Source Code
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These source-code files are part of a reconstructed copy of Comanche 45, the
second release, though not the final mission release, of the Apollo 10
Command Module (CM) Apollo Guidance Computer (AGC) software. Comanche 45 was
preceded by Comanche 44 and followed by Comanche 45/2 (the flown release). The reconstruction
is believed to be exactly accurate, but in the absence of an actual Apollo-era
listing of Comanche 45, some explanation of the reconstruction process is needed
to insure confidence in that accuracy.
The starting point was the source code of Comanche 44 (itself previously accurately
reconstructed). Comanche 44 source code was then modified
by incorporating changes known from contemporary documentation to have been
made between revisions 44 and 45. The now-reconstructed Comanche 45 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:
There is also
a detailed commentary about the reconstruction process.
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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055608,000002: ## Copyright: Public domain.
055609,000003: ## Filename: INTEGRATION_INITIALIZATION.agc
055610,000004: ## Purpose: A section of Comanche revision 045.
055611,000005: ## It is part of the reconstructed source code for the
055612,000006: ## second release of the flight software for the Command
055613,000007: ## Module's (CM) Apollo Guidance Computer (AGC) for Apollo 10.
055614,000008: ## The code has been recreated from a copy of Comanche 055. It
055615,000009: ## has been adapted such that the resulting bugger words
055616,000010: ## exactly match those specified for Comanche 45 in NASA drawing
055617,000011: ## 2021153D, which gives relatively high confidence that the
055618,000012: ## reconstruction is correct.
055619,000013: ## Assembler: yaYUL
055620,000014: ## Contact: Ron Burkey <info@sandroid.org>.
055621,000015: ## Website: www.ibiblio.org/apollo/index.html
055622,000016: ## Mod history: 2020-12-06 MAS Created from Comanche 44.
055623,000017:
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Page 1309
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055625,000019: # 1.0 INTRODUCTION
055626,000020: # ----------------
055627,000021:
055628,000022: # FROM A USERS POINT OF VIEW, ORBITAL INTEGRATION IS ESSENTIALLY THE SAME AS THE 278 INTEGRATION
055629,000023: # PROGRAM. THE SAME ENTRANCES TO THE PROGRAM WILL BE MAINTAINED, THE SAME STALLING ROUTINE WILL BE USED AND
055630,000024: # OUTPUT WILL STILL BE VIA THE PUSHLIST. THE PRIMARY DIFFERENCES TO A USER INVOLVE THE ADDED CAPABILITY OF
055631,000025: # TERMINATING INTEGRATION AT A SPECIFIC FINAL RADIUS AND THE DIFFERENCE IN STATE VECTOR SCALING INSIDE AND OUT-
055632,000026: # SIDE THE LUNAR SPHERE OF INFLUENCE.
055633,000027:
055634,000028: # IN ORDER TO MAKE THE CSM(LEM)PREC AND CSM(LEM)CONIC ENTRANCES SIMILAR TO FLIGHT 278, THE INTEGRATION PROGRAM
055635,000029: # WILL ITSELF SET THE FINAL RADIUS (RFINAL) TO 0 SO THAT REACHING THE DESIRED TIME ONLY WILL TERMINATE
055636,000030: # INTEGRATION. THE DP REGISTER RFINAL MUST BE SET BY USERS OF INTEGRVS AND INTEGRV, AND MUST BE DONE AFTER THE
055637,000031: # CALL TC INTSTALL.
055638,000032:
055639,000033: # WHEN THE LM IS ON THE LUNAR SURFACE (INDICATED BY LUNAR SURFACE FLAG SET) CALLS TO LEMCONIC, LEMPREC, AND
055640,000034: # INTEGRV WITH VINFLAG = 0 WILL RESULT IN THE USE OF THE PLANETARY INERTIAL ORIENTATION SUBROUTINES TO PROVIDE
055641,000035: # BOTH THE LMS POSITION AND VELOCITY IN THE REFERENCE COORDINATE SYSTEM.
055642,000036: # THE PROGRAM WILL PROVIDE OUTPUT AS IF INTEGRATION WAS USED. THAT IS, THE PUSHLIST WILL BE SET AS NOTED BELOW AND
055643,000037: # THE PERMANENT STATE VECTOR UPDATED WHEN SPECIFIED BY AN INTEGRV CALL.
055644,000038:
055645,000039: # USERS OF INTEGRVS DESIRING INTEGRATION (INTYPFLG = 0) SHOULD NOTE THAT THE OBLATENESS PERTURBATION COMPUTATION
055646,000040: # IN LUNAR ORBIT IS TIME DEPENDENT. THEREFORE, THE USER SHOULD SUPPLY AN INITIAL STATE VECTOR VALID AT SOME REAL
055647,000041: # TIME AND THE DESIRED TIME (TDEC1) ALSO AT SOME REAL TIME. FOR CONIC ,,INTEGRATION,, THE USER MAY STILL USE ZERO
055648,000042: # AS THE INITIAL TIME AND DELTA TIME AS THE DESIRED TIME.
055649,000043:
055650,000044: # 2.0 GENERAL DESCRIPTION
055651,000045: # -----------------------
055652,000046:
055653,000047: # THE INTEGRATION PROGRAM OPERATES AS A CLOSED INTERPRETIVE SUBROUTINE AND PERFORMS THESE FUNCTIONS ---
055654,000048: # 1) INTEGRATES (PRECISION OR CONIC) EITHER CSM OR LM STATE VECTOR
055655,000049: # 2) INTEGRATES THE W-MATRIX
055656,000050: # 3) PERMANENT OR TEMPORARY UPDATE OF THE STATE VECTOR
055657,000051:
055658,000052: # THERE ARE SIX ENTRANCES TO THE INTEGRATION PROGRAM. FOUR OF THESE (CSMPREC, LEMPREC, CSMCONIC, LEMCONIC) SET
055659,000053: # ALL THE FLAGS REQUIRED IN THE INTEGRATION PROGRAM ITSELF TO CAUSE THE PRECISION OR CONIC INTEGRATION (KEPLER) OF
055660,000054: # THE LM OR CSM STATE VECTOR, AS THE NAMES SUGGEST. ONE ENTRANCE (INTEGRVS) PERMITS THE CALLING PROGRAM TO
055661,000055: # PROVIDE A STATE VECTOR TO BE INTEGRATED. THE CALLING PROGRAM MUST SET THE FLAGS INDICATING (1) PRECISION OR
055662,000056: # CONIC INTEGRATION, (2) IN OR OUT OF LUNAR SPHERE, (3) MIDCOURSE OR NOT, AND THE INTEGRATION PROGRAM COMPLETES
055663,000057: # THE FLAG SETTING TO BYPASS W-MATRIX INTEGRATION. THE LAST ENTRANCE (INTEGRV, USED IN GENERAL BY THE
055664,000058: # NAVIGATION PROGRAMS) PERMITS THE CALLER TO SET FIVE FLAGS (NOT MOONFLAG OR MIDFLAG) BUT NOT TO INPUT A STATE
055665,000059: # VECTOR. ANY PROGRAM WHICH CALLS INTEGRVS OR INTEGRV MUST CALL INTSTALL BEFORE IT SETS THE INTEGRATION FLAGS
055666,000060: # AND/OR STATE VECTOR.
055667,000061:
055668,000062: # THREE SETS OF 42 REGISTERS AND 2 FLAGS ARE USED FOR THE STATE VECTORS. TWO SETS, WHICH MAY NOT BE OVERLAYED, ARE
055669,000063: # USED FOR THE PERMANENT STATE VECTORS FOR THE CSM AND LM. THE THIRD SET, WHICH MAY BE OVERLAYED WHEN INTEGRATION
055670,000064: # IS NOT BEING DONE, IS USED IN THE COMPUTATIONS.
055671,000065:
055672,000066: # THE PERMANENT STATE VECTORS WILL BE PERIODICALLY UPDATED SO THAT THE VECTORS WILL NOT BE OLDER THAN 4 TIMESTEPS.
055673,000067: # THE PERMANENT STATE VECTORS WILL ALSO BE UPDATED WHENEVER THE W-MATRIX IS INTEGRATED OR WHEN A CALLER OF INTEGRV
055674,000068: # SETS STATEFLG (THE NAVIGATION PROGRAMS P20, P22.)
055675,000069:
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Page 1310
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055677,000071: # APPENDIX B OF THE USERS GUIDE LISTS THE STATE VECTOR QUANTITIES.
055678,000072:
055679,000073: # 2.1 RESTARTS
055680,000074:
055681,000075: # PHASE CHANGES WILL BE MADE IN THE INTEGRATION PROGRAM ONLY FOR THE INTEGRV ENTRANCE (I.E., WHEN THE W-MATRIX IS
055682,000076: # INTEGRATED OR PERMANENT STATE VECTOR IS UPDATED.) THE GROUP NUMBER USED WILL BE THAT FOR THE P20-25 PROGRAMS
055683,000077: # (I.E., GROUP2) SINCE THE INTEGRV ENTRANCE WILL ONLY BE USED BY THESE PROGRAMS. IF A RESTART OCCURS DURING AN
055684,000078: # INTEGRATION OF THE STATE VECTOR ONLY, THE RECOVERY WILL BE TO THE LAST PHASE IN THE CALLING PROGRAM. CALLING
055685,000079: # PROGRAMS WHICH USE THE INTEGRV OR INTEGRVS ENTRANCE OF INTEGRATION SHOULD ENSURE THAT IF PHASE CHANGING IS DONE
055686,000080: # THAT IT IS PRIOR TO SETTING THE INTEGRATION INPUTS IN THE PUSHLIST.
055687,000081: # THIS IS BECAUSE THE PUSHLIST IS LOST DURING A RESTART.
055688,000082:
055689,000083: # 2.2 SCALING
055690,000084:
055691,000085: # THE INTEGRATION ROUTINE WILL MAINTAIN THE PERMANENT MEMORY STATE VECTORS IN THE SCALING AND UNITS DEFINED IN
055692,000086: # APPENDIX B OF THE USERS GUIDE. THE SCALING OF THE OUTPUT POSITION VECTOR DEPENDS ON THE ORIGIN OF THE COORDINATE
055693,000087: # SYSTEM AT THE DESIRED INTEGRATION TIME. THE COORDINATE SYSTEM TRANSFORMATION WILL BE DONE AUTOMATICALLY ON
055694,000088: # MULTIPLE TIMESTEP ENCKE INTEGRATION ONLY. THUS IT IS POSSIBLE TO HAVE OUTPUT FROM SUCCESSIVE INTEGRATIONS IN
055695,000089: # DIFFERENT SCALING.
055696,000090: # HOWEVER, RATT, VATT WILL ALWAYS BE SCALED THE SAME.
055697,000091:
055698,000092: # 3.0 INPUT/OUTPUT
055699,000093: # ----------------
055700,000094:
055701,000095: # PROGRAM INPUTS ARE THE FLAGS DESCRIBED IN APPENDIX A AND THE PERMANENT STATE VECTOR QUANTITIES DESCRIBED IN AP-
055702,000096: # PENDIX B OF THE USERS GUIDE, PLUS THE DESIRED TIME TO INTEGRATE TO IN TDEC1 (A PUSH LIST LOCATION).
055703,000097: # FOR INTEGRVS, THE RCV,VCV,TET OF THE TEMPORARY STATE VECTOR MUST BE SET, PLUS MOONFLAG AND MIDFLAG
055704,000098:
055705,000099: # FOR SIMULATION THE FOLLOWING QUANTITIES MUST BE PRESET ---
055706,000100: # EARTH MOON
055707,000101: # 29 27
055708,000102: # RRECTCSM(LEM) - RECTIFIED POSITION VECTOR METERS 2 2
055709,000103:
055710,000104: # 7 5
055711,000105: # VRECTCSM(LEM) - RECTIFIED VELOCITY VECTOR M/CSEC 2 2
055712,000106:
055713,000107: # 28 28
055714,000108: # TETCSM(LEM) - TIME STATE VECTOR IS VALID CSEC 2 2
055715,000109: # CUSTOMARILY 0, BUT NOTE LUNAR
055716,000110: # ORBIT DEPENDENCE ON REAL TIME.
055717,000111:
055718,000112: # 22 18
055719,000113: # DELTAVCSM(LEM) - POSITION DEVIATION METERS 2 2
055720,000114: # 0 IF TCCSM(LEM) = 0
055721,000115:
055722,000116: # 3 -1
055723,000117: # NUVCSM(LEM) - VELOCITY DEVIATION M/CSEC 2 2
055724,000118: # 0 IF TCCSM(LEM) = 0
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Page 1311
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055726,000120: # 29 27
055727,000121: # RCVCSM(LEM) - CONIC POSITION METERS 2 2
055728,000122: # EQUALS RRECTCSM(LEM) IF
055729,000123: # TCCSM(LEM) = 0
055730,000124:
055731,000125: # 7 5
055732,000126: # VCVCSM(LEM) - CONIC VELOCITY M/CSEC 2 2
055733,000127: # EQUALS VRECTCSM(LEM) IF
055734,000128: # TCCSM(LEM) = 0
055735,000129:
055736,000130: # 28 28
055737,000131: # TCCSM(LEM) - TIME SINCE RECTIFICATION CSECS 2 2
055738,000132: # CUSTOMARILY 0
055739,000133:
055740,000134: # 1/2 17 16
055741,000135: # XKEPCSM(LEM) - ROOT OF KEPLERS EQUATION M 2 2
055742,000136: # 0 IF TCCSM(LEM) = 0
055743,000137:
055744,000138: # CMOONFLG - PERMANENT FLAGS CORRESPONDING 0 0
055745,000139: # CMIDFLAG TO MOONFLAG AND MIDFLAG 0,1 0,1
055746,000140: # LMOONFLG C = CSM, L = LM 0 0
055747,000141: # LMIDFLG 0,1 0,1
055748,000142:
055749,000143: # SURFFLAG - LUNAR SURFACE FLAG 0,1 0,1
055750,000144:
055751,000145: # IN ADDITION, IF (L)CMIDFLAG IS SET, THE INITIAL INPUT VALUES FOR LUNAR
055752,000146: # SOLAR EPHEMERIDES SUBROUTINE AND PLANETARY INERTIAL ORIENTATION SUB-
055753,000147: # ROUTINE MUST BE PRESET.
055754,000148:
055755,000149: # OUTPUT
055756,000150: # AFTER EVERY CALL TO INTEGRATION
055757,000151: # EARTH MOON
055758,000152: # 29 29
055759,000153: # 0D RATT POSITION METERS 2 2
055760,000154:
055761,000155: # 7 7
055762,000156: # 6D VATT VELOCITY M/CSEC 2 2
055763,000157:
055764,000158: # 28 28
055765,000159: # 12D TAT TIME 2 2
055766,000160:
055767,000161: # 29 27
055768,000162: # 14D RATT1 POSITION METERS 2 2
055769,000163:
055770,000164: # 7 5
055771,000165: # 20D VATT1 VELOCITY M/CSEC 2 2
055772,000166:
055773,000167: # 3 2 36 30
055774,000168: # 26D MU(P) MU M /CS 2 2
055775,000169:
055776,000170: # X1 MUTABLE ENTRY -2 -10D
055777,000171:
055778,000172: # X2 COORDINT
055779,000173: # X2 COORDINATE SYSTEM ORIGEN 0 2
055780,000174: # (THIS, NOT MOONFLAG, SHOULD BE
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Page 1312
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055782,000176: # USED TO DETERMINE ORIGIN.)
055783,000177:
055784,000178: # IN ADDITION TO THE ABOVE, THE PERMANENT STATE VECTOR IS UPDATED WHENEVER
055785,000179: # STATEFLG WAS SET AND WHENEVER A W-MATRIX IS TO BE INTEGRATED. THE PUSH
055786,000180: # COUNTER IS SET TO 0 AND OVERFLOW IS CLEARED BEFORE RETURNING TO THE
055787,000181: # CALLING PROGRAM.
055788,000182:
055789,000183: # 4.0 CALLING SEQUENCES AND SAMPLE CODE
055790,000184: # -------------------------------------
055791,000185:
055792,000186: # A) PRECISION ORBITAL INTEGRATION. CSMPREC, LEMPREC ENTRANCES
055793,000187: # L-X STORE TIME TO 95T5791T5 T 95 PUS L9ST (T4531)
055794,000188: # L CALL
055795,000189: # L+1 CSMPREC (OR LEMPREC)
055796,000190: # L+2 RETURN
055797,000191: # INPUT 28
055798,000192: # TDEC1 (PD 32D) TIME TO INTEGRATE TO...CENTISECONDS SCALED 2
055799,000193: # OUTPUT
055800,000194: # THE DATA LISTED IN SECTION 3.0 PLUS
055801,000195: # RQVV POSITION VECTOR OF VEHICLE WITH RESPECT TO SECONDARY
055802,000196: # BODY... METERS B-29 ONLY IF MIDFLAG = DIMOFLAG = 1
055803,000197: # B) CONIC INTEGRATION. CSMCONIC, LEMCONIC ENTRANCES
055804,000198: # L-X STORE TIME IN PUSH LIST (TDEC1)
055805,000199: # L CALL
055806,000200: # L+1 CSMCONIC (OR LEMCONIC)
055807,000201: # INPUT/OUTPUT
055808,000202: # SAME AS PRECISION INTEGRATION, EXCEPT RQVV NOT SET
055809,000203: # C) INTEGRATE GIVEN STATE VECTOR. INTEGRVS ENTRANCE
055810,000204: # CALL
055811,000205: # INTSTALL
055812,000206: # VLOAD
055813,000207: # POSITION VECTOR
055814,000208: # STOVL RCV
055815,000209: # VELOCITY VECTOR
055816,000210: # STODL VCV
055817,000211: # TIME STATE VECTOR VALID
055818,000212: # STODL TET
055819,000213: # FINAL RADIUS
055820,000214: # STORE RFINAL
055821,000215: # SET(CLEAR) SET(CLEAR)
055822,000216: # INTYPFLAG
055823,000217: # MOONFLAG
055824,000218: # SET(CLEAR) DLOAD
055825,000219: # DESIRED TIME
055826,000220: # STCALL TDEC1
055827,000221: # INTEGRVS
055828,000222: # INPUT
055829,000223: # RCV POSITION VECTOR METERS
055830,000224: # VCV VELOCITY VECTOR M/CSEC
055831,000225: # TET TIME OF STATE VECTOR (MAY = 0) CSEC B-28
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Page 1313
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055833,000227: # TDEC1 TIME TO INTEGRATE TO CSEC B-28 (PD 32D)
055834,000228: # (MAY BE INCREMENT IF TET=0)
055835,000229: # OUTPUT
055836,000230: # SAME AS FOR PRECISION OR CONIC INTEGRATION,
055837,000231: # DEPENDING ON INTYPFLG.
055838,000232: # D) INTEGRATE STATE VECTOR. INTGRV ENTRANCE
055839,000233: # L-X STORE TIME IN PUSH LIST (TDEC1) (MAY BE DONE AFTER CALL TO INTSTALL)
055840,000234: # L-8 CALL
055841,000235: # L-7
055842,000236: # L-6 SET(CLEAR) SET(CLEAR)
055843,000237: # L-5 VINTFLAG 1=CSM, 0=LM
055844,000238: # L-4 INTYPFLAG 1=CONIC, 0=PRECISION
055845,000239: # L-3 SET(CLEAR) SET(CLEAR)
055846,000240: # L-2 DIMOFLAG 1=W-MATRIX, 0=NO W-MATRIX
055847,000241: # L-1 D6OR9FLG 1=9X9, 0=6X6
055848,000242: # L SET DLOAD
055849,000243: # L+1 STATEFLG DESIRE PERMANENT UPDATE
055850,000244: # L+2 FINAL RAD. OF STATE VECTOR
055851,000245: # L+3 STCALL RFINAL
055852,000246: # L+4 INTEGRV
055853,000247: # L CALL NORMAL USE -- WILL UPDATE STATE
055854,000248: # L+1 INTEGRV VECTOR IF DIMOFLAG=1. (STATEFLG IS
055855,000249: # L+2 RETURN ALWAYS RESET IN INTEGRATION AFTER
055856,000250: # IT IS USED.)
055857,000251: # INPUT
055858,000252: # TDEC1 (PD 32D) TIME TO INTEGRATE TO CSEC B-28
055859,000253: # OUTPUT
055860,000254: # SAME AS FOR PRECISION OR CONIC INTEGRATION
055861,000255: # THE PROGRAM WILL SET MOONFLAG, MIDFLAG DEPENDING ON
055862,000256: # THE PERMANENT STATE VECTOR REPRESENTATION.
055863,000257:
055864,000258: 11,2363 BANK 11
055865,000259: 13,2000 SETLOC INTINIT
055866,000260: 13,2000 BANK
055867,000261: 13,2627 E3,1554 EBANK= RRECTCSM
055868,000262: 13,2627 COUNT 13/INTIN
055869,000263:
055870,000264: 13,2627 05412 STATEINT TC PHASCHNG
055871,000265: 13,2630 00052 OCT 00052
055872,000266: 13,2631 35061 CAF PRIO5
055873,000267: 13,2632 05147 TC FINDVAC
055874,000268: 13,2633 E3,1554 EBANK= RRECTCSM
055875,000269: 13,2633 02636 26063 2CADR STATINT1
055876,000270:
055877,000271: 13,2635 05324 TC TASKOVER
055878,000272: 13,2636 06006 STATINT1 TC INTPRET
055879,000273: 13,2637 47014 BON RTB
055880,000274: 13,2640 04712 QUITFLAG
055881,000275: 13,2641 26677 NOINT # NO STATEINT IF V96
055882,000276: 13,2642 45510 LOADTIME
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Page 1314
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055884,000278: 13,2643 00041 STORE TDEC1
055885,000279: 13,2644 45014 CLEAR CALL
055886,000280: 13,2645 04274 V96ONFLG
055887,000281: 13,2646 27442 INTSTALL
055888,000282: 13,2647 45014 SET CALL
055889,000283: 13,2650 01076 NODOFLAG
055890,000284: 13,2651 26670 SETIFLGS
055891,000285: 13,2652 77650 GOTO
055892,000286: 13,2653 26000 STATEUP
055893,000287: 13,2654 00003 25140 600SECS 2DEC 60000 B-28
055894,000288:
055895,000289: 13,2656 77414 ENDINT CLEAR EXIT
055896,000290: 13,2657 01672 STATEFLG
055897,000291: 13,2660 05412 TC PHASCHNG
055898,000292: 13,2661 20032 OCT 20032
055899,000293: 13,2662 00006 EXTEND
055900,000294: 13,2663 32655 DCA 600SECS
055901,000295: 13,2664 05342 TC LONGCALL
055902,000296: 13,2665 E3,1554 EBANK= RRECTHIS
055903,000297: 13,2665 02627 26063 2CADR STATEINT
055904,000298:
055905,000299: 13,2667 05217 TC ENDOFJOB
055906,000300: 13,2670 43014 SETIFLGS SET CLEAR
055907,000301: 13,2671 01472 STATEFLG
055908,000302: 13,2672 01673 INTYPFLG
055909,000303: 13,2673 43014 CLEAR CLEAR
055910,000304: 13,2674 01676 DIM0FLAG
055911,000305: 13,2675 01675 D6OR9FLG
055912,000306: 13,2676 77616 RVQ
055913,000307: 13,2677 77776 NOINT EXIT
055914,000308: 13,2700 05412 TC PHASCHNG
055915,000309: 13,2701 00002 OCT 2
055916,000310:
055917,000311: 13,2702 05560 TC DOWNFLAG
055918,000312: 13,2703 00221 ADRES QUITFLAG
055919,000313:
055920,000314: 13,2704 05217 TC ENDOFJOB
055921,000315:
055922,000316: # ATOPCSM TRANSFERS RRECT TO RRECT +41 TO RRECTCSM TO RRECTCSM +41
055923,000317:
055924,000318: # CALLING SEQUENCE
055925,000319: # L CALL
055926,000320: # L+1 ATOPCSM
055927,000321:
055928,000322: # NORMAL EXIT AT L+2
055929,000323:
055930,000324: 13,2705 47020 ATOPCSM STQ RTB
055931,000325: 13,2706 00051 S2
055932,000326: 13,2707 26720 MOVEACSM
055933,000327: 13,2710 45014 SET CALL
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Page 1315
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055935,000329: 13,2711 04063 CMOONFLG
055936,000330: 13,2712 20237 SVDWN1
055937,000331: 13,2713 43014 BON CLRGO
055938,000332: 13,2714 00303 MOONFLAG
055939,000333: 13,2715 00051 S2
055940,000334: 13,2716 04223 CMOONFLG
055941,000335: 13,2717 00051 S2
055942,000336: 13,2720 03064 MOVEACSM TC SETBANK
055943,000337: 13,2721 55500 TS DIFEQCNT # INITIALIZE INDEX
055944,000338: 13,2722 51500 INDEX DIFEQCNT
055945,000339: 13,2723 31502 CA RRECT
055946,000340: 13,2724 51500 INDEX DIFEQCNT
055947,000341: 13,2725 55554 TS RRECTCSM
055948,000342: 13,2726 11500 CCS DIFEQCNT # IS TRANSFER COMPLETE
055949,000343: 13,2727 12721 TCF MOVEACSM +1 # NO-LOOP
055950,000344: 13,2730 06030 TC DANZIG # COMPLETE - RETURN
055951,000345:
055952,000346: # PTOACSM TRANSFERS RRECTCSM TO RRECTCSM +41 TO RRECT TO RRECT +41
055953,000347:
055954,000348: # CALLING SEQUENCE
055955,000349: # L CALL
055956,000350: # PTOACSM
055957,000351:
055958,000352: # NORMAL EXIT AT L+2
055959,000353:
055960,000354: 13,2731 43034 PTOACSM RTB BON
055961,000355: 13,2732 26747 MOVEPCSM
055962,000356: 13,2733 04303 CMOONFLG
055963,000357: 13,2734 26742 SETMOON
055964,000358: 13,2735 66214 CLRMOON CLEAR SSP
055965,000359: 13,2736 00263 MOONFLAG
055966,000360: 13,2737 02151 PBODY
055967,000361: 13,2740 00000 0
055968,000362: 13,2741 77616 RVQ
055969,000363: 13,2742 66214 SETMOON SET SSP
055970,000364: 13,2743 00063 MOONFLAG
055971,000365: 13,2744 02151 PBODY
055972,000366: 13,2745 00002 2
055973,000367: 13,2746 77616 RVQ
055974,000368: 13,2747 03064 MOVEPCSM TC SETBANK
055975,000369: 13,2750 55500 TS DIFEQCNT
055976,000370: 13,2751 51500 INDEX DIFEQCNT
055977,000371: 13,2752 31554 CA RRECTCSM
055978,000372: 13,2753 51500 INDEX DIFEQCNT
055979,000373: 13,2754 55502 TS RRECT
055980,000374: 13,2755 11500 CCS DIFEQCNT
055981,000375: 13,2756 12750 TCF MOVEPCSM +1
055982,000376: 13,2757 06030 TC DANZIG
055983,000377:
|
|
Page 1316
|
055985,000379: # ATOPLEM TRANSFERS RRECT TO RRECT +41 TO RRECTLEM TO RRECTLEM +41
055986,000380: 13,2760 47020 ATOPLEM STQ RTB
055987,000381: 13,2761 00051 S2
055988,000382: 13,2762 26773 MOVEALEM
055989,000383: 13,2763 45014 SET CALL
055990,000384: 13,2764 04064 LMOONFLG
055991,000385: 13,2765 20263 SVDWN2
055992,000386: 13,2766 43014 BON CLRGO
055993,000387: 13,2767 00303 MOONFLAG
055994,000388: 13,2770 00051 S2
055995,000389: 13,2771 04224 LMOONFLG
055996,000390: 13,2772 00051 S2
055997,000391: 13,2773 03064 MOVEALEM TC SETBANK
055998,000392: 13,2774 55500 TS DIFEQCNT
055999,000393: 13,2775 51500 INDEX DIFEQCNT
056000,000394: 13,2776 31502 CA RRECT
056001,000395: 13,2777 51500 INDEX DIFEQCNT
056002,000396: 13,3000 55626 TS RRECTLEM
056003,000397: 13,3001 11500 CCS DIFEQCNT
056004,000398: 13,3002 12774 TCF MOVEALEM +1
056005,000399: 13,3003 06030 TC DANZIG
056006,000400:
056007,000401: # PTOALEM TRANSFERS RRECTLEM TO RRECTLEM +41 TO RRECT TO RRECT +41
056008,000402:
056009,000403: 13,3004 47014 PTOALEM BON RTB
056010,000404: 13,3005 04307 SURFFLAG
056011,000405: 13,3006 27025 USEPIOS
056012,000406: 13,3007 27014 MOVEPLEM
056013,000407: 13,3010 52014 BON GOTO
056014,000408: 13,3011 04304 LMOONFLG
056015,000409: 13,3012 26742 SETMOON
056016,000410: 13,3013 26735 CLRMOON
056017,000411: 13,3014 03064 MOVEPLEM TC SETBANK
056018,000412: 13,3015 55500 TS DIFEQCNT
056019,000413: 13,3016 51500 INDEX DIFEQCNT
056020,000414: 13,3017 31626 CA RRECTLEM
056021,000415: 13,3020 51500 INDEX DIFEQCNT
056022,000416: 13,3021 55502 TS RRECT
056023,000417: 13,3022 11500 CCS DIFEQCNT
056024,000418: 13,3023 13015 TCF MOVEPLEM +1
056025,000419: 13,3024 06030 TC DANZIG
056026,000420:
056027,000421: 13,3025 77201 USEPIOS SETPD VLOAD
056028,000422: 13,3026 00001 0
056029,000423: 13,3027 02026 RLS
056030,000424: 13,3030 41525 PDDL PUSH
056031,000425: 13,3031 00041 TDEC1
|
|
Page 1317
|
056033,000427: 13,3032 15517 STODL TET
056034,000428: 13,3033 27755 5/8
056035,000429: 13,3034 77624 CALL
056036,000430: 13,3035 55344 RP-TO-R
056037,000431: 13,3036 25535 STOVL RCV
056038,000432: 13,3037 11555 ZUNIT
056039,000433: 13,3040 14001 STODL 0D
056040,000434: 13,3041 01517 TET
056041,000435: 13,3042 14007 STODL 6D
056042,000436: 13,3043 27755 5/8
056043,000437: 13,3044 45014 SET CALL # NEEDED FOR SETTING X1 ON EXIT
056044,000438: 13,3045 00063 MOONFLAG
056045,000439: 13,3046 55344 RP-TO-R
056046,000440: 13,3047 74235 VXV VXSC
056047,000441: 13,3050 01535 RCV
056048,000442: 13,3051 27063 OMEGMOON
056049,000443: 13,3052 25543 STOVL VCV
056050,000444: 13,3053 11563 ZEROVEC
056051,000445: 13,3054 01521 STORE TDELTAV
056052,000446: 13,3055 67174 AXT,2 SXA,2
056053,000447: 13,3056 00002 2
056054,000448: 13,3057 02150 PBODY
056055,000449: 13,3060 35527 STCALL TNUV
056056,000450: 13,3061 27176 A-PCHK
056057,000451: 13,3062 07112 06620 OMEGMOON 2DEC* 2.66169947 E-8 B+23*
056058,000452:
056059,000453: 13,3064 33070 SETBANK CAF INTBANK
056060,000454: 13,3065 54006 TS BBANK
056061,000455: 13,3066 33507 CAF FORTYONE
056062,000456: 13,3067 00002 TC Q
056063,000457: 13,3070 E3,1554 EBANK= RRECTCSM
056064,000458: 13,3070 26063 INTBANK BBCON INTEGRV
056065,000459:
056066,000460: # SPECIAL PURPOSE ENTRIES TO ORBITAL INTEGRATION. THESE ROUTINES PROVIDE ENTRANCES TO INTEGRATION WITH
056067,000461: # APPROPRIATE SWITCHES SET OR CLEARED FOR THE DESIRED INTEGRATION.
056068,000462:
056069,000463: # CSMPREC AND LEMPREC PERFORM ORBIT INTEGRATION BY THE ENCKE METHOD TO THE TIME INDICATED IN TDEC1
056070,000464: # ACCELERATIONS DUE TO OBLATENESS ARE INCLUDED. NO W-MATRIX INT. IS DONE.
056071,000465: # THE PERMANENT STATE VECTOR IS NOT UPDATED.
056072,000466: # CSMCONIC AND LEMCONIC PERFORM ORBIT INTEG. BY KEPLERS METHOD TO THE TIME INDICATED IN TDEC1
056073,000467: # NO DISTURBING ACCELERATIONS ARE INCLUDED. IN THE PROGRAM FLOW THE GIVEN
056074,000468: # STATE VECTOR IS RECTIFIED BEFORE SOLUTION OF KEPLERS EQUATION
056075,000469:
056076,000470: # THE ROUTINES ASSUME THAT THE CSM (LEM) STATE VECTOR IN P-MEM IS VALID.
056077,000471: # SWITCHES SET PRIOR TO ENTRY TO THE MAIN INTEG. PROG ARE AS FOLLOWS
056078,000472: # CSMPREC CSMCONIC LEMPREC LEMCONIC
056079,000473: # VINTFLAG SET SET CLEAR CLEAR
056080,000474: # INTYPFLG CLEAR SET CLEAR SET
056081,000475: # DIM0FLAG CLEAR CLEAR CLEAR CLEAR
|
|
Page 1318
|
056083,000477:
056084,000478: # CALLING SEQUENCE
056085,000479: # L-X STORE TDEC1
056086,000480: # L CALL (STCALL TDEC1)
056087,000481: # L+1 CSMPREC (CSMCONIC, LEMPREC, LEMCONIC)
056088,000482:
056089,000483: # NORMAL EXIT TO L+2
056090,000484:
056091,000485: # SUBROUTINES CALLED
056092,000486: # INTEGRV1
056093,000487: # PRECOUT FOR CSMPREC AND LEMPREC
056094,000488: # CONICOUT FOR CSMCONIC AND LEMCONIC
056095,000489:
056096,000490: # OUTPUT - SEE PAGE 2 OF THIS LOG SECTION
056097,000491:
056098,000492: # INPUT
056099,000493: # TDEC1 TIME TO INTEGRATE TO. CSECS B-28
056100,000494:
056101,000495: 13,3071 45020 CSMPREC STQ CALL
056102,000496: 13,3072 00046 X1
056103,000497: 13,3073 27442 INTSTALL
056104,000498: 13,3074 43130 SXA,1 SET
056105,000499: 13,3075 02214 IRETURN
056106,000500: 13,3076 01474 VINTFLAG
056107,000501:
056108,000502: 13,3077 43014 IFLAGP SET CLEAR
056109,000503: 13,3100 01467 PRECIFLG
056110,000504: 13,3101 01676 DIM0FLAG
056111,000505: 13,3102 77614 CLRGO
056112,000506: 13,3103 01633 INTYPFLG
056113,000507: 13,3104 27164 INTEGRV1
056114,000508: 13,3105 45020 LEMPREC STQ CALL
056115,000509: 13,3106 00046 X1
056116,000510: 13,3107 27442 INTSTALL
056117,000511: 13,3110 43130 SXA,1 CLRGO
056118,000512: 13,3111 02214 IRETURN
056119,000513: 13,3112 01634 VINTFLAG
056120,000514: 13,3113 27077 IFLAGP
056121,000515:
056122,000516: 13,3114 45020 CSMCONIC STQ CALL
056123,000517: 13,3115 00046 X1
056124,000518: 13,3116 27442 INTSTALL
056125,000519: 13,3117 43130 SXA,1 SET
056126,000520: 13,3120 02214 IRETURN
056127,000521: 13,3121 01474 VINTFLAG
056128,000522: 13,3122 43014 IFLAGC CLEAR SETGO
056129,000523: 13,3123 01676 DIM0FLAG
056130,000524: 13,3124 01433 INTYPFLG
056131,000525: 13,3125 27164 INTEGRV1
056132,000526: 13,3126 45020 LEMCONIC STQ CALL
056133,000527: 13,3127 00046 X1
|
|
Page 1319
|
056135,000529: 13,3130 27442 INTSTALL
056136,000530: 13,3131 43130 SXA,1 CLRGO
056137,000531: 13,3132 02214 IRETURN
056138,000532: 13,3133 01634 VINTFLAG
056139,000533: 13,3134 27122 IFLAGC
056140,000534:
056141,000535: 13,3135 66214 INTEGRVS SET SSP
056142,000536: 13,3136 01467 PRECIFLG
056143,000537: 13,3137 02151 PBODY
056144,000538: 13,3140 00000 0
056145,000539: 13,3141 66214 BOF SSP
056146,000540: 13,3142 00343 MOONFLAG
056147,000541: 13,3143 27146 +3
056148,000542: 13,3144 02151 PBODY
056149,000543: 13,3145 00002 2
056150,000544: 13,3146 77220 STQ VLOAD
056151,000545: 13,3147 02214 IRETURN
056152,000546: 13,3150 11563 ZEROVEC
056153,000547: 13,3151 01521 STORE TDELTAV
056154,000548: 13,3152 35527 STCALL TNUV
056155,000549: 13,3153 23421 RECTIFY
056156,000550: 13,3154 43014 CLEAR SET
056157,000551: 13,3155 01676 DIM0FLAG
056158,000552: 13,3156 04062 NEWIFLG
056159,000553: 13,3157 77614 SETGO
056160,000554: 13,3160 04020 RPQFLAG
056161,000555: 13,3161 22363 ALOADED
056162,000556:
056163,000557: # INTEGRV IS AN ENTRY TO ORBIT INTEGRATION WHICH PERMITS THE CALLER,
056164,000558: # NORMALLY THE NAVIGATION PROGRAM, TO SET THE INTEG. FLAGS. THE ROUTINE
056165,000559: # IS ENTERED AT INTEGRV1 BY CSMPREC ET. AL. AND AT ALOADED BY INTEGRVS.
056166,000560: # THE ROUTINE SETS UP A-MEMORY IF ENTERED AT INTEGRV,1 AND SETS THE INTEG.
056167,000561: # PROGRAM FOR PRECISION OR CONIC
056168,000562:
056169,000563: # THE CALLER MUST FIRST CALL INTSTALL TO CHECK IF INTEG. IS IN USE BEFORE
056170,000564: # SETTING ANY FLAGS.
056171,000565:
056172,000566: # THE FLAGS WHICH SHOULD BE SET OR CLEARED ARE
056173,000567: # VINTFLAG (IGNORED WHEN ENTERED FROM INTEGRVS)
056174,000568: # INTYPFLG
056175,000569: # DIM0FLAG
056176,000570: # D6OR9FLG
056177,000571:
056178,000572: # CALLING SEQUENCE
056179,000573: # L-X CALL
056180,000574: # L-Y INTSTALL
056181,000575: # L-1 SET OR CLEAR ALL FOUR FLAGS. ALSO CAN SET STATEFLG IF DESIRED
056182,000576: # AND DIM0FLAG IS CLEAR.
056183,000577: # L CALL
056184,000578: # L+1 INTEGRV
056185,000579:
056186,000580: # INITIALIZATION
056187,000581: # FLAGS AS ABOVE
056188,000582: # STORE TIME TO INTEGRATE TO IN TDEC1
056189,000583:
|
|
Page 1320
|
056191,000585: # OUTPUT
056192,000586: # RATT AS
056193,000587: # VATT DEFINED
056194,000588: # TAT BEFORE
056195,000589:
056196,000590: 13,3162 77620 INTEGRV STQ
056197,000591: 13,3163 02214 IRETURN
056198,000592: 13,3164 43014 INTEGRV1 SET SET
056199,000593: 13,3165 04060 RPQFLAG
056200,000594: 13,3166 04062 NEWIFLG
056201,000595: 13,3167 77731 INTEGRV2 SSP
056202,000596: 13,3170 00053 QPRET
056203,000597: 13,3171 22363 ALOADED
056204,000598: 13,3172 52014 BON GOTO
056205,000599: 13,3173 01714 VINTFLAG
056206,000600: 13,3174 26731 PTOACSM
056207,000601: 13,3175 27004 PTOALEM
056208,000602: 11,2000 SETLOC INTINIT1
056209,000603: 11,2000 BANK
056210,000604: 11,2363 77745 ALOADED DLOAD
056211,000605: 11,2364 00041 TDEC1
056212,000606: 11,2365 01101 STORE TDEC
056213,000607: 11,2366 52014 BOFF GOTO
056214,000608: 11,2367 01753 INTYPFLG
056215,000609: 11,2370 27305 TESTLOOP
056216,000610: 11,2371 27271 RVCON
056217,000611: 13,2000 SETLOC INTINIT
056218,000612: 13,2000 BANK
056219,000613: 13,3176 45014 A-PCHK BOF CALL
056220,000614: 13,3177 00342 MIDFLAG
056221,000615: 13,3200 27205 ANDOUT # DONT MAKE ORIGIN CHANGE CHECK
056222,000616: 13,3201 23320 CHKSWTCH
056223,000617: 13,3202 45044 BPL CALL
056224,000618: 13,3203 27205 ANDOUT # NO ORIGIN CHANGE
056225,000619: 13,3204 23361 ORIGCHNG # MAKE THE SWITCH
056226,000620: 13,3205 77414 ANDOUT BOFCLR EXIT
056227,000621: 13,3206 01652 STATEFLG
056228,000622: 13,3207 27226 RECTOUT
056229,000623: 13,3210 05412 TC PHASCHNG
056230,000624: 13,3211 04022 OCT 04022
056231,000625: 13,3212 05546 TC UPFLAG # PHASE CHANGE HAS OCCURRED BETWEEN
056232,000626: 13,3213 00236 ADRES REINTFLG # INTSTALL AND INTWAKE
056233,000627: 13,3214 06006 TC INTPRET
056234,000628: 13,3215 77731 SSP
056235,000629: 13,3216 00053 QPRET
056236,000630: 13,3217 27224 PHEXIT
056237,000631: 13,3220 52014 BON GOTO
056238,000632: 13,3221 01714 VINTFLAG
056239,000633: 13,3222 26705 ATOPCSM
|
|
Page 1321
|
056241,000635: 13,3223 26760 ATOPLEM
056242,000636: 13,3224 77624 PHEXIT CALL
056243,000637: 13,3225 56750 GRP2PC
056244,000638: 13,3226 45001 RECTOUT SETPD CALL
056245,000639: 13,3227 00001 0
056246,000640: 13,3230 23421 RECTIFY
056247,000641: 13,3231 53775 VLOAD VSL*
056248,000642: 13,3232 01503 RRECT
056249,000643: 13,3233 57576 0,2
056250,000644: 13,3234 53715 PDVL VSL* # RATT TO PD0
056251,000645: 13,3235 01511 VRECT
056252,000646: 13,3236 57576 0,2
056253,000647: 13,3237 63325 PDDL PDVL # VATT TO PD6 TAT TO PD12
056254,000648: 13,3240 01517 TET
056255,000649: 13,3241 01503 RRECT
056256,000650: 13,3242 64715 PDVL PDDL*
056257,000651: 13,3243 01511 VRECT
056258,000652: 13,3244 50042 MUEARTH,2
056259,000653: 13,3245 76006 PUSH AXT,1
056260,000654: 13,3246 77765 DEC -10 B-14
056261,000655: 13,3247 76014 BON AXT,1
056262,000656: 13,3250 00303 MOONFLAG
056263,000657: 13,3251 27253 +2
056264,000658: 13,3252 77775 DEC -2 B-14
056265,000659: 13,3253 40001 INTEXIT SETPD BOV
056266,000660: 13,3254 00001 0
056267,000661: 13,3255 27256 +1
056268,000662: 13,3256 77614 CLEAR
056269,000663: 13,3257 04675 MIDAVFLG
056270,000664: 13,3260 43014 CLEAR CLEAR
056271,000665: 13,3261 04676 AVEMIDSW # ALLOW UPDATE OF DOWNLINK STATE VECTOR
056272,000666: 13,3262 01667 PRECIFLG
056273,000667: 13,3263 77535 SLOAD EXIT
056274,000668: 13,3264 02215 IRETURN
056275,000669: 13,3265 30154 CA MPAC
056276,000670: 13,3266 50120 INDEX FIXLOC
056277,000671: 13,3267 54052 TS QPRET
056278,000672: 13,3270 03457 TC INTWAKE
056279,000673:
056280,000674: # RVCON SETS UP ORBIT INTEGRATION TO DO A CONIC SOLUTION FOR POSITION AND
056281,000675: # VELOCITY FOR THE INTERVAL (TET-TDEC)
056282,000676:
056283,000677: 13,3271 45345 RVCON DLOAD DSU
056284,000678: 13,3272 01101 TDEC
056285,000679: 13,3273 01517 TET
056286,000680: 13,3274 36312 STCALL TAU.
056287,000681: 13,3275 23421 RECTIFY
056288,000682: 13,3276 77624 CALL
056289,000683: 13,3277 22372 KEPPREP
056290,000684: 13,3300 43345 DLOAD DAD
056291,000685: 13,3301 01551 TC
|
|
Page 1322
|
056293,000687: 13,3302 01517 TET
056294,000688: 13,3303 35517 STCALL TET
056295,000689: 13,3304 27226 RECTOUT
056296,000690:
|
|
Page 1323
|
056298,000692: # TESTLOOP
056299,000693:
056300,000694: 13,3305 43014 TESTLOOP BOF CLRGO
056301,000695: 13,3306 04752 QUITFLAG
056302,000696: 13,3307 27312 +3
056303,000697: 13,3310 01632 STATEFLG
056304,000698: 13,3311 27253 INTEXIT # STOP INTEGRATION
056305,000699: 13,3312 73001 +3 SETPD LXA,2
056306,000700: 13,3313 00013 10D
056307,000701: 13,3314 02150 PBODY
056308,000702: 13,3315 51575 VLOAD ABVAL
056309,000703: 13,3316 01535 RCV
056310,000704: 13,3317 43006 PUSH CLEAR # RC TO 10D
056311,000705: 13,3320 00262 MIDFLAG
056312,000706: 13,3321 50023 DSU* BMN # MIDFLAG=0 IF R G.T. RMP
056313,000707: 13,3322 67212 RME,2
056314,000708: 13,3323 27326 +3
056315,000709: 13,3324 77614 SET
056316,000710: 13,3325 00062 MIDFLAG
056317,000711: 13,3326 41345 NORFINAL DLOAD DMP
056318,000712: 13,3327 00013 10D
056319,000713: 13,3330 00043 34D
056320,000714: 13,3331 55762 SR1R DDV*
056321,000715: 13,3332 50042 MUEARTH,2
056322,000716: 13,3333 41366 SQRT DMP
056323,000717: 13,3334 23752 .3D
056324,000718: 13,3335 40442 SR3 SR4 # DT IS TRUNCATED TO A MULTIPLE
056325,000719: 13,3336 54345 DLOAD SL
056326,000720: 13,3337 00155 MPAC
056327,000721: 13,3340 20220 15D # OF 128 CSECS.
056328,000722: 13,3341 40006 PUSH BOV
056329,000723: 13,3342 27367 MAXDT
056330,000724: 13,3343 50021 BDSU BMN
056331,000725: 13,3344 27441 DT/2MAX
056332,000726: 13,3345 27367 MAXDT
056333,000727: 13,3346 45345 DT/2COMP DLOAD DSU
056334,000728: 13,3347 01101 TDEC
056335,000729: 13,3350 01517 TET
056336,000730: 13,3351 54234 RTB SL
056337,000731: 13,3352 45544 SGNAGREE
056338,000732: 13,3353 20211 8D
056339,000733: 13,3354 02314 STORE DT/2 # B-19
056340,000734: 13,3355 51400 BOV ABS
056341,000735: 13,3356 27373 GETMAXDT
056342,000736: 13,3357 50025 DSU BMN # IS TIME TO INTEG. TO GR THAN MAXTIME
056343,000737: 13,3360 00015 12D
056344,000738: 13,3361 27377 P00HCHK
056345,000739: 13,3362 75345 USEMAXDT DLOAD SIGN
056346,000740: 13,3363 00015 12D
056347,000741: 13,3364 02314 DT/2
|
|
Page 1324
|
056349,000743: 13,3365 36314 STCALL DT/2
056350,000744: 13,3366 27377 P00HCHK
056351,000745: 13,3367 65345 MAXDT DLOAD PDDL # EXCHANGE DT/2MAX WITH COMPUTED MAX.
056352,000746: 13,3370 27441 DT/2MAX
056353,000747: 13,3371 77650 GOTO
056354,000748: 13,3372 27346 DT/2COMP
056355,000749: 13,3373 77634 GETMAXDT RTB
056356,000750: 13,3374 45712 SIGNMPAC
056357,000751: 13,3375 36314 STCALL DT/2
056358,000752: 13,3376 27362 USEMAXDT
056359,000753: 13,3377 51545 P00HCHK DLOAD ABS
056360,000754: 13,3400 02314 DT/2
056361,000755: 13,3401 50025 DSU BMN
056362,000756: 13,3402 27437 DT/2MIN
056363,000757: 13,3403 27176 A-PCHK
056364,000758: 13,3404 46135 SLOAD BHIZ
056365,000759: 13,3405 01012 MODREG
056366,000760: 13,3406 27411 +3
056367,000761: 13,3407 77650 GOTO
056368,000762: 13,3410 23240 TIMESTEP
056369,000763: 13,3411 77614 BON # WAS THIS CALL VIA CSM(LEM)PREC
056370,000764: 13,3412 01707 PRECIFLG
056371,000765: 13,3413 23240 TIMESTEP # YES
056372,000766: 13,3414 45345 DLOAD DSU
056373,000767: 13,3415 02314 DT/2
056374,000768: 13,3416 00015 12D
056375,000769: 13,3417 43040 BMN BOFCLR
056376,000770: 13,3420 27176 A-PCHK
056377,000771: 13,3421 04242 NEWIFLG
056378,000772: 13,3422 23240 TIMESTEP
056379,000773: 13,3423 45345 DLOAD DSU
056380,000774: 13,3424 01101 TDEC
056381,000775: 13,3425 01517 TET
056382,000776: 13,3426 77640 BMN # NO BACKWARD INTEGRATION
056383,000777: 13,3427 27253 INTEXIT
056384,000778: 13,3430 40525 PDDL SR4
056385,000779: 13,3431 02314 DT/2 # IS 4(DT) LS (TDEC - TET)
056386,000780: 13,3432 44322 SR2R BDSU # NO
056387,000781: 13,3433 52040 BMN GOTO
056388,000782: 13,3434 27253 INTEXIT
056389,000783: 13,3435 23240 TIMESTEP
056390,000784: 13,3436 00000 01400 DT/2MIN 2DEC 3 B-20
056391,000785:
056392,000786: 13,3440 14152 00000 DT/2MAX 2DEC 4000 E2 B-20
056393,000787:
056394,000788: 13,3442 77776 INTSTALL EXIT
056395,000789: 13,3443 35021 CAF ZERO
056396,000790: 13,3444 54001 ALLSTALL TS L
056397,000791: 13,3445 30106 CA RASFLAG
056398,000792: 13,3446 50001 INDEX L
|
|
Page 1325
|
056400,000794: 13,3447 73540 MASK INTBITAB # IS THIS STALL AREA FREE
056401,000795: 13,3450 00006 EXTEND
056402,000796: 13,3451 13516 BZF OKTOGRAB # YES
056403,000797: 13,3452 50001 INDEX L
056404,000798: 13,3453 33535 CAF WAKESTAL
056405,000799: 13,3454 05175 TC JOBSLEEP
056406,000800: 13,3455 77776 INTWAKE0 EXIT
056407,000801: 13,3456 13477 TCF INTWAKE1
056408,000802:
056409,000803: 13,3457 40106 INTWAKE CS RASFLAG # IS THIS INTSTALLED ROUTINE TO BE
056410,000804: 13,3460 75011 MASK REINTBIT # RESTARTED
056411,000805: 13,3461 10000 CCS A
056412,000806: 13,3462 03477 TC INTWAKE1 # NO
056413,000807:
056414,000808: 13,3463 50120 INDEX FIXLOC
056415,000809: 13,3464 30052 CA QPRET
056416,000810: 13,3465 55055 TS TBASE2 # YES, DONT RESTART WITH SOMEONE ELSES Q
056417,000811:
056418,000812: 13,3466 05412 TC PHASCHNG
056419,000813: 13,3467 04022 OCT 04022
056420,000814:
056421,000815: 13,3470 31055 CA TBASE2
056422,000816: 13,3471 50120 INDEX FIXLOC
056423,000817: 13,3472 54052 TS QPRET
056424,000818:
056425,000819: 13,3473 35011 CAF REINTBIT
056426,000820: 13,3474 70106 MASK RASFLAG
056427,000821: 13,3475 00006 EXTEND
056428,000822: 13,3476 13521 BZF GOBAC # DONT INTWAKE IF WE CAME HERE VIA RESTART
056429,000823:
056430,000824: 13,3477 35021 INTWAKE1 CAF ZERO
056431,000825: 13,3500 54154 WAKE TS STALTEM # INDEX OF ANY STALL USER
056432,000826: 13,3501 50154 WAKE1 INDEX STALTEM
056433,000827: 13,3502 33535 CAF WAKESTAL
056434,000828: 13,3503 00004 INHINT
056435,000829: 13,3504 05201 TC JOBWAKE
056436,000830: 13,3505 10064 CCS LOCCTR
056437,000831: 13,3506 13501 TCF WAKE1 # MAY BE MORE TO WAKE UP
056438,000832: 13,3507 00051 FORTYONE DEC 41 B-14
056439,000833: 13,3510 50154 INDEX STALTEM
056440,000834: 13,3511 43540 CS INTBITAB
056441,000835: 13,3512 70106 MASK RASFLAG
056442,000836: 13,3513 54106 TS RASFLAG # RELEASE STALL AREA
056443,000837: 13,3514 00003 RELINT
056444,000838: 13,3515 13521 TCF GOBAC
056445,000839: 13,3516 50001 OKTOGRAB INDEX L # NO, WAIT UNTIL AVAILABLE
056446,000840: 13,3517 35002 CAF INTFLBIT
056447,000841: 13,3520 26106 ADS RASFLAG
056448,000842: 13,3521 06006 GOBAC TC INTPRET
056449,000843: 13,3522 77616 RVQ
|
|
Page 1326
|
056451,000845: 13,3523 77776 ERASTAL1 EXIT
056452,000846: 13,3524 35017 CAF ONE
056453,000847: 13,3525 13444 TCF ALLSTALL
056454,000848: 13,3526 77776 ERASTAL2 EXIT
056455,000849: 13,3527 35016 CAF TWO
056456,000850: 13,3530 13444 TCF ALLSTALL
056457,000851: 13,3531 35017 ERASWAK1 CAF ONE
056458,000852: 13,3532 13500 TCF WAKE
056459,000853: 13,3533 35016 ERASWAK2 CAF TWO
056460,000854: 13,3534 13500 TCF WAKE
056461,000855: 13,3535 27443 WAKESTAL CADR INTSTALL +1
056462,000856: 13,3536 27524 CADR ERASTAL1 +1
056463,000857: 13,3537 27527 CADR ERASTAL2 +1
056464,000858: 13,3540 0154 STALTEM EQUALS MPAC
056465,000859: 13,3540 20100 INTBITAB OCT 20100
056466,000860: 13,3541 10040 OCT 10040
056467,000861: 13,3542 04020 OCT 04020
056468,000862:
|
|
Page 1327
|
056470,000864: # AVETOMID
056471,000865:
056472,000866: # THIS ROUTINE PERFORMS THE TRANSITION FROM A THRUSTING PHASE TO THE COAST
056473,000867: # PHASE BY INITIALIZING THIS VEHICLES PERMANENT STATE VECTOR WITH THE
056474,000868: # VALUES LEFT BY THE AVERAGEG ROUTINE IN RN,VN,PIPTIME.
056475,000869:
056476,000870: # BEFORE THIS IS DONE THE W-MATRIX, IF ITS VALID (ORWFLAG OR RENDWFLG IS
056477,000871: # SET) IS INTEGRATED FORWARD TO PIPTIME WITH THE PRE-THRUST STATE VECTOR.
056478,000872:
056479,000873: # IN ADDITION, THE OTHER VEHICLE IS INTEGRATED (PERMANENT) TO PIPTIME.
056480,000874:
056481,000875: # FINALLY TRKMKCNT IS ZEROED
056482,000876:
056483,000877: 35,2000 SETLOC INTINIT2
056484,000878: 35,2000 BANK
056485,000879:
056486,000880: 35,3702 COUNT* $$/INTIN
056487,000881: 35,3702 43020 AVETOMID STQ BON
056488,000882: 35,3703 02317 EGRESS
056489,000883: 35,3704 02716 RENDWFLG
056490,000884: 35,3705 73760 INT/W # W-MATRIX VALID, GO INTEGRATE IT
056491,000885: 35,3706 77614 BON
056492,000886: 35,3707 01711 ORBWFLAG
056493,000887: 35,3710 73760 INT/W # W-MATRIX VALID, GO INTEGRATE IT
056494,000888:
056495,000889: 35,3711 45174 SETCOAST AXT,2 CALL # NOW MOVE PROPERLY SCALED RN,VN AND
056496,000890: 35,3712 00002 2 # PIPTIME TO INTEGRATION ERASABLES.
056497,000891: 35,3713 27442 INTSTALL
056498,000892: 35,3714 77014 BON AXT,2
056499,000893: 35,3715 00315 AMOONFLG
056500,000894: 35,3716 73720 +2
056501,000895: 35,3717 00000 0
056502,000896: 35,3720 53775 VLOAD VSR*
056503,000897: 35,3721 01171 RN
056504,000898: 35,3722 57176 0,2
056505,000899: 35,3723 01503 STORE RRECT
056506,000900: 35,3724 15535 STODL RCV
056507,000901: 35,3725 01205 PIPTIME
056508,000902: 35,3726 25517 STOVL TET
056509,000903: 35,3727 01177 VN
056510,000904: 35,3730 45057 VSR* CALL
056511,000905: 35,3731 57176 0,2
056512,000906: 35,3732 23435 MINIRECT # FINISH SETTING UP STATE VECTOR
056513,000907: 35,3733 66234 RTB SSP
056514,000908: 35,3734 26720 MOVATHIS # PUT TEMP STATE VECTOR INTO PERMANENT
056515,000909: 35,3735 01127 TRKMKCNT
056516,000910: 35,3736 00000 0
056517,000911: 35,3737 43014 SET BON
056518,000912: 35,3740 04063 CMOONFLG
|
|
Page 1328
|
056520,000914: 35,3741 00315 AMOONFLG
056521,000915: 35,3742 73745 +3
056522,000916: 35,3743 77614 CLEAR
056523,000917: 35,3744 04263 CMOONFLG
056524,000918:
056525,000919: 35,3745 71214 BON DLOAD # NOW DO LM
056526,000920: 35,3746 04307 SURFFLAG
056527,000921: 35,3747 75737 FAZAB5 # NO COASTING LM
056528,000922: 35,3750 01205 PIPTIME
056529,000923: 35,3751 34041 STCALL TDEC1
056530,000924: 35,3752 26670 SETIFLGS
056531,000925: 35,3753 45014 CLEAR CALL
056532,000926: 35,3754 01674 VINTFLAG
056533,000927: 35,3755 27162 INTEGRV
056534,000928: 35,3756 77650 GOTO
056535,000929: 35,3757 02317 EGRESS
056536,000930: 35,3760 45145 INT/W DLOAD CALL
056537,000931: 35,3761 01205 PIPTIME # INTEGRATE W THRU BURN
056538,000932: 35,3762 27442 INTSTALL
056539,000933: 35,3763 43014 SET SET
056540,000934: 35,3764 01476 DIM0FLAG # DO W-MATRIX
056541,000935: 35,3765 04476 AVEMIDSW # SO WONT CLOBBER RN,VN,PIPTIME
056542,000936: 35,3766 43014 CLEAR SET
056543,000937: 35,3767 01675 D6OR9FLG
056544,000938: 35,3770 01474 VINTFLAG
056545,000939: 35,3771 34041 STCALL TDEC1
056546,000940: 35,3772 27162 INTEGRV
056547,000941: 35,3773 77650 GOTO
056548,000942: 35,3774 73711 SETCOAST
056549,000943:
|
|
Page 1329
|
056551,000945: # MIDTOAV1
056552,000946:
056553,000947: # THIS ROUTINE INTEGRATES (PRECISION) TO THE TIME SPECIFIED IN TDEC1.
056554,000948: # IF, AT THE END OF AN INTEGRATION TIME STEP, CURRENT TIME PLUS A DELTA
056555,000949: # TIME (SEE TIMEDELT.....BASED ON THE COMPUTATUON TIME FOR ONE TIME STEP)
056556,000950: # IS GREATER THAN THE DESIRED TIME, ALARM 1703 IS SET AND THE INTEGRATION
056557,000951: # IS DONE AS IT IS FOR MIDTOAV2.
056558,000952: # RETURN IS IN BASIC TO THE RETURN ADDRESS PLUS ONE.
056559,000953:
056560,000954: # IF THE INTEGRATION IS FINISHED TO THE DESIRED TIME, RETURN IS IN BASIC
056561,000955: # TO THE RETURN ADDRESS
056562,000956:
056563,000957: # IN EITHER CASE, BEFORE RETURNING, THE EXTRAPOLATED STATE VECTOR IS TRAN
056564,000958: # FERRED FROM R,VATT TO R,VN1-PIPTIME1 IS SET TO THE FINISHING INTEGRA-
056565,000959: # TION TIME AND MPAC IS SET TO THE DELTA TIME---
056566,000960: # TAT MINUS CURRENT TIME.
056567,000961:
056568,000962: # MIDTOAV2
056569,000963:
056570,000964: # THIS ROUTINE INTEGRATES THE CSM STATE VECTOR TO CURRENT TIME PLUS
056571,000965: # INCREMENTS OF TIMEDELT SUCH THAT THE DIFFERENCE BETWEEN CURRENT TIME
056572,000966: # AND THE STATE VECTOR TIME AT THE END OF THE LAST STEP IS AT LEAST 5.6
056573,000967: # SECS.
056574,000968: # NO INPUTS ARE REQUIRED OF THE CALLER. RETURN IS IN BASIC TO THE RETURN
056575,000969: # ADDRESS WITH THE ABOVE TRANSFERS TO R,VN1-PIPTIME1-AND MPAC DONE
056576,000970:
056577,000971: 13,2000 SETLOC INTINIT
056578,000972: 13,2000 BANK
056579,000973: 13,3543 1127 EBANK= IRETURN1
056580,000974: 13,3543 45020 MIDTOAV2 STQ CALL
056581,000975: 13,3544 01127 IRETURN1
056582,000976: 13,3545 27442 INTSTALL
056583,000977: 13,3546 43145 DLOAD CLEAR
056584,000978: 13,3547 27711 TIMEDELT
056585,000979: 13,3550 04674 MID1FLAG
056586,000980: 13,3551 37732 STCALL T-TO-ADD
056587,000981: 13,3552 27567 ENTMID2
056588,000982:
056589,000983: 13,3553 45020 MIDTOAV1 STQ CALL
056590,000984: 13,3554 01127 IRETURN1
056591,000985: 13,3555 27442 INTSTALL
056592,000986: 13,3556 47014 SET RTB
056593,000987: 13,3557 04474 MID1FLAG
056594,000988: 13,3560 45510 LOADTIME
056595,000989: 13,3561 44215 DAD BDSU # INITIAL CHECK, IS TDEC1 IN THE FUTURE.
056596,000990: 13,3562 27711 TIMEDELT
056597,000991: 13,3563 00041 TDEC1
056598,000992: 13,3564 45044 BPL CALL
056599,000993: 13,3565 27573 ENTMID1
|
|
Page 1330
|
056601,000995: 13,3566 27674 NOTIME # NO SET ALARM.SWITCH TO MIDTOAV2
056602,000996:
056603,000997: 13,3567 43234 ENTMID2 RTB DAD
056604,000998: 13,3570 45510 LOADTIME
056605,000999: 13,3571 03732 T-TO-ADD
056606,001000: 13,3572 00041 STORE TDEC1
056607,001001:
056608,001002: 13,3573 45014 ENTMID1 CLEAR CALL
056609,001003: 13,3574 01676 DIM0FLAG # NO W-MATRIX
056610,001004: 13,3575 26034 THISVINT
056611,001005: 13,3576 43014 CLEAR SET
056612,001006: 13,3577 01673 INTYPFLG
056613,001007: 13,3600 04475 MIDAVFLG # LET INTEG. KNOW THE CALL IS FOR MIDTOAV.
056614,001008: 13,3601 77624 CALL
056615,001009: 13,3602 27162 INTEGRV # GO INTEGRATE
056616,001010: 13,3603 66134 SXA,2 SXA,1
056617,001011: 13,3604 03746 RTX2
056618,001012: 13,3605 03745 RTX1
056619,001013: 13,3606 67214 CLEAR SLOAD
056620,001014: 13,3607 00275 AMOONFLG
056621,001015: 13,3610 03747 RTX2
056622,001016: 13,3611 43054 BZE SET
056623,001017: 13,3612 27614 +2
056624,001018: 13,3613 00075 AMOONFLG
056625,001019: 13,3614 77775 VLOAD
056626,001020: 13,3615 00001 RATT
056627,001021: 13,3616 25232 STOVL RN1
056628,001022: 13,3617 00007 VATT
056629,001023: 13,3620 15240 STODL VN1
056630,001024: 13,3621 00015 TAT
056631,001025: 13,3622 01246 STORE PIPTIME1
056632,001026: 13,3623 77776 EXIT
056633,001027:
056634,001028: 13,3624 00004 INHINT
056635,001029: 13,3625 00006 EXTEND
056636,001030: 13,3626 40025 DCS TIME2
056637,001031: 13,3627 20155 DAS MPAC
056638,001032: 13,3630 07226 TC TPAGREE
056639,001033:
056640,001034: 13,3631 31127 CA IRETURN1
056641,001035: 13,3632 04704 TC BANKJUMP
056642,001036: 13,3633 47014 CKMID2 BOF RTB
056643,001037: 13,3634 04754 MID1FLAG
056644,001038: 13,3635 27652 MID2
056645,001039: 13,3636 45510 LOADTIME
056646,001040: 13,3637 44215 DAD BDSU
056647,001041: 13,3640 27711 TIMEDELT
056648,001042: 13,3641 01101 TDEC
056649,001043: 13,3642 45044 BPL CALL
056650,001044: 13,3643 27305 TESTLOOP # YES
|
|
Page 1331
|
056652,001046: 13,3644 27674 NOTIME
056653,001047:
056654,001048: 13,3645 43234 TIMEINC RTB DAD
056655,001049: 13,3646 45510 LOADTIME
056656,001050: 13,3647 03732 T-TO-ADD
056657,001051: 13,3650 35101 STCALL TDEC
056658,001052: 13,3651 27305 TESTLOOP
056659,001053:
056660,001054: 13,3652 45345 MID2 DLOAD DSU
056661,001055: 13,3653 01101 TDEC
056662,001056: 13,3654 01517 TET
056663,001057: 13,3655 45246 ABS DSU
056664,001058: 13,3656 27707 3CSECS
056665,001059: 13,3657 77644 BPL
056666,001060: 13,3660 27645 TIMEINC
056667,001061:
056668,001062: 13,3661 44234 RTB BDSU # SEE IF 5.6 SECS. AVAILABLE TO CALLER.
056669,001063: 13,3662 45510 LOADTIME
056670,001064: 13,3663 01517 TET
056671,001065: 13,3664 51025 DSU BPL
056672,001066: 13,3665 27713 5.6SECS
056673,001067: 13,3666 27176 A-PCHK # YES,GET OUT.
056674,001068:
056675,001069: 13,3667 43345 DLOAD DAD # NO,ADD TIMEDELT TO T-TO-ADD AND TRY
056676,001070: 13,3670 03732 T-TO-ADD # AGAIN.
056677,001071: 13,3671 27711 TIMEDELT
056678,001072: 13,3672 37732 STCALL T-TO-ADD
056679,001073: 13,3673 27645 TIMEINC
056680,001074: 13,3674 77414 NOTIME CLEAR EXIT # TOO LATE
056681,001075: 13,3675 04674 MID1FLAG
056682,001076: 13,3676 25127 INCR IRETURN1 # SET ERROR EXIT (CALLOC +2)
056683,001077: 13,3677 05650 TC ALARM # INSUFFICIENT TIME FOR INTEGRATION --
056684,001078: 13,3700 01703 OCT 1703 # TIG WILL BE SLIPPED...
056685,001079: 13,3701 06006 TC INTPRET
056686,001080: 13,3702 77745 DLOAD
056687,001081: 13,3703 27711 TIMEDELT
056688,001082: 13,3704 03732 STORE T-TO-ADD
056689,001083: 13,3705 77616 RVQ
056690,001084:
056691,001085: 13,3706 00000 00003 3CSECS 2DEC 3 B-28
056692,001086:
056693,001087: 13,3710 00000 02342 TIMEDELT 2DEC 1250 B-28
056694,001088:
056695,001089: 13,3712 00000 01060 5.6SECS 2DEC 560 B-28
056696,001090:
056697,001091: 27,2671 BANK 27
056698,001092: 27,2000 SETLOC UPDATE2
056699,001093: 27,2000 BANK
056700,001094: 27,2671 0330 EBANK= INTWAKUQ
056701,001095:
|
|
Page 1332
|
056703,001097: 27,2671 COUNT* $$/INTIN
056704,001098:
056705,001099: 27,2671 0330 INTWAKUQ = INTWAK1Q # TEMPORARY UNTIL NAME OF INTWAK1Q IS CHNG
056706,001100:
056707,001101: 27,2671 00003 INTWAKEU RELINT
056708,001102: 27,2672 00006 EXTEND
056709,001103: 27,2673 22330 QXCH INTWAKUQ # SAVE Q FOR RETURN
056710,001104:
056711,001105: 27,2674 06006 TC INTPRET
056712,001106:
056713,001107: 27,2675 53135 SLOAD BZE # IS THIS A CSM/LEM STATE VECTOR UPDATE
056714,001108: 27,2676 01502 UPSVFLAG # REQUEST. IF NOT GO TO INTWAKUP.
056715,001109: 27,2677 56736 INTWAKUP
056716,001110:
056717,001111: 27,2700 77775 VLOAD # MOVE RRECT(6) AND VRECT(6) INTO
056718,001112: 27,2701 01503 RRECT # RCV(6) AND VCV(6) RESPECTIVELY.
056719,001113: 27,2702 25535 STOVL RCV
056720,001114: 27,2703 01511 VRECT # NOW GO TO 'RECTIFY +13D' TO
056721,001115: 27,2704 77624 CALL # STORE VRECT INTO VCV AND ZERO OUT
056722,001116: 27,2705 23436 RECTIFY +13D # TDELTAV(6),TNUV(6),TC(2) AND XKEP(2)
056723,001117: 27,2706 51535 SLOAD ABS # COMPARE ABSOLUTE VALUE OF 'UPSVFLAG'
056724,001118: 27,2707 01502 UPSVFLAG # TO 'UPDATE MOON STATE VECTOR CODE'
056725,001119: 27,2710 53025 DSU BZE # TO DETERMINE WHETHER THE STATE VECTOR TO
056726,001120: 27,2711 16747 UPMNSVCD # BE UPDATED IS IN THE EARTH OR LUNAR
056727,001121: 27,2712 56717 INTWAKEM # SPHERE OF INFLUENCE.........
056728,001122: 27,2713 43174 AXT,2 CLRGO # EARTH SPHERE OF INFLUENCE.
056729,001123: 27,2714 00000 DEC 0 B-14
056730,001124: 27,2715 00223 MOONFLAG
056731,001125: 27,2716 56722 INTWAKEC
056732,001126: 27,2717 43174 INTWAKEM AXT,2 SET # LUNAR SPHERE OF INFLUENCE.
056733,001127: 27,2720 00002 DEC 2 B-14
056734,001128: 27,2721 00063 MOONFLAG
056735,001129: 27,2722 50135 INTWAKEC SLOAD BMN # COMMON CODING AFTER X2 INITIALIZED AND
056736,001130: # MOONFLAG SET (OR CLEARED).
056737,001131: 27,2723 01502 UPSVFLAG # IS THIS A REQUEST FOR A LEM OR CSM
056738,001132: 27,2724 56732 INTWAKLM # STATE VECTOR UPDATE......
056739,001133: 27,2725 77624 CALL # UPDATE CSM STATE VECTOR
056740,001134: 27,2726 26705 ATOPCSM
056741,001135:
056742,001136: 27,2727 52014 CLEAR GOTO
056743,001137: 27,2730 01671 ORBWFLAG
056744,001138: 27,2731 56734 INTWAKEX
056745,001139:
056746,001140: 27,2732 77624 INTWAKLM CALL # UPDATE LM STATE VECTOR
056747,001141: 27,2733 26760 ATOPLEM
056748,001142:
056749,001143: 27,2734 77614 INTWAKEX CLEAR
056750,001144: 27,2735 02676 RENDWFLG
056751,001145:
056752,001146: 27,2736 45131 INTWAKUP SSP CALL # REMOVE :UPDATE STATE VECTOR INDICATOR:
|
|
Page 1333
|
056754,001148: 27,2737 01502 UPSVFLAG
056755,001149: 27,2740 00000 0
056756,001150: 27,2741 27455 INTWAKE0 # RELEASE :GRAB: OF ORBIT INTEG
056757,001151: 27,2742 77776 EXIT
056758,001152:
056759,001153: 27,2743 05412 TC PHASCHNG
056760,001154: 27,2744 04026 OCT 04026
056761,001155: 27,2745 00330 TC INTWAKUQ
056762,001156:
056763,001157: 27,2746 00002 UPMNSVCD OCT 2
056764,001158: 27,2747 00000 OCT 0
056765,001159:
056766,001160: 27,2750 77420 GRP2PC STQ EXIT
056767,001161: 27,2751 03536 GRP2SVQ
056768,001162: 27,2752 05412 TC PHASCHNG
056769,001163: 27,2753 04022 OCT 04022
056770,001164: 27,2754 06006 TC INTPRET
056771,001165: 27,2755 77650 GOTO
056772,001166: 27,2756 03536 GRP2SVQ
056773,001167:
056774,001168:
056775,001169:
End of include-file INTEGRATION_INITIALIZATION.agc. Parent file is MAIN.agc