTO
055914,000408: 13,3011 04304 LMOONFLG
055915,000409: 13,3012 26742 SETMOON
055916,000410: 13,3013 26735 CLRMOON
055917,000411: 13,3014 03064 MOVEPLEM TC SETBANK
055918,000412: 13,3015 55500 TS DIFEQCNT
055919,000413: 13,3016 51500 INDEX DIFEQCNT
055920,000414: 13,3017 31626 CA RRECTLEM
055921,000415: 13,3020 51500 INDEX DIFEQCNT
055922,000416: 13,3021 55502 TS RRECT
055923,000417: 13,3022 11500 CCS DIFEQCNT
055924,000418: 13,3023 13015 TCF MOVEPLEM +1
055925,000419: 13,3024 06030 TC DANZIG
055926,000420:
055927,000421: 13,3025 77201 USEPIOS SETPD VLOAD
055928,000422: 13,3026 00001 0
055929,000423: 13,3027 02026 RLS
055930,000424: 13,3030 41525 PDDL PUSH
055931,000425: 13,3031 00041 TDEC1
|
|
Page 1317
|
055933,000427: 13,3032 15517 STODL TET
055934,000428: 13,3033 27755 5/8
055935,000429: 13,3034 77624 CALL
055936,000430: 13,3035 55344 RP-TO-R
055937,000431: 13,3036 25535 STOVL RCV
055938,000432: 13,3037 11555 ZUNIT
055939,000433: 13,3040 14001 STODL 0D
055940,000434: 13,3041 01517 TET
055941,000435: 13,3042 14007 STODL 6D
055942,000436: 13,3043 27755 5/8
055943,000437: 13,3044 45014 SET CALL # NEEDED FOR SETTING X1 ON EXIT
055944,000438: 13,3045 00063 MOONFLAG
055945,000439: 13,3046 55344 RP-TO-R
055946,000440: 13,3047 74235 VXV VXSC
055947,000441: 13,3050 01535 RCV
055948,000442: 13,3051 27063 OMEGMOON
055949,000443: 13,3052 25543 STOVL VCV
055950,000444: 13,3053 11563 ZEROVEC
055951,000445: 13,3054 01521 STORE TDELTAV
055952,000446: 13,3055 67174 AXT,2 SXA,2
055953,000447: 13,3056 00002 2
055954,000448: 13,3057 02150 PBODY
055955,000449: 13,3060 35527 STCALL TNUV
055956,000450: 13,3061 27176 A-PCHK
055957,000451: 13,3062 07112 06620 OMEGMOON 2DEC* 2.66169947 E-8 B+23*
055958,000452:
055959,000453: 13,3064 33070 SETBANK CAF INTBANK
055960,000454: 13,3065 54006 TS BBANK
055961,000455: 13,3066 33507 CAF FORTYONE
055962,000456: 13,3067 00002 TC Q
055963,000457: 13,3070 E3,1554 EBANK= RRECTCSM
055964,000458: 13,3070 26063 INTBANK BBCON INTEGRV
055965,000459:
055966,000460: # SPECIAL PURPOSE ENTRIES TO ORBITAL INTEGRATION. THESE ROUTINES PROVIDE ENTRANCES TO INTEGRATION WITH
055967,000461: # APPROPRIATE SWITCHES SET OR CLEARED FOR THE DESIRED INTEGRATION.
055968,000462:
055969,000463: # CSMPREC AND LEMPREC PERFORM ORBIT INTEGRATION BY THE ENCKE METHOD TO THE TIME INDICATED IN TDEC1
055970,000464: # ACCELERATIONS DUE TO OBLATENESS ARE INCLUDED. NO W-MATRIX INT. IS DONE.
055971,000465: # THE PERMANENT STATE VECTOR IS NOT UPDATED.
055972,000466: # CSMCONIC AND LEMCONIC PERFORM ORBIT INTEG. BY KEPLERS METHOD TO THE TIME INDICATED IN TDEC1
055973,000467: # NO DISTURBING ACCELERATIONS ARE INCLUDED. IN THE PROGRAM FLOW THE GIVEN
055974,000468: # STATE VECTOR IS RECTIFIED BEFORE SOLUTION OF KEPLERS EQUATION
055975,000469:
055976,000470: # THE ROUTINES ASSUME THAT THE CSM (LEM) STATE VECTOR IN P-MEM IS VALID.
055977,000471: # SWITCHES SET PRIOR TO ENTRY TO THE MAIN INTEG. PROG ARE AS FOLLOWS
055978,000472: # CSMPREC CSMCONIC LEMPREC LEMCONIC
055979,000473: # VINTFLAG SET SET CLEAR CLEAR
055980,000474: # INTYPFLG CLEAR SET CLEAR SET
055981,000475: # DIM0FLAG CLEAR CLEAR CLEAR CLEAR
|
|
Page 1318
|
055983,000477:
055984,000478: # CALLING SEQUENCE
055985,000479: # L-X STORE TDEC1
055986,000480: # L CALL (STCALL TDEC1)
055987,000481: # L+1 CSMPREC (CSMCONIC, LEMPREC, LEMCONIC)
055988,000482:
055989,000483: # NORMAL EXIT TO L+2
055990,000484:
055991,000485: # SUBROUTINES CALLED
055992,000486: # INTEGRV1
055993,000487: # PRECOUT FOR CSMPREC AND LEMPREC
055994,000488: # CONICOUT FOR CSMCONIC AND LEMCONIC
055995,000489:
055996,000490: # OUTPUT - SEE PAGE 2 OF THIS LOG SECTION
055997,000491:
055998,000492: # INPUT
055999,000493: # TDEC1 TIME TO INTEGRATE TO. CSECS B-28
056000,000494:
056001,000495: 13,3071 45020 CSMPREC STQ CALL
056002,000496: 13,3072 00046 X1
056003,000497: 13,3073 27442 INTSTALL
056004,000498: 13,3074 43130 SXA,1 SET
056005,000499: 13,3075 02214 IRETURN
056006,000500: 13,3076 01474 VINTFLAG
056007,000501:
056008,000502: 13,3077 43014 IFLAGP SET CLEAR
056009,000503: 13,3100 01467 PRECIFLG
056010,000504: 13,3101 01676 DIM0FLAG
056011,000505: 13,3102 77614 CLRGO
056012,000506: 13,3103 01633 INTYPFLG
056013,000507: 13,3104 27164 INTEGRV1
056014,000508: 13,3105 45020 LEMPREC STQ CALL
056015,000509: 13,3106 00046 X1
056016,000510: 13,3107 27442 INTSTALL
056017,000511: 13,3110 43130 SXA,1 CLRGO
056018,000512: 13,3111 02214 IRETURN
056019,000513: 13,3112 01634 VINTFLAG
056020,000514: 13,3113 27077 IFLAGP
056021,000515:
056022,000516: 13,3114 45020 CSMCONIC STQ CALL
056023,000517: 13,3115 00046 X1
056024,000518: 13,3116 27442 INTSTALL
056025,000519: 13,3117 43130 SXA,1 SET
056026,000520: 13,3120 02214 IRETURN
056027,000521: 13,3121 01474 VINTFLAG
056028,000522: 13,3122 43014 IFLAGC CLEAR SETGO
056029,000523: 13,3123 01676 DIM0FLAG
056030,000524: 13,3124 01433 INTYPFLG
056031,000525: 13,3125 27164 INTEGRV1
056032,000526: 13,3126 45020 LEMCONIC STQ CALL
056033,000527: 13,3127 00046 X1
|
|
Page 1319
|
056035,000529: 13,3130 27442 INTSTALL
056036,000530: 13,3131 43130 SXA,1 CLRGO
056037,000531: 13,3132 02214 IRETURN
056038,000532: 13,3133 01634 VINTFLAG
056039,000533: 13,3134 27122 IFLAGC
056040,000534:
056041,000535: 13,3135 66214 INTEGRVS SET SSP
056042,000536: 13,3136 01467 PRECIFLG
056043,000537: 13,3137 02151 PBODY
056044,000538: 13,3140 00000 0
056045,000539: 13,3141 66214 BOF SSP
056046,000540: 13,3142 00343 MOONFLAG
056047,000541: 13,3143 27146 +3
056048,000542: 13,3144 02151 PBODY
056049,000543: 13,3145 00002 2
056050,000544: 13,3146 77220 STQ VLOAD
056051,000545: 13,3147 02214 IRETURN
056052,000546: 13,3150 11563 ZEROVEC
056053,000547: 13,3151 01521 STORE TDELTAV
056054,000548: 13,3152 35527 STCALL TNUV
056055,000549: 13,3153 23421 RECTIFY
056056,000550: 13,3154 43014 CLEAR SET
056057,000551: 13,3155 01676 DIM0FLAG
056058,000552: 13,3156 04062 NEWIFLG
056059,000553: 13,3157 77614 SETGO
056060,000554: 13,3160 04020 RPQFLAG
056061,000555: 13,3161 22363 ALOADED
056062,000556:
056063,000557: # INTEGRV IS AN ENTRY TO ORBIT INTEGRATION WHICH PERMITS THE CALLER,
056064,000558: # NORMALLY THE NAVIGATION PROGRAM, TO SET THE INTEG. FLAGS. THE ROUTINE
056065,000559: # IS ENTERED AT INTEGRV1 BY CSMPREC ET. AL. AND AT ALOADED BY INTEGRVS.
056066,000560: # THE ROUTINE SETS UP A-MEMORY IF ENTERED AT INTEGRV,1 AND SETS THE INTEG.
056067,000561: # PROGRAM FOR PRECISION OR CONIC
056068,000562:
056069,000563: # THE CALLER MUST FIRST CALL INTSTALL TO CHECK IF INTEG. IS IN USE BEFORE
056070,000564: # SETTING ANY FLAGS.
056071,000565:
056072,000566: # THE FLAGS WHICH SHOULD BE SET OR CLEARED ARE
056073,000567: # VINTFLAG (IGNORED WHEN ENTERED FROM INTEGRVS)
056074,000568: # INTYPFLG
056075,000569: # DIM0FLAG
056076,000570: # D6OR9FLG
056077,000571:
056078,000572: # CALLING SEQUENCE
056079,000573: # L-X CALL
056080,000574: # L-Y INTSTALL
056081,000575: # L-1 SET OR CLEAR ALL FOUR FLAGS. ALSO CAN SET STATEFLG IF DESIRED
056082,000576: # AND DIM0FLAG IS CLEAR.
056083,000577: # L CALL
056084,000578: # L+1 INTEGRV
056085,000579:
056086,000580: # INITIALIZATION
056087,000581: # FLAGS AS ABOVE
056088,000582: # STORE TIME TO INTEGRATE TO IN TDEC1
056089,000583:
|
|
Page 1320
|
056091,000585: # OUTPUT
056092,000586: # RATT AS
056093,000587: # VATT DEFINED
056094,000588: # TAT BEFORE
056095,000589:
056096,000590: 13,3162 77620 INTEGRV STQ
056097,000591: 13,3163 02214 IRETURN
056098,000592: 13,3164 43014 INTEGRV1 SET SET
056099,000593: 13,3165 04060 RPQFLAG
056100,000594: 13,3166 04062 NEWIFLG
056101,000595: 13,3167 77731 INTEGRV2 SSP
056102,000596: 13,3170 00053 QPRET
056103,000597: 13,3171 22363 ALOADED
056104,000598: 13,3172 52014 BON GOTO
056105,000599: 13,3173 01714 VINTFLAG
056106,000600: 13,3174 26731 PTOACSM
056107,000601: 13,3175 27004 PTOALEM
056108,000602: 11,2000 SETLOC INTINIT1
056109,000603: 11,2000 BANK
056110,000604: 11,2363 77745 ALOADED DLOAD
056111,000605: 11,2364 00041 TDEC1
056112,000606: 11,2365 01101 STORE TDEC
056113,000607: 11,2366 52014 BOFF GOTO
056114,000608: 11,2367 01753 INTYPFLG
056115,000609: 11,2370 27305 TESTLOOP
056116,000610: 11,2371 27271 RVCON
056117,000611: 13,2000 SETLOC INTINIT
056118,000612: 13,2000 BANK
056119,000613: 13,3176 45014 A-PCHK BOF CALL
056120,000614: 13,3177 00342 MIDFLAG
056121,000615: 13,3200 27205 ANDOUT # DONT MAKE ORIGIN CHANGE CHECK
056122,000616: 13,3201 23320 CHKSWTCH
056123,000617: 13,3202 45044 BPL CALL
056124,000618: 13,3203 27205 ANDOUT # NO ORIGIN CHANGE
056125,000619: 13,3204 23361 ORIGCHNG # MAKE THE SWITCH
056126,000620: 13,3205 77414 ANDOUT BOFCLR EXIT
056127,000621: 13,3206 01652 STATEFLG
056128,000622: 13,3207 27226 RECTOUT
056129,000623: 13,3210 05412 TC PHASCHNG
056130,000624: 13,3211 04022 OCT 04022
056131,000625: 13,3212 05546 TC UPFLAG # PHASE CHANGE HAS OCCURRED BETWEEN
056132,000626: 13,3213 00236 ADRES REINTFLG # INTSTALL AND INTWAKE
056133,000627: 13,3214 06006 TC INTPRET
056134,000628: 13,3215 77731 SSP
056135,000629: 13,3216 00053 QPRET
056136,000630: 13,3217 27224 PHEXIT
056137,000631: 13,3220 52014 BON GOTO
056138,000632: 13,3221 01714 VINTFLAG
056139,000633: 13,3222 26705 ATOPCSM
|
|
Page 1321
|
056141,000635: 13,3223 26760 ATOPLEM
056142,000636: 13,3224 77624 PHEXIT CALL
056143,000637: 13,3225 56750 GRP2PC
056144,000638: 13,3226 45001 RECTOUT SETPD CALL
056145,000639: 13,3227 00001 0
056146,000640: 13,3230 23421 RECTIFY
056147,000641: 13,3231 53775 VLOAD VSL*
056148,000642: 13,3232 01503 RRECT
056149,000643: 13,3233 57576 0,2
056150,000644: 13,3234 53715 PDVL VSL* # RATT TO PD0
056151,000645: 13,3235 01511 VRECT
056152,000646: 13,3236 57576 0,2
056153,000647: 13,3237 63325 PDDL PDVL # VATT TO PD6 TAT TO PD12
056154,000648: 13,3240 01517 TET
056155,000649: 13,3241 01503 RRECT
056156,000650: 13,3242 64715 PDVL PDDL*
056157,000651: 13,3243 01511 VRECT
056158,000652: 13,3244 50042 MUEARTH,2
056159,000653: 13,3245 76006 PUSH AXT,1
056160,000654: 13,3246 77765 DEC -10 B-14
056161,000655: 13,3247 76014 BON AXT,1
056162,000656: 13,3250 00303 MOONFLAG
056163,000657: 13,3251 27253 +2
056164,000658: 13,3252 77775 DEC -2 B-14
056165,000659: 13,3253 40001 INTEXIT SETPD BOV
056166,000660: 13,3254 00001 0
056167,000661: 13,3255 27256 +1
056168,000662: 13,3256 77614 CLEAR
056169,000663: 13,3257 04675 MIDAVFLG
056170,000664: 13,3260 43014 CLEAR CLEAR
056171,000665: 13,3261 04676 AVEMIDSW # ALLOW UPDATE OF DOWNLINK STATE VECTOR
056172,000666: 13,3262 01667 PRECIFLG
056173,000667: 13,3263 77535 SLOAD EXIT
056174,000668: 13,3264 02215 IRETURN
056175,000669: 13,3265 30154 CA MPAC
056176,000670: 13,3266 50120 INDEX FIXLOC
056177,000671: 13,3267 54052 TS QPRET
056178,000672: 13,3270 03457 TC INTWAKE
056179,000673:
056180,000674: # RVCON SETS UP ORBIT INTEGRATION TO DO A CONIC SOLUTION FOR POSITION AND
056181,000675: # VELOCITY FOR THE INTERVAL (TET-TDEC)
056182,000676:
056183,000677: 13,3271 45345 RVCON DLOAD DSU
056184,000678: 13,3272 01101 TDEC
056185,000679: 13,3273 01517 TET
056186,000680: 13,3274 36312 STCALL TAU.
056187,000681: 13,3275 23421 RECTIFY
056188,000682: 13,3276 77624 CALL
056189,000683: 13,3277 22372 KEPPREP
056190,000684: 13,3300 43345 DLOAD DAD
056191,000685: 13,3301 01551 TC
|
|
Page 1322
|
056193,000687: 13,3302 01517 TET
056194,000688: 13,3303 35517 STCALL TET
056195,000689: 13,3304 27226 RECTOUT
056196,000690:
|
|
Page 1323
|
056198,000692: # TESTLOOP
056199,000693:
056200,000694: 13,3305 43014 TESTLOOP BOF CLRGO
056201,000695: 13,3306 04752 QUITFLAG
056202,000696: 13,3307 27312 +3
056203,000697: 13,3310 01632 STATEFLG
056204,000698: 13,3311 27253 INTEXIT # STOP INTEGRATION
056205,000699: 13,3312 73001 +3 SETPD LXA,2
056206,000700: 13,3313 00013 10D
056207,000701: 13,3314 02150 PBODY
056208,000702: 13,3315 51575 VLOAD ABVAL
056209,000703: 13,3316 01535 RCV
056210,000704: 13,3317 43006 PUSH CLEAR # RC TO 10D
056211,000705: 13,3320 00262 MIDFLAG
056212,000706: 13,3321 50023 DSU* BMN # MIDFLAG=0 IF R G.T. RMP
056213,000707: 13,3322 67212 RME,2
056214,000708: 13,3323 27326 +3
056215,000709: 13,3324 77614 SET
056216,000710: 13,3325 00062 MIDFLAG
056217,000711: 13,3326 41345 NORFINAL DLOAD DMP
056218,000712: 13,3327 00013 10D
056219,000713: 13,3330 00043 34D
056220,000714: 13,3331 55762 SR1R DDV*
056221,000715: 13,3332 50042 MUEARTH,2
056222,000716: 13,3333 41366 SQRT DMP
056223,000717: 13,3334 23752 .3D
056224,000718: 13,3335 40442 SR3 SR4 # DT IS TRUNCATED TO A MULTIPLE
056225,000719: 13,3336 54345 DLOAD SL
056226,000720: 13,3337 00155 MPAC
056227,000721: 13,3340 20220 15D # OF 128 CSECS.
056228,000722: 13,3341 40006 PUSH BOV
056229,000723: 13,3342 27367 MAXDT
056230,000724: 13,3343 50021 BDSU BMN
056231,000725: 13,3344 27441 DT/2MAX
056232,000726: 13,3345 27367 MAXDT
056233,000727: 13,3346 45345 DT/2COMP DLOAD DSU
056234,000728: 13,3347 01101 TDEC
056235,000729: 13,3350 01517 TET
056236,000730: 13,3351 54234 RTB SL
056237,000731: 13,3352 45544 SGNAGREE
056238,000732: 13,3353 20211 8D
056239,000733: 13,3354 02314 STORE DT/2 # B-19
056240,000734: 13,3355 51400 BOV ABS
056241,000735: 13,3356 27373 GETMAXDT
056242,000736: 13,3357 50025 DSU BMN # IS TIME TO INTEG. TO GR THAN MAXTIME
056243,000737: 13,3360 00015 12D
056244,000738: 13,3361 27377 P00HCHK
056245,000739: 13,3362 75345 USEMAXDT DLOAD SIGN
056246,000740: 13,3363 00015 12D
056247,000741: 13,3364 02314 DT/2
|
|
Page 1324
|
056249,000743: 13,3365 36314 STCALL DT/2
056250,000744: 13,3366 27377 P00HCHK
056251,000745: 13,3367 65345 MAXDT DLOAD PDDL # EXCHANGE DT/2MAX WITH COMPUTED MAX.
056252,000746: 13,3370 27441 DT/2MAX
056253,000747: 13,3371 77650 GOTO
056254,000748: 13,3372 27346 DT/2COMP
056255,000749: 13,3373 77634 GETMAXDT RTB
056256,000750: 13,3374 45712 SIGNMPAC
056257,000751: 13,3375 36314 STCALL DT/2
056258,000752: 13,3376 27362 USEMAXDT
056259,000753: 13,3377 51545 P00HCHK DLOAD ABS
056260,000754: 13,3400 02314 DT/2
056261,000755: 13,3401 50025 DSU BMN
056262,000756: 13,3402 27437 DT/2MIN
056263,000757: 13,3403 27176 A-PCHK
056264,000758: 13,3404 46135 SLOAD BHIZ
056265,000759: 13,3405 01012 MODREG
056266,000760: 13,3406 27411 +3
056267,000761: 13,3407 77650 GOTO
056268,000762: 13,3410 23240 TIMESTEP
056269,000763: 13,3411 77614 BON # WAS THIS CALL VIA CSM(LEM)PREC
056270,000764: 13,3412 01707 PRECIFLG
056271,000765: 13,3413 23240 TIMESTEP # YES
056272,000766: 13,3414 45345 DLOAD DSU
056273,000767: 13,3415 02314 DT/2
056274,000768: 13,3416 00015 12D
056275,000769: 13,3417 43040 BMN BOFCLR
056276,000770: 13,3420 27176 A-PCHK
056277,000771: 13,3421 04242 NEWIFLG
056278,000772: 13,3422 23240 TIMESTEP
056279,000773: 13,3423 45345 DLOAD DSU
056280,000774: 13,3424 01101 TDEC
056281,000775: 13,3425 01517 TET
056282,000776: 13,3426 77640 BMN # NO BACKWARD INTEGRATION
056283,000777: 13,3427 27253 INTEXIT
056284,000778: 13,3430 40525 PDDL SR4
056285,000779: 13,3431 02314 DT/2 # IS 4(DT) LS (TDEC - TET)
056286,000780: 13,3432 44322 SR2R BDSU # NO
056287,000781: 13,3433 52040 BMN GOTO
056288,000782: 13,3434 27253 INTEXIT
056289,000783: 13,3435 23240 TIMESTEP
056290,000784: 13,3436 00000 01400 DT/2MIN 2DEC 3 B-20
056291,000785:
056292,000786: 13,3440 14152 00000 DT/2MAX 2DEC 4000 E2 B-20
056293,000787:
056294,000788: 13,3442 77776 INTSTALL EXIT
056295,000789: 13,3443 35021 CAF ZERO
056296,000790: 13,3444 54001 ALLSTALL TS L
056297,000791: 13,3445 30106 CA RASFLAG
056298,000792: 13,3446 50001 INDEX L
|
|
Page 1325
|
056300,000794: 13,3447 73540 MASK INTBITAB # IS THIS STALL AREA FREE
056301,000795: 13,3450 00006 EXTEND
056302,000796: 13,3451 13516 BZF OKTOGRAB # YES
056303,000797: 13,3452 50001 INDEX L
056304,000798: 13,3453 33535 CAF WAKESTAL
056305,000799: 13,3454 05175 TC JOBSLEEP
056306,000800: 13,3455 77776 INTWAKE0 EXIT
056307,000801: 13,3456 13477 TCF INTWAKE1
056308,000802:
056309,000803: 13,3457 40106 INTWAKE CS RASFLAG # IS THIS INTSTALLED ROUTINE TO BE
056310,000804: 13,3460 75011 MASK REINTBIT # RESTARTED
056311,000805: 13,3461 10000 CCS A
056312,000806: 13,3462 03477 TC INTWAKE1 # NO
056313,000807:
056314,000808: 13,3463 50120 INDEX FIXLOC
056315,000809: 13,3464 30052 CA QPRET
056316,000810: 13,3465 55055 TS TBASE2 # YES, DONT RESTART WITH SOMEONE ELSES Q
056317,000811:
056318,000812: 13,3466 05412 TC PHASCHNG
056319,000813: 13,3467 04022 OCT 04022
056320,000814:
056321,000815: 13,3470 31055 CA TBASE2
056322,000816: 13,3471 50120 INDEX FIXLOC
056323,000817: 13,3472 54052 TS QPRET
056324,000818:
056325,000819: 13,3473 35011 CAF REINTBIT
056326,000820: 13,3474 70106 MASK RASFLAG
056327,000821: 13,3475 00006 EXTEND
056328,000822: 13,3476 13521 BZF GOBAC # DONT INTWAKE IF WE CAME HERE VIA RESTART
056329,000823:
056330,000824: 13,3477 35021 INTWAKE1 CAF ZERO
056331,000825: 13,3500 54154 WAKE TS STALTEM # INDEX OF ANY STALL USER
056332,000826: 13,3501 50154 WAKE1 INDEX STALTEM
056333,000827: 13,3502 33535 CAF WAKESTAL
056334,000828: 13,3503 00004 INHINT
056335,000829: 13,3504 05201 TC JOBWAKE
056336,000830: 13,3505 10064 CCS LOCCTR
056337,000831: 13,3506 13501 TCF WAKE1 # MAY BE MORE TO WAKE UP
056338,000832: 13,3507 00051 FORTYONE DEC 41 B-14
056339,000833: 13,3510 50154 INDEX STALTEM
056340,000834: 13,3511 43540 CS INTBITAB
056341,000835: 13,3512 70106 MASK RASFLAG
056342,000836: 13,3513 54106 TS RASFLAG # RELEASE STALL AREA
056343,000837: 13,3514 00003 RELINT
056344,000838: 13,3515 13521 TCF GOBAC
056345,000839: 13,3516 50001 OKTOGRAB INDEX L # NO, WAIT UNTIL AVAILABLE
056346,000840: 13,3517 35002 CAF INTFLBIT
056347,000841: 13,3520 26106 ADS RASFLAG
056348,000842: 13,3521 06006 GOBAC TC INTPRET
056349,000843: 13,3522 77616 RVQ
|
|
Page 1326
|
056351,000845: 13,3523 77776 ERASTAL1 EXIT
056352,000846: 13,3524 35017 CAF ONE
056353,000847: 13,3525 13444 TCF ALLSTALL
056354,000848: 13,3526 77776 ERASTAL2 EXIT
056355,000849: 13,3527 35016 CAF TWO
056356,000850: 13,3530 13444 TCF ALLSTALL
056357,000851: 13,3531 35017 ERASWAK1 CAF ONE
056358,000852: 13,3532 13500 TCF WAKE
056359,000853: 13,3533 35016 ERASWAK2 CAF TWO
056360,000854: 13,3534 13500 TCF WAKE
056361,000855: 13,3535 27443 WAKESTAL CADR INTSTALL +1
056362,000856: 13,3536 27524 CADR ERASTAL1 +1
056363,000857: 13,3537 27527 CADR ERASTAL2 +1
056364,000858: 13,3540 0154 STALTEM EQUALS MPAC
056365,000859: 13,3540 20100 INTBITAB OCT 20100
056366,000860: 13,3541 10040 OCT 10040
056367,000861: 13,3542 04020 OCT 04020
056368,000862:
|
|
Page 1327
|
056370,000864: # AVETOMID
056371,000865:
056372,000866: # THIS ROUTINE PERFORMS THE TRANSITION FROM A THRUSTING PHASE TO THE COAST
056373,000867: # PHASE BY INITIALIZING THIS VEHICLES PERMANENT STATE VECTOR WITH THE
056374,000868: # VALUES LEFT BY THE AVERAGEG ROUTINE IN RN,VN,PIPTIME.
056375,000869:
056376,000870: # BEFORE THIS IS DONE THE W-MATRIX, IF ITS VALID (ORWFLAG OR RENDWFLG IS
056377,000871: # SET) IS INTEGRATED FORWARD TO PIPTIME WITH THE PRE-THRUST STATE VECTOR.
056378,000872:
056379,000873: # IN ADDITION, THE OTHER VEHICLE IS INTEGRATED (PERMANENT) TO PIPTIME.
056380,000874:
056381,000875: # FINALLY TRKMKCNT IS ZEROED
056382,000876:
056383,000877: 35,2000 SETLOC INTINIT2
056384,000878: 35,2000 BANK
056385,000879:
056386,000880: 35,3702 COUNT* $$/INTIN
056387,000881: 35,3702 43020 AVETOMID STQ BON
056388,000882: 35,3703 02317 EGRESS
056389,000883: 35,3704 02716 RENDWFLG
056390,000884: 35,3705 73760 INT/W # W-MATRIX VALID, GO INTEGRATE IT
056391,000885: 35,3706 77614 BON
056392,000886: 35,3707 01711 ORBWFLAG
056393,000887: 35,3710 73760 INT/W # W-MATRIX VALID, GO INTEGRATE IT
056394,000888:
056395,000889: 35,3711 45174 SETCOAST AXT,2 CALL # NOW MOVE PROPERLY SCALED RN,VN AND
056396,000890: 35,3712 00002 2 # PIPTIME TO INTEGRATION ERASABLES.
056397,000891: 35,3713 27442 INTSTALL
056398,000892: 35,3714 77014 BON AXT,2
056399,000893: 35,3715 00315 AMOONFLG
056400,000894: 35,3716 73720 +2
056401,000895: 35,3717 00000 0
056402,000896: 35,3720 53775 VLOAD VSR*
056403,000897: 35,3721 01171 RN
056404,000898: 35,3722 57176 0,2
056405,000899: 35,3723 01503 STORE RRECT
056406,000900: 35,3724 15535 STODL RCV
056407,000901: 35,3725 01205 PIPTIME
056408,000902: 35,3726 25517 STOVL TET
056409,000903: 35,3727 01177 VN
056410,000904: 35,3730 45057 VSR* CALL
056411,000905: 35,3731 57176 0,2
056412,000906: 35,3732 23435 MINIRECT # FINISH SETTING UP STATE VECTOR
056413,000907: 35,3733 66234 RTB SSP
056414,000908: 35,3734 26720 MOVATHIS # PUT TEMP STATE VECTOR INTO PERMANENT
056415,000909: 35,3735 01127 TRKMKCNT
056416,000910: 35,3736 00000 0
056417,000911: 35,3737 43014 SET BON
056418,000912: 35,3740 04063 CMOONFLG
|
|
Page 1328
|
056420,000914: 35,3741 00315 AMOONFLG
056421,000915: 35,3742 73745 +3
056422,000916: 35,3743 77614 CLEAR
056423,000917: 35,3744 04263 CMOONFLG
056424,000918:
056425,000919: 35,3745 71214 BON DLOAD # NOW DO LM
056426,000920: 35,3746 04307 SURFFLAG
056427,000921: 35,3747 75737 FAZAB5 # NO COASTING LM
056428,000922: 35,3750 01205 PIPTIME
056429,000923: 35,3751 34041 STCALL TDEC1
056430,000924: 35,3752 26670 SETIFLGS
056431,000925: 35,3753 45014 CLEAR CALL
056432,000926: 35,3754 01674 VINTFLAG
056433,000927: 35,3755 27162 INTEGRV
056434,000928: 35,3756 77650 GOTO
056435,000929: 35,3757 02317 EGRESS
056436,000930: 35,3760 45145 INT/W DLOAD CALL
056437,000931: 35,3761 01205 PIPTIME # INTEGRATE W THRU BURN
056438,000932: 35,3762 27442 INTSTALL
056439,000933: 35,3763 43014 SET SET
056440,000934: 35,3764 01476 DIM0FLAG # DO W-MATRIX
056441,000935: 35,3765 04476 AVEMIDSW # SO WONT CLOBBER RN,VN,PIPTIME
056442,000936: 35,3766 43014 CLEAR SET
056443,000937: 35,3767 01675 D6OR9FLG
056444,000938: 35,3770 01474 VINTFLAG
056445,000939: 35,3771 34041 STCALL TDEC1
056446,000940: 35,3772 27162 INTEGRV
056447,000941: 35,3773 77650 GOTO
056448,000942: 35,3774 73711 SETCOAST
056449,000943:
|
|
Page 1329
|
056451,000945: # MIDTOAV1
056452,000946:
056453,000947: # THIS ROUTINE INTEGRATES (PRECISION) TO THE TIME SPECIFIED IN TDEC1.
056454,000948: # IF, AT THE END OF AN INTEGRATION TIME STEP, CURRENT TIME PLUS A DELTA
056455,000949: # TIME (SEE TIMEDELT.....BASED ON THE COMPUTATUON TIME FOR ONE TIME STEP)
056456,000950: # IS GREATER THAN THE DESIRED TIME, ALARM 1703 IS SET AND THE INTEGRATION
056457,000951: # IS DONE AS IT IS FOR MIDTOAV2.
056458,000952: # RETURN IS IN BASIC TO THE RETURN ADDRESS PLUS ONE.
056459,000953:
056460,000954: # IF THE INTEGRATION IS FINISHED TO THE DESIRED TIME, RETURN IS IN BASIC
056461,000955: # TO THE RETURN ADDRESS
056462,000956:
056463,000957: # IN EITHER CASE, BEFORE RETURNING, THE EXTRAPOLATED STATE VECTOR IS TRAN
056464,000958: # FERRED FROM R,VATT TO R,VN1-PIPTIME1 IS SET TO THE FINISHING INTEGRA-
056465,000959: # TION TIME AND MPAC IS SET TO THE DELTA TIME---
056466,000960: # TAT MINUS CURRENT TIME.
056467,000961:
056468,000962: # MIDTOAV2
056469,000963:
056470,000964: # THIS ROUTINE INTEGRATES THE CSM STATE VECTOR TO CURRENT TIME PLUS
056471,000965: # INCREMENTS OF TIMEDELT SUCH THAT THE DIFFERENCE BETWEEN CURRENT TIME
056472,000966: # AND THE STATE VECTOR TIME AT THE END OF THE LAST STEP IS AT LEAST 5.6
056473,000967: # SECS.
056474,000968: # NO INPUTS ARE REQUIRED OF THE CALLER. RETURN IS IN BASIC TO THE RETURN
056475,000969: # ADDRESS WITH THE ABOVE TRANSFERS TO R,VN1-PIPTIME1-AND MPAC DONE
056476,000970:
056477,000971: 13,2000 SETLOC INTINIT
056478,000972: 13,2000 BANK
056479,000973: 13,3543 1127 EBANK= IRETURN1
056480,000974: 13,3543 45020 MIDTOAV2 STQ CALL
056481,000975: 13,3544 01127 IRETURN1
056482,000976: 13,3545 27442 INTSTALL
056483,000977: 13,3546 43145 DLOAD CLEAR
056484,000978: 13,3547 27711 TIMEDELT
056485,000979: 13,3550 04674 MID1FLAG
056486,000980: 13,3551 37732 STCALL T-TO-ADD
056487,000981: 13,3552 27567 ENTMID2
056488,000982:
056489,000983: 13,3553 45020 MIDTOAV1 STQ CALL
056490,000984: 13,3554 01127 IRETURN1
056491,000985: 13,3555 27442 INTSTALL
056492,000986: 13,3556 47014 SET RTB
056493,000987: 13,3557 04474 MID1FLAG
056494,000988: 13,3560 45510 LOADTIME
056495,000989: 13,3561 44215 DAD BDSU # INITIAL CHECK, IS TDEC1 IN THE FUTURE.
056496,000990: 13,3562 27711 TIMEDELT
056497,000991: 13,3563 00041 TDEC1
056498,000992: 13,3564 45044 BPL CALL
056499,000993: 13,3565 27573 ENTMID1
|
|
Page 1330
|
056501,000995: 13,3566 27674 NOTIME # NO SET ALARM.SWITCH TO MIDTOAV2
056502,000996:
056503,000997: 13,3567 43234 ENTMID2 RTB DAD
056504,000998: 13,3570 45510 LOADTIME
056505,000999: 13,3571 03732 T-TO-ADD
056506,001000: 13,3572 00041 STORE TDEC1
056507,001001:
056508,001002: 13,3573 45014 ENTMID1 CLEAR CALL
056509,001003: 13,3574 01676 DIM0FLAG # NO W-MATRIX
056510,001004: 13,3575 26034 THISVINT
056511,001005: 13,3576 43014 CLEAR SET
056512,001006: 13,3577 01673 INTYPFLG
056513,001007: 13,3600 04475 MIDAVFLG # LET INTEG. KNOW THE CALL IS FOR MIDTOAV.
056514,001008: 13,3601 77624 CALL
056515,001009: 13,3602 27162 INTEGRV # GO INTEGRATE
056516,001010: 13,3603 66134 SXA,2 SXA,1
056517,001011: 13,3604 03746 RTX2
056518,001012: 13,3605 03745 RTX1
056519,001013: 13,3606 67214 CLEAR SLOAD
056520,001014: 13,3607 00275 AMOONFLG
056521,001015: 13,3610 03747 RTX2
056522,001016: 13,3611 43054 BZE SET
056523,001017: 13,3612 27614 +2
056524,001018: 13,3613 00075 AMOONFLG
056525,001019: 13,3614 77775 VLOAD
056526,001020: 13,3615 00001 RATT
056527,001021: 13,3616 25232 STOVL RN1
056528,001022: 13,3617 00007 VATT
056529,001023: 13,3620 15240 STODL VN1
056530,001024: 13,3621 00015 TAT
056531,001025: 13,3622 01246 STORE PIPTIME1
056532,001026: 13,3623 77776 EXIT
056533,001027:
056534,001028: 13,3624 00004 INHINT
056535,001029: 13,3625 00006 EXTEND
056536,001030: 13,3626 40025 DCS TIME2
056537,001031: 13,3627 20155 DAS MPAC
056538,001032: 13,3630 07226 TC TPAGREE
056539,001033:
056540,001034: 13,3631 31127 CA IRETURN1
056541,001035: 13,3632 04704 TC BANKJUMP
056542,001036: 13,3633 47014 CKMID2 BOF RTB
056543,001037: 13,3634 04754 MID1FLAG
056544,001038: 13,3635 27652 MID2
056545,001039: 13,3636 45510 LOADTIME
056546,001040: 13,3637 44215 DAD BDSU
056547,001041: 13,3640 27711 TIMEDELT
056548,001042: 13,3641 01101 TDEC
056549,001043: 13,3642 45044 BPL CALL
056550,001044: 13,3643 27305 TESTLOOP # YES
|
|
Page 1331
|
056552,001046: 13,3644 27674 NOTIME
056553,001047:
056554,001048: 13,3645 43234 TIMEINC RTB DAD
056555,001049: 13,3646 45510 LOADTIME
056556,001050: 13,3647 03732 T-TO-ADD
056557,001051: 13,3650 35101 STCALL TDEC
056558,001052: 13,3651 27305 TESTLOOP
056559,001053:
056560,001054: 13,3652 45345 MID2 DLOAD DSU
056561,001055: 13,3653 01101 TDEC
056562,001056: 13,3654 01517 TET
056563,001057: 13,3655 45246 ABS DSU
056564,001058: 13,3656 27707 3CSECS
056565,001059: 13,3657 77644 BPL
056566,001060: 13,3660 27645 TIMEINC
056567,001061:
056568,001062: 13,3661 44234 RTB BDSU # SEE IF 5.6 SECS. AVAILABLE TO CALLER.
056569,001063: 13,3662 45510 LOADTIME
056570,001064: 13,3663 01517 TET
056571,001065: 13,3664 51025 DSU BPL
056572,001066: 13,3665 27713 5.6SECS
056573,001067: 13,3666 27176 A-PCHK # YES,GET OUT.
056574,001068:
056575,001069: 13,3667 43345 DLOAD DAD # NO,ADD TIMEDELT TO T-TO-ADD AND TRY
056576,001070: 13,3670 03732 T-TO-ADD # AGAIN.
056577,001071: 13,3671 27711 TIMEDELT
056578,001072: 13,3672 37732 STCALL T-TO-ADD
056579,001073: 13,3673 27645 TIMEINC
056580,001074: 13,3674 77414 NOTIME CLEAR EXIT # TOO LATE
056581,001075: 13,3675 04674 MID1FLAG
056582,001076: 13,3676 25127 INCR IRETURN1 # SET ERROR EXIT (CALLOC +2)
056583,001077: 13,3677 05650 TC ALARM # INSUFFICIENT TIME FOR INTEGRATION --
056584,001078: 13,3700 01703 OCT 1703 # TIG WILL BE SLIPPED...
056585,001079: 13,3701 06006 TC INTPRET
056586,001080: 13,3702 77745 DLOAD
056587,001081: 13,3703 27711 TIMEDELT
056588,001082: 13,3704 03732 STORE T-TO-ADD
056589,001083: 13,3705 77616 RVQ
056590,001084:
056591,001085: 13,3706 00000 00003 3CSECS 2DEC 3 B-28
056592,001086:
056593,001087: 13,3710 00000 02342 TIMEDELT 2DEC 1250 B-28
056594,001088:
056595,001089: 13,3712 00000 01060 5.6SECS 2DEC 560 B-28
056596,001090:
056597,001091: 27,2671 BANK 27
056598,001092: 27,2000 SETLOC UPDATE2
056599,001093: 27,2000 BANK
056600,001094: 27,2671 0330 EBANK= INTWAKUQ
056601,001095:
|
|
Page 1332
|
056603,001097: 27,2671 COUNT* $$/INTIN
056604,001098:
056605,001099: 27,2671 0330 INTWAKUQ = INTWAK1Q # TEMPORARY UNTIL NAME OF INTWAK1Q IS CHNG
056606,001100:
056607,001101: 27,2671 00003 INTWAKEU RELINT
056608,001102: 27,2672 00006 EXTEND
056609,001103: 27,2673 22330 QXCH INTWAKUQ # SAVE Q FOR RETURN
056610,001104:
056611,001105: 27,2674 06006 TC INTPRET
056612,001106:
056613,001107: 27,2675 53135 SLOAD BZE # IS THIS A CSM/LEM STATE VECTOR UPDATE
056614,001108: 27,2676 01502 UPSVFLAG # REQUEST. IF NOT GO TO INTWAKUP.
056615,001109: 27,2677 56736 INTWAKUP
056616,001110:
056617,001111: 27,2700 77775 VLOAD # MOVE RRECT(6) AND VRECT(6) INTO
056618,001112: 27,2701 01503 RRECT # RCV(6) AND VCV(6) RESPECTIVELY.
056619,001113: 27,2702 25535 STOVL RCV
056620,001114: 27,2703 01511 VRECT # NOW GO TO 'RECTIFY +13D' TO
056621,001115: 27,2704 77624 CALL # STORE VRECT INTO VCV AND ZERO OUT
056622,001116: 27,2705 23436 RECTIFY +13D # TDELTAV(6),TNUV(6),TC(2) AND XKEP(2)
056623,001117: 27,2706 51535 SLOAD ABS # COMPARE ABSOLUTE VALUE OF 'UPSVFLAG'
056624,001118: 27,2707 01502 UPSVFLAG # TO 'UPDATE MOON STATE VECTOR CODE'
056625,001119: 27,2710 53025 DSU BZE # TO DETERMINE WHETHER THE STATE VECTOR TO
056626,001120: 27,2711 16747 UPMNSVCD # BE UPDATED IS IN THE EARTH OR LUNAR
056627,001121: 27,2712 56717 INTWAKEM # SPHERE OF INFLUENCE.........
056628,001122: 27,2713 43174 AXT,2 CLRGO # EARTH SPHERE OF INFLUENCE.
056629,001123: 27,2714 00000 DEC 0 B-14
056630,001124: 27,2715 00223 MOONFLAG
056631,001125: 27,2716 56722 INTWAKEC
056632,001126: 27,2717 43174 INTWAKEM AXT,2 SET # LUNAR SPHERE OF INFLUENCE.
056633,001127: 27,2720 00002 DEC 2 B-14
056634,001128: 27,2721 00063 MOONFLAG
056635,001129: 27,2722 50135 INTWAKEC SLOAD BMN # COMMON CODING AFTER X2 INITIALIZED AND
056636,001130: # MOONFLAG SET (OR CLEARED).
056637,001131: 27,2723 01502 UPSVFLAG # IS THIS A REQUEST FOR A LEM OR CSM
056638,001132: 27,2724 56732 INTWAKLM # STATE VECTOR UPDATE......
056639,001133: 27,2725 77624 CALL # UPDATE CSM STATE VECTOR
056640,001134: 27,2726 26705 ATOPCSM
056641,001135:
056642,001136: 27,2727 52014 CLEAR GOTO
056643,001137: 27,2730 01671 ORBWFLAG
056644,001138: 27,2731 56734 INTWAKEX
056645,001139:
056646,001140: 27,2732 77624 INTWAKLM CALL # UPDATE LM STATE VECTOR
056647,001141: 27,2733 26760 ATOPLEM
056648,001142:
056649,001143: 27,2734 77614 INTWAKEX CLEAR
056650,001144: 27,2735 02676 RENDWFLG
056651,001145:
056652,001146: 27,2736 45131 INTWAKUP SSP CALL # REMOVE :UPDATE STATE VECTOR INDICATOR:
|
|
Page 1333
|
056654,001148: 27,2737 01502 UPSVFLAG
056655,001149: 27,2740 00000 0
056656,001150: 27,2741 27455 INTWAKE0 # RELEASE :GRAB: OF ORBIT INTEG
056657,001151: 27,2742 77776 EXIT
056658,001152:
056659,001153: 27,2743 05412 TC PHASCHNG
056660,001154: 27,2744 04026 OCT 04026
056661,001155: 27,2745 00330 TC INTWAKUQ
056662,001156:
056663,001157: 27,2746 00002 UPMNSVCD OCT 2
056664,001158: 27,2747 00000 OCT 0
056665,001159:
056666,001160: 27,2750 77420 GRP2PC STQ EXIT
056667,001161: 27,2751 03536 GRP2SVQ
056668,001162: 27,2752 05412 TC PHASCHNG
056669,001163: 27,2753 04022 OCT 04022
056670,001164: 27,2754 06006 TC INTPRET
056671,001165: 27,2755 77650 GOTO
056672,001166: 27,2756 03536 GRP2SVQ
056673,001167:
056674,001168:
056675,001169:
End of include-file INTEGRATION_INITIALIZATION.agc. Parent file is MAIN.agc