Source Code
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These source-code files are part of a reconstructed copy of Comanche 51, the
initial release (though not the final mission release) of the Apollo 11
Command Module (CM) Apollo Guidance Computer (AGC) software. The flown, final
release was Comanche 55. The reconstruction is believed to be exactly accurate,
but in the absence of an actual Apollo-era listing of Comanche 51, some
explanation of the reconstruction process is needed to insure confidence in
that accuracy.
The starting point was the source code of Comanche 55, whose original source code
is available. Comanche 55 source code was then modified by undoing changes known
to have been made between revisions 51 and 55. The most-significant steps involved
reverting changes related to the R-2 lunar potential model, the details of which
were known from the previous, separate, independent reconstruction of the Apollo 10
Lunar Module software Luminary 69/2. The now-reconstructed
Comanche 51 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 match those on the Comanche 55 or Luminary 69 printouts, although
the source code would likely have different page numbers in a contemporary Comanche 51 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 55. Here's a guide
to some of the Apollo documentation relevant to those annotations:
Among documentation not actually referenced in the annotations, there is
a short writeup about the reconstruction process in our software repository
that may be helpful in understanding it from a different perspective. There's also
a handy table
that lists what the number of memory-words should be for each routine in Comanche 51,
which could make a nice double-check; however, we've not performed that double-check ourselves.
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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055587,000002: ## Copyright: Public domain.
055588,000003: ## Filename: INTEGRATION_INITIALIZATION.agc
055589,000004: ## Purpose: A section of Comanche revision 051.
055590,000005: ## It is part of the reconstructed source code for the
055591,000006: ## original release of the flight software for the Command
055592,000007: ## Module's (CM) Apollo Guidance Computer (AGC) for Apollo 11.
055593,000008: ## The code has been recreated from a copy of Comanche 055. It
055594,000009: ## has been adapted such that the resulting bugger words
055595,000010: ## exactly match those specified for Comanche 51 in NASA drawing
055596,000011: ## 2021153D, which gives relatively high confidence that the
055597,000012: ## reconstruction is correct.
055598,000013: ## Reference: pp. 1309-1333
055599,000014: ## Assembler: yaYUL
055600,000015: ## Contact: Ron Burkey <info@sandroid.org>.
055601,000016: ## Website: www.ibiblio.org/apollo/index.html
055602,000017: ## Mod history: 2019-07-30 MAS Created from Comanche 55.
055603,000018:
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Page 1309
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055605,000020: # 1.0 INTRODUCTION
055606,000021: # ----------------
055607,000022:
055608,000023: # FROM A USERS POINT OF VIEW, ORBITAL INTEGRATION IS ESSENTIALLY THE SAME AS THE 278 INTEGRATION
055609,000024: # PROGRAM. THE SAME ENTRANCES TO THE PROGRAM WILL BE MAINTAINED, THE SAME STALLING ROUTINE WILL BE USED AND
055610,000025: # OUTPUT WILL STILL BE VIA THE PUSHLIST. THE PRIMARY DIFFERENCES TO A USER INVOLVE THE ADDED CAPABILITY OF
055611,000026: # TERMINATING INTEGRATION AT A SPECIFIC FINAL RADIUS AND THE DIFFERENCE IN STATE VECTOR SCALING INSIDE AND OUT-
055612,000027: # SIDE THE LUNAR SPHERE OF INFLUENCE.
055613,000028:
055614,000029: # IN ORDER TO MAKE THE CSM(LEM)PREC AND CSM(LEM)CONIC ENTRANCES SIMILAR TO FLIGHT 278, THE INTEGRATION PROGRAM
055615,000030: # WILL ITSELF SET THE FINAL RADIUS (RFINAL) TO 0 SO THAT REACHING THE DESIRED TIME ONLY WILL TERMINATE
055616,000031: # INTEGRATION. THE DP REGISTER RFINAL MUST BE SET BY USERS OF INTEGRVS AND INTEGRV, AND MUST BE DONE AFTER THE
055617,000032: # CALL TC INTSTALL.
055618,000033:
055619,000034: # WHEN THE LM IS ON THE LUNAR SURFACE (INDICATED BY LUNAR SURFACE FLAG SET) CALLS TO LEMCONIC, LEMPREC, AND
055620,000035: # INTEGRV WITH VINFLAG = 0 WILL RESULT IN THE USE OF THE PLANETARY INERTIAL ORIENTATION SUBROUTINES TO PROVIDE
055621,000036: # BOTH THE LMS POSITION AND VELOCITY IN THE REFERENCE COORDINATE SYSTEM.
055622,000037: # THE PROGRAM WILL PROVIDE OUTPUT AS IF INTEGRATION WAS USED. THAT IS, THE PUSHLIST WILL BE SET AS NOTED BELOW AND
055623,000038: # THE PERMANENT STATE VECTOR UPDATED WHEN SPECIFIED BY AN INTEGRV CALL.
055624,000039:
055625,000040: # USERS OF INTEGRVS DESIRING INTEGRATION (INTYPFLG = 0) SHOULD NOTE THAT THE OBLATENESS PERTURBATION COMPUTATION
055626,000041: # IN LUNAR ORBIT IS TIME DEPENDENT. THEREFORE, THE USER SHOULD SUPPLY AN INITIAL STATE VECTOR VALID AT SOME REAL
055627,000042: # TIME AND THE DESIRED TIME (TDEC1) ALSO AT SOME REAL TIME. FOR CONIC ,,INTEGRATION,, THE USER MAY STILL USE ZERO
055628,000043: # AS THE INITIAL TIME AND DELTA TIME AS THE DESIRED TIME.
055629,000044:
055630,000045: # 2.0 GENERAL DESCRIPTION
055631,000046: # -----------------------
055632,000047:
055633,000048: # THE INTEGRATION PROGRAM OPERATES AS A CLOSED INTERPRETIVE SUBROUTINE AND PERFORMS THESE FUNCTIONS ---
055634,000049: # 1) INTEGRATES (PRECISION OR CONIC) EITHER CSM OR LM STATE VECTOR
055635,000050: # 2) INTEGRATES THE W-MATRIX
055636,000051: # 3) PERMANENT OR TEMPORARY UPDATE OF THE STATE VECTOR
055637,000052:
055638,000053: # THERE ARE SIX ENTRANCES TO THE INTEGRATION PROGRAM. FOUR OF THESE (CSMPREC, LEMPREC, CSMCONIC, LEMCONIC) SET
055639,000054: # ALL THE FLAGS REQUIRED IN THE INTEGRATION PROGRAM ITSELF TO CAUSE THE PRECISION OR CONIC INTEGRATION (KEPLER) OF
055640,000055: # THE LM OR CSM STATE VECTOR, AS THE NAMES SUGGEST. ONE ENTRANCE (INTEGRVS) PERMITS THE CALLING PROGRAM TO
055641,000056: # PROVIDE A STATE VECTOR TO BE INTEGRATED. THE CALLING PROGRAM MUST SET THE FLAGS INDICATING (1) PRECISION OR
055642,000057: # CONIC INTEGRATION, (2) IN OR OUT OF LUNAR SPHERE, (3) MIDCOURSE OR NOT, AND THE INTEGRATION PROGRAM COMPLETES
055643,000058: # THE FLAG SETTING TO BYPASS W-MATRIX INTEGRATION. THE LAST ENTRANCE (INTEGRV, USED IN GENERAL BY THE
055644,000059: # NAVIGATION PROGRAMS) PERMITS THE CALLER TO SET FIVE FLAGS (NOT MOONFLAG OR MIDFLAG) BUT NOT TO INPUT A STATE
055645,000060: # VECTOR. ANY PROGRAM WHICH CALLS INTEGRVS OR INTEGRV MUST CALL INTSTALL BEFORE IT SETS THE INTEGRATION FLAGS
055646,000061: # AND/OR STATE VECTOR.
055647,000062:
055648,000063: # THREE SETS OF 42 REGISTERS AND 2 FLAGS ARE USED FOR THE STATE VECTORS. TWO SETS, WHICH MAY NOT BE OVERLAYED, ARE
055649,000064: # USED FOR THE PERMANENT STATE VECTORS FOR THE CSM AND LM. THE THIRD SET, WHICH MAY BE OVERLAYED WHEN INTEGRATION
055650,000065: # IS NOT BEING DONE, IS USED IN THE COMPUTATIONS.
055651,000066:
055652,000067: # THE PERMANENT STATE VECTORS WILL BE PERIODICALLY UPDATED SO THAT THE VECTORS WILL NOT BE OLDER THAN 4 TIMESTEPS.
055653,000068: # THE PERMANENT STATE VECTORS WILL ALSO BE UPDATED WHENEVER THE W-MATRIX IS INTEGRATED OR WHEN A CALLER OF INTEGRV
055654,000069: # SETS STATEFLG (THE NAVIGATION PROGRAMS P20, P22.)
055655,000070:
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Page 1310
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055657,000072: # APPENDIX B OF THE USERS GUIDE LISTS THE STATE VECTOR QUANTITIES.
055658,000073:
055659,000074: # 2.1 RESTARTS
055660,000075:
055661,000076: # PHASE CHANGES WILL BE MADE IN THE INTEGRATION PROGRAM ONLY FOR THE INTEGRV ENTRANCE (I.E., WHEN THE W-MATRIX IS
055662,000077: # INTEGRATED OR PERMANENT STATE VECTOR IS UPDATED.) THE GROUP NUMBER USED WILL BE THAT FOR THE P20-25 PROGRAMS
055663,000078: # (I.E., GROUP2) SINCE THE INTEGRV ENTRANCE WILL ONLY BE USED BY THESE PROGRAMS. IF A RESTART OCCURS DURING AN
055664,000079: # INTEGRATION OF THE STATE VECTOR ONLY, THE RECOVERY WILL BE TO THE LAST PHASE IN THE CALLING PROGRAM. CALLING
055665,000080: # PROGRAMS WHICH USE THE INTEGRV OR INTEGRVS ENTRANCE OF INTEGRATION SHOULD ENSURE THAT IF PHASE CHANGING IS DONE
055666,000081: # THAT IT IS PRIOR TO SETTING THE INTEGRATION INPUTS IN THE PUSHLIST.
055667,000082: # THIS IS BECAUSE THE PUSHLIST IS LOST DURING A RESTART.
055668,000083:
055669,000084: # 2.2 SCALING
055670,000085:
055671,000086: # THE INTEGRATION ROUTINE WILL MAINTAIN THE PERMANENT MEMORY STATE VECTORS IN THE SCALING AND UNITS DEFINED IN
055672,000087: # APPENDIX B OF THE USERS GUIDE. THE SCALING OF THE OUTPUT POSITION VECTOR DEPENDS ON THE ORIGIN OF THE COORDINATE
055673,000088: # SYSTEM AT THE DESIRED INTEGRATION TIME. THE COORDINATE SYSTEM TRANSFORMATION WILL BE DONE AUTOMATICALLY ON
055674,000089: # MULTIPLE TIMESTEP ENCKE INTEGRATION ONLY. THUS IT IS POSSIBLE TO HAVE OUTPUT FROM SUCCESSIVE INTEGRATIONS IN
055675,000090: # DIFFERENT SCALING.
055676,000091: # HOWEVER, RATT, VATT WILL ALWAYS BE SCALED THE SAME.
055677,000092:
055678,000093: # 3.0 INPUT/OUTPUT
055679,000094: # ----------------
055680,000095:
055681,000096: # PROGRAM INPUTS ARE THE FLAGS DESCRIBED IN APPENDIX A AND THE PERMANENT STATE VECTOR QUANTITIES DESCRIBED IN AP-
055682,000097: # PENDIX B OF THE USERS GUIDE, PLUS THE DESIRED TIME TO INTEGRATE TO IN TDEC1 (A PUSH LIST LOCATION).
055683,000098: # FOR INTEGRVS, THE RCV,VCV,TET OF THE TEMPORARY STATE VECTOR MUST BE SET, PLUS MOONFLAG AND MIDFLAG
055684,000099:
055685,000100: # FOR SIMULATION THE FOLLOWING QUANTITIES MUST BE PRESET ---
055686,000101: # EARTH MOON
055687,000102: # 29 27
055688,000103: # RRECTCSM(LEM) - RECTIFIED POSITION VECTOR METERS 2 2
055689,000104:
055690,000105: # 7 5
055691,000106: # VRECTCSM(LEM) - RECTIFIED VELOCITY VECTOR M/CSEC 2 2
055692,000107:
055693,000108: # 28 28
055694,000109: # TETCSM(LEM) - TIME STATE VECTOR IS VALID CSEC 2 2
055695,000110: # CUSTOMARILY 0, BUT NOTE LUNAR
055696,000111: # ORBIT DEPENDENCE ON REAL TIME.
055697,000112:
055698,000113: # 22 18
055699,000114: # DELTAVCSM(LEM) - POSITION DEVIATION METERS 2 2
055700,000115: # 0 IF TCCSM(LEM) = 0
055701,000116:
055702,000117: # 3 -1
055703,000118: # NUVCSM(LEM) - VELOCITY DEVIATION M/CSEC 2 2
055704,000119: # 0 IF TCCSM(LEM) = 0
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Page 1311
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055706,000121: # 29 27
055707,000122: # RCVCSM(LEM) - CONIC POSITION METERS 2 2
055708,000123: # EQUALS RRECTCSM(LEM) IF
055709,000124: # TCCSM(LEM) = 0
055710,000125:
055711,000126: # 7 5
055712,000127: # VCVCSM(LEM) - CONIC VELOCITY M/CSEC 2 2
055713,000128: # EQUALS VRECTCSM(LEM) IF
055714,000129: # TCCSM(LEM) = 0
055715,000130:
055716,000131: # 28 28
055717,000132: # TCCSM(LEM) - TIME SINCE RECTIFICATION CSECS 2 2
055718,000133: # CUSTOMARILY 0
055719,000134:
055720,000135: # 1/2 17 16
055721,000136: # XKEPCSM(LEM) - ROOT OF KEPLERS EQUATION M 2 2
055722,000137: # 0 IF TCCSM(LEM) = 0
055723,000138:
055724,000139: # CMOONFLG - PERMANENT FLAGS CORRESPONDING 0 0
055725,000140: # CMIDFLAG TO MOONFLAG AND MIDFLAG 0,1 0,1
055726,000141: # LMOONFLG C = CSM, L = LM 0 0
055727,000142: # LMIDFLG 0,1 0,1
055728,000143:
055729,000144: # SURFFLAG - LUNAR SURFACE FLAG 0,1 0,1
055730,000145:
055731,000146: # IN ADDITION, IF (L)CMIDFLAG IS SET, THE INITIAL INPUT VALUES FOR LUNAR
055732,000147: # SOLAR EPHEMERIDES SUBROUTINE AND PLANETARY INERTIAL ORIENTATION SUB-
055733,000148: # ROUTINE MUST BE PRESET.
055734,000149:
055735,000150: # OUTPUT
055736,000151: # AFTER EVERY CALL TO INTEGRATION
055737,000152: # EARTH MOON
055738,000153: # 29 29
055739,000154: # 0D RATT POSITION METERS 2 2
055740,000155:
055741,000156: # 7 7
055742,000157: # 6D VATT VELOCITY M/CSEC 2 2
055743,000158:
055744,000159: # 28 28
055745,000160: # 12D TAT TIME 2 2
055746,000161:
055747,000162: # 29 27
055748,000163: # 14D RATT1 POSITION METERS 2 2
055749,000164:
055750,000165: # 7 5
055751,000166: # 20D VATT1 VELOCITY M/CSEC 2 2
055752,000167:
055753,000168: # 3 2 36 30
055754,000169: # 26D MU(P) MU M /CS 2 2
055755,000170:
055756,000171: # X1 MUTABLE ENTRY -2 -10D
055757,000172:
055758,000173: # X2 COORDINT
055759,000174: # X2 COORDINATE SYSTEM ORIGEN 0 2
055760,000175: # (THIS, NOT MOONFLAG, SHOULD BE
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Page 1312
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055762,000177: # USED TO DETERMINE ORIGIN.)
055763,000178:
055764,000179: # IN ADDITION TO THE ABOVE, THE PERMANENT STATE VECTOR IS UPDATED WHENEVER
055765,000180: # STATEFLG WAS SET AND WHENEVER A W-MATRIX IS TO BE INTEGRATED. THE PUSH
055766,000181: # COUNTER IS SET TO 0 AND OVERFLOW IS CLEARED BEFORE RETURNING TO THE
055767,000182: # CALLING PROGRAM.
055768,000183:
055769,000184: # 4.0 CALLING SEQUENCES AND SAMPLE CODE
055770,000185: # -------------------------------------
055771,000186:
055772,000187: # A) PRECISION ORBITAL INTEGRATION. CSMPREC, LEMPREC ENTRANCES
055773,000188: # L-X STORE TIME TO 95T5791T5 T 95 PUS L9ST (T4531)
055774,000189: # L CALL
055775,000190: # L+1 CSMPREC (OR LEMPREC)
055776,000191: # L+2 RETURN
055777,000192: # INPUT 28
055778,000193: # TDEC1 (PD 32D) TIME TO INTEGRATE TO...CENTISECONDS SCALED 2
055779,000194: # OUTPUT
055780,000195: # THE DATA LISTED IN SECTION 3.0 PLUS
055781,000196: # RQVV POSITION VECTOR OF VEHICLE WITH RESPECT TO SECONDARY
055782,000197: # BODY... METERS B-29 ONLY IF MIDFLAG = DIMOFLAG = 1
055783,000198: # B) CONIC INTEGRATION. CSMCONIC, LEMCONIC ENTRANCES
055784,000199: # L-X STORE TIME IN PUSH LIST (TDEC1)
055785,000200: # L CALL
055786,000201: # L+1 CSMCONIC (OR LEMCONIC)
055787,000202: # INPUT/OUTPUT
055788,000203: # SAME AS PRECISION INTEGRATION, EXCEPT RQVV NOT SET
055789,000204: # C) INTEGRATE GIVEN STATE VECTOR. INTEGRVS ENTRANCE
055790,000205: # CALL
055791,000206: # INTSTALL
055792,000207: # VLOAD
055793,000208: # POSITION VECTOR
055794,000209: # STOVL RCV
055795,000210: # VELOCITY VECTOR
055796,000211: # STODL VCV
055797,000212: # TIME STATE VECTOR VALID
055798,000213: # STODL TET
055799,000214: # FINAL RADIUS
055800,000215: # STORE RFINAL
055801,000216: # SET(CLEAR) SET(CLEAR)
055802,000217: # INTYPFLAG
055803,000218: # MOONFLAG
055804,000219: # SET(CLEAR) DLOAD
055805,000220: # DESIRED TIME
055806,000221: # STCALL TDEC1
055807,000222: # INTEGRVS
055808,000223: # INPUT
055809,000224: # RCV POSITION VECTOR METERS
055810,000225: # VCV VELOCITY VECTOR M/CSEC
055811,000226: # TET TIME OF STATE VECTOR (MAY = 0) CSEC B-28
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Page 1313
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055813,000228: # TDEC1 TIME TO INTEGRATE TO CSEC B-28 (PD 32D)
055814,000229: # (MAY BE INCREMENT IF TET=0)
055815,000230: # OUTPUT
055816,000231: # SAME AS FOR PRECISION OR CONIC INTEGRATION,
055817,000232: # DEPENDING ON INTYPFLG.
055818,000233: # D) INTEGRATE STATE VECTOR. INTGRV ENTRANCE
055819,000234: # L-X STORE TIME IN PUSH LIST (TDEC1) (MAY BE DONE AFTER CALL TO INTSTALL)
055820,000235: # L-8 CALL
055821,000236: # L-7
055822,000237: # L-6 SET(CLEAR) SET(CLEAR)
055823,000238: # L-5 VINTFLAG 1=CSM, 0=LM
055824,000239: # L-4 INTYPFLAG 1=CONIC, 0=PRECISION
055825,000240: # L-3 SET(CLEAR) SET(CLEAR)
055826,000241: # L-2 DIMOFLAG 1=W-MATRIX, 0=NO W-MATRIX
055827,000242: # L-1 D6OR9FLG 1=9X9, 0=6X6
055828,000243: # L SET DLOAD
055829,000244: # L+1 STATEFLG DESIRE PERMANENT UPDATE
055830,000245: # L+2 FINAL RAD. OF STATE VECTOR
055831,000246: # L+3 STCALL RFINAL
055832,000247: # L+4 INTEGRV
055833,000248: # L CALL NORMAL USE -- WILL UPDATE STATE
055834,000249: # L+1 INTEGRV VECTOR IF DIMOFLAG=1. (STATEFLG IS
055835,000250: # L+2 RETURN ALWAYS RESET IN INTEGRATION AFTER
055836,000251: # IT IS USED.)
055837,000252: # INPUT
055838,000253: # TDEC1 (PD 32D) TIME TO INTEGRATE TO CSEC B-28
055839,000254: # OUTPUT
055840,000255: # SAME AS FOR PRECISION OR CONIC INTEGRATION
055841,000256: # THE PROGRAM WILL SET MOONFLAG, MIDFLAG DEPENDING ON
055842,000257: # THE PERMANENT STATE VECTOR REPRESENTATION.
055843,000258:
055844,000259: 11,2363 BANK 11
055845,000260: 13,2000 SETLOC INTINIT
055846,000261: 13,2000 BANK
055847,000262: 13,2627 E3,1554 EBANK= RRECTCSM
055848,000263: 13,2627 COUNT 13/INTIN
055849,000264:
055850,000265: 13,2627 05412 STATEINT TC PHASCHNG
055851,000266: 13,2630 00052 OCT 00052
055852,000267: 13,2631 35061 CAF PRIO5
055853,000268: 13,2632 05147 TC FINDVAC
055854,000269: 13,2633 E3,1554 EBANK= RRECTCSM
055855,000270: 13,2633 02636 26063 2CADR STATINT1
055856,000271:
055857,000272: 13,2635 05324 TC TASKOVER
055858,000273: 13,2636 06006 STATINT1 TC INTPRET
055859,000274: 13,2637 47014 BON RTB
055860,000275: 13,2640 04712 QUITFLAG
055861,000276: 13,2641 26677 NOINT # NO STATEINT IF V96
055862,000277: 13,2642 45510 LOADTIME
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Page 1314
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055864,000279: 13,2643 00041 STORE TDEC1
055865,000280: 13,2644 45014 CLEAR CALL
055866,000281: 13,2645 04274 V96ONFLG
055867,000282: 13,2646 27442 INTSTALL
055868,000283: 13,2647 45014 SET CALL
055869,000284: 13,2650 01076 NODOFLAG
055870,000285: 13,2651 26670 SETIFLGS
055871,000286: 13,2652 77650 GOTO
055872,000287: 13,2653 26000 STATEUP
055873,000288: 13,2654 00003 25140 600SECS 2DEC 60000 B-28
055874,000289:
055875,000290: 13,2656 77414 ENDINT CLEAR EXIT
055876,000291: 13,2657 01672 STATEFLG
055877,000292: 13,2660 05412 TC PHASCHNG
055878,000293: 13,2661 20032 OCT 20032
055879,000294: 13,2662 00006 EXTEND
055880,000295: 13,2663 32655 DCA 600SECS
055881,000296: 13,2664 05342 TC LONGCALL
055882,000297: 13,2665 E3,1554 EBANK= RRECTHIS
055883,000298: 13,2665 02627 26063 2CADR STATEINT
055884,000299:
055885,000300: 13,2667 05217 TC ENDOFJOB
055886,000301: 13,2670 43014 SETIFLGS SET CLEAR
055887,000302: 13,2671 01472 STATEFLG
055888,000303: 13,2672 01673 INTYPFLG
055889,000304: 13,2673 43014 CLEAR CLEAR
055890,000305: 13,2674 01676 DIM0FLAG
055891,000306: 13,2675 01675 D6OR9FLG
055892,000307: 13,2676 77616 RVQ
055893,000308: 13,2677 77776 NOINT EXIT
055894,000309: 13,2700 05412 TC PHASCHNG
055895,000310: 13,2701 00002 OCT 2
055896,000311:
055897,000312: 13,2702 05560 TC DOWNFLAG
055898,000313: 13,2703 00221 ADRES QUITFLAG
055899,000314:
055900,000315: 13,2704 05217 TC ENDOFJOB
055901,000316:
055902,000317: # ATOPCSM TRANSFERS RRECT TO RRECT +41 TO RRECTCSM TO RRECTCSM +41
055903,000318:
055904,000319: # CALLING SEQUENCE
055905,000320: # L CALL
055906,000321: # L+1 ATOPCSM
055907,000322:
055908,000323: # NORMAL EXIT AT L+2
055909,000324:
055910,000325: 13,2705 47020 ATOPCSM STQ RTB
055911,000326: 13,2706 00051 S2
055912,000327: 13,2707 26720 MOVEACSM
055913,000328: 13,2710 45014 SET CALL
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Page 1315
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055915,000330: 13,2711 04063 CMOONFLG
055916,000331: 13,2712 20237 SVDWN1
055917,000332: 13,2713 43014 BON CLRGO
055918,000333: 13,2714 00303 MOONFLAG
055919,000334: 13,2715 00051 S2
055920,000335: 13,2716 04223 CMOONFLG
055921,000336: 13,2717 00051 S2
055922,000337: 13,2720 03064 MOVEACSM TC SETBANK
055923,000338: 13,2721 55500 TS DIFEQCNT # INITIALIZE INDEX
055924,000339: 13,2722 51500 INDEX DIFEQCNT
055925,000340: 13,2723 31502 CA RRECT
055926,000341: 13,2724 51500 INDEX DIFEQCNT
055927,000342: 13,2725 55554 TS RRECTCSM
055928,000343: 13,2726 11500 CCS DIFEQCNT # IS TRANSFER COMPLETE
055929,000344: 13,2727 12721 TCF MOVEACSM +1 # NO-LOOP
055930,000345: 13,2730 06030 TC DANZIG # COMPLETE - RETURN
055931,000346:
055932,000347: # PTOACSM TRANSFERS RRECTCSM TO RRECTCSM +41 TO RRECT TO RRECT +41
055933,000348:
055934,000349: # CALLING SEQUENCE
055935,000350: # L CALL
055936,000351: # PTOACSM
055937,000352:
055938,000353: # NORMAL EXIT AT L+2
055939,000354:
055940,000355: 13,2731 43034 PTOACSM RTB BON
055941,000356: 13,2732 26747 MOVEPCSM
055942,000357: 13,2733 04303 CMOONFLG
055943,000358: 13,2734 26742 SETMOON
055944,000359: 13,2735 66214 CLRMOON CLEAR SSP
055945,000360: 13,2736 00263 MOONFLAG
055946,000361: 13,2737 02151 PBODY
055947,000362: 13,2740 00000 0
055948,000363: 13,2741 77616 RVQ
055949,000364: 13,2742 66214 SETMOON SET SSP
055950,000365: 13,2743 00063 MOONFLAG
055951,000366: 13,2744 02151 PBODY
055952,000367: 13,2745 00002 2
055953,000368: 13,2746 77616 RVQ
055954,000369: 13,2747 03064 MOVEPCSM TC SETBANK
055955,000370: 13,2750 55500 TS DIFEQCNT
055956,000371: 13,2751 51500 INDEX DIFEQCNT
055957,000372: 13,2752 31554 CA RRECTCSM
055958,000373: 13,2753 51500 INDEX DIFEQCNT
055959,000374: 13,2754 55502 TS RRECT
055960,000375: 13,2755 11500 CCS DIFEQCNT
055961,000376: 13,2756 12750 TCF MOVEPCSM +1
055962,000377: 13,2757 06030 TC DANZIG
055963,000378:
|
|
Page 1316
|
055965,000380: # ATOPLEM TRANSFERS RRECT TO RRECT +41 TO RRECTLEM TO RRECTLEM +41
055966,000381: 13,2760 47020 ATOPLEM STQ RTB
055967,000382: 13,2761 00051 S2
055968,000383: 13,2762 26773 MOVEALEM
055969,000384: 13,2763 45014 SET CALL
055970,000385: 13,2764 04064 LMOONFLG
055971,000386: 13,2765 20263 SVDWN2
055972,000387: 13,2766 43014 BON CLRGO
055973,000388: 13,2767 00303 MOONFLAG
055974,000389: 13,2770 00051 S2
055975,000390: 13,2771 04224 LMOONFLG
055976,000391: 13,2772 00051 S2
055977,000392: 13,2773 03064 MOVEALEM TC SETBANK
055978,000393: 13,2774 55500 TS DIFEQCNT
055979,000394: 13,2775 51500 INDEX DIFEQCNT
055980,000395: 13,2776 31502 CA RRECT
055981,000396: 13,2777 51500 INDEX DIFEQCNT
055982,000397: 13,3000 55626 TS RRECTLEM
055983,000398: 13,3001 11500 CCS DIFEQCNT
055984,000399: 13,3002 12774 TCF MOVEALEM +1
055985,000400: 13,3003 06030 TC DANZIG
055986,000401:
055987,000402: # PTOALEM TRANSFERS RRECTLEM TO RRECTLEM +41 TO RRECT TO RRECT +41
055988,000403:
055989,000404: 13,3004 47014 PTOALEM BON RTB
055990,000405: 13,3005 04307 SURFFLAG
055991,000406: 13,3006 27025 USEPIOS
055992,000407: 13,3007 27014 MOVEPLEM
055993,000408: 13,3010 52014 BON GOTO
055994,000409: 13,3011 04304 LMOONFLG
055995,000410: 13,3012 26742 SETMOON
055996,000411: 13,3013 26735 CLRMOON
055997,000412: 13,3014 03064 MOVEPLEM TC SETBANK
055998,000413: 13,3015 55500 TS DIFEQCNT
055999,000414: 13,3016 51500 INDEX DIFEQCNT
056000,000415: 13,3017 31626 CA RRECTLEM
056001,000416: 13,3020 51500 INDEX DIFEQCNT
056002,000417: 13,3021 55502 TS RRECT
056003,000418: 13,3022 11500 CCS DIFEQCNT
056004,000419: 13,3023 13015 TCF MOVEPLEM +1
056005,000420: 13,3024 06030 TC DANZIG
056006,000421:
056007,000422: 13,3025 77201 USEPIOS SETPD VLOAD
056008,000423: 13,3026 00001 0
056009,000424: 13,3027 02026 RLS
056010,000425: 13,3030 41525 PDDL PUSH
056011,000426: 13,3031 00041 TDEC1
|
|
Page 1317
|
056013,000428: 13,3032 15517 STODL TET
056014,000429: 13,3033 27755 5/8
056015,000430: 13,3034 77624 CALL
056016,000431: 13,3035 55344 RP-TO-R
056017,000432: 13,3036 25535 STOVL RCV
056018,000433: 13,3037 11560 ZUNIT
056019,000434: 13,3040 14001 STODL 0D
056020,000435: 13,3041 01517 TET
056021,000436: 13,3042 14007 STODL 6D
056022,000437: 13,3043 27755 5/8
056023,000438: 13,3044 45014 SET CALL # NEEDED FOR SETTING X1 ON EXIT
056024,000439: 13,3045 00063 MOONFLAG
056025,000440: 13,3046 55344 RP-TO-R
056026,000441: 13,3047 74235 VXV VXSC
056027,000442: 13,3050 01535 RCV
056028,000443: 13,3051 27063 OMEGMOON
056029,000444: 13,3052 25543 STOVL VCV
056030,000445: 13,3053 11566 ZEROVEC
056031,000446: 13,3054 01521 STORE TDELTAV
056032,000447: 13,3055 67174 AXT,2 SXA,2
056033,000448: 13,3056 00002 2
056034,000449: 13,3057 02150 PBODY
056035,000450: 13,3060 35527 STCALL TNUV
056036,000451: 13,3061 27176 A-PCHK
056037,000452: 13,3062 07112 06620 OMEGMOON 2DEC* 2.66169947 E-8 B+23*
056038,000453:
056039,000454: 13,3064 33070 SETBANK CAF INTBANK
056040,000455: 13,3065 54006 TS BBANK
056041,000456: 13,3066 33507 CAF FORTYONE
056042,000457: 13,3067 00002 TC Q
056043,000458: 13,3070 E3,1554 EBANK= RRECTCSM
056044,000459: 13,3070 26063 INTBANK BBCON INTEGRV
056045,000460:
056046,000461: # SPECIAL PURPOSE ENTRIES TO ORBITAL INTEGRATION. THESE ROUTINES PROVIDE ENTRANCES TO INTEGRATION WITH
056047,000462: # APPROPRIATE SWITCHES SET OR CLEARED FOR THE DESIRED INTEGRATION.
056048,000463:
056049,000464: # CSMPREC AND LEMPREC PERFORM ORBIT INTEGRATION BY THE ENCKE METHOD TO THE TIME INDICATED IN TDEC1
056050,000465: # ACCELERATIONS DUE TO OBLATENESS ARE INCLUDED. NO W-MATRIX INT. IS DONE.
056051,000466: # THE PERMANENT STATE VECTOR IS NOT UPDATED.
056052,000467: # CSMCONIC AND LEMCONIC PERFORM ORBIT INTEG. BY KEPLERS METHOD TO THE TIME INDICATED IN TDEC1
056053,000468: # NO DISTURBING ACCELERATIONS ARE INCLUDED. IN THE PROGRAM FLOW THE GIVEN
056054,000469: # STATE VECTOR IS RECTIFIED BEFORE SOLUTION OF KEPLERS EQUATION
056055,000470:
056056,000471: # THE ROUTINES ASSUME THAT THE CSM (LEM) STATE VECTOR IN P-MEM IS VALID.
056057,000472: # SWITCHES SET PRIOR TO ENTRY TO THE MAIN INTEG. PROG ARE AS FOLLOWS
056058,000473: # CSMPREC CSMCONIC LEMPREC LEMCONIC
056059,000474: # VINTFLAG SET SET CLEAR CLEAR
056060,000475: # INTYPFLG CLEAR SET CLEAR SET
056061,000476: # DIM0FLAG CLEAR CLEAR CLEAR CLEAR
|
|
Page 1318
|
056063,000478:
056064,000479: # CALLING SEQUENCE
056065,000480: # L-X STORE TDEC1
056066,000481: # L CALL (STCALL TDEC1)
056067,000482: # L+1 CSMPREC (CSMCONIC, LEMPREC, LEMCONIC)
056068,000483:
056069,000484: # NORMAL EXIT TO L+2
056070,000485:
056071,000486: # SUBROUTINES CALLED
056072,000487: # INTEGRV1
056073,000488: # PRECOUT FOR CSMPREC AND LEMPREC
056074,000489: # CONICOUT FOR CSMCONIC AND LEMCONIC
056075,000490:
056076,000491: # OUTPUT - SEE PAGE 2 OF THIS LOG SECTION
056077,000492:
056078,000493: # INPUT
056079,000494: # TDEC1 TIME TO INTEGRATE TO. CSECS B-28
056080,000495:
056081,000496: 13,3071 45020 CSMPREC STQ CALL
056082,000497: 13,3072 00046 X1
056083,000498: 13,3073 27442 INTSTALL
056084,000499: 13,3074 43130 SXA,1 SET
056085,000500: 13,3075 02214 IRETURN
056086,000501: 13,3076 01474 VINTFLAG
056087,000502:
056088,000503: 13,3077 43014 IFLAGP SET CLEAR
056089,000504: 13,3100 01467 PRECIFLG
056090,000505: 13,3101 01676 DIM0FLAG
056091,000506: 13,3102 77614 CLRGO
056092,000507: 13,3103 01633 INTYPFLG
056093,000508: 13,3104 27164 INTEGRV1
056094,000509: 13,3105 45020 LEMPREC STQ CALL
056095,000510: 13,3106 00046 X1
056096,000511: 13,3107 27442 INTSTALL
056097,000512: 13,3110 43130 SXA,1 CLRGO
056098,000513: 13,3111 02214 IRETURN
056099,000514: 13,3112 01634 VINTFLAG
056100,000515: 13,3113 27077 IFLAGP
056101,000516:
056102,000517: 13,3114 45020 CSMCONIC STQ CALL
056103,000518: 13,3115 00046 X1
056104,000519: 13,3116 27442 INTSTALL
056105,000520: 13,3117 43130 SXA,1 SET
056106,000521: 13,3120 02214 IRETURN
056107,000522: 13,3121 01474 VINTFLAG
056108,000523: 13,3122 43014 IFLAGC CLEAR SETGO
056109,000524: 13,3123 01676 DIM0FLAG
056110,000525: 13,3124 01433 INTYPFLG
056111,000526: 13,3125 27164 INTEGRV1
056112,000527: 13,3126 45020 LEMCONIC STQ CALL
056113,000528: 13,3127 00046 X1
|
|
Page 1319
|
056115,000530: 13,3130 27442 INTSTALL
056116,000531: 13,3131 43130 SXA,1 CLRGO
056117,000532: 13,3132 02214 IRETURN
056118,000533: 13,3133 01634 VINTFLAG
056119,000534: 13,3134 27122 IFLAGC
056120,000535:
056121,000536: 13,3135 66214 INTEGRVS SET SSP
056122,000537: 13,3136 01467 PRECIFLG
056123,000538: 13,3137 02151 PBODY
056124,000539: 13,3140 00000 0
056125,000540: 13,3141 66214 BOF SSP
056126,000541: 13,3142 00343 MOONFLAG
056127,000542: 13,3143 27146 +3
056128,000543: 13,3144 02151 PBODY
056129,000544: 13,3145 00002 2
056130,000545: 13,3146 77220 STQ VLOAD
056131,000546: 13,3147 02214 IRETURN
056132,000547: 13,3150 11566 ZEROVEC
056133,000548: 13,3151 01521 STORE TDELTAV
056134,000549: 13,3152 35527 STCALL TNUV
056135,000550: 13,3153 23421 RECTIFY
056136,000551: 13,3154 43014 CLEAR SET
056137,000552: 13,3155 01676 DIM0FLAG
056138,000553: 13,3156 04062 NEWIFLG
056139,000554: 13,3157 77614 SETGO
056140,000555: 13,3160 04020 RPQFLAG
056141,000556: 13,3161 22363 ALOADED
056142,000557:
056143,000558: # INTEGRV IS AN ENTRY TO ORBIT INTEGRATION WHICH PERMITS THE CALLER,
056144,000559: # NORMALLY THE NAVIGATION PROGRAM, TO SET THE INTEG. FLAGS. THE ROUTINE
056145,000560: # IS ENTERED AT INTEGRV1 BY CSMPREC ET. AL. AND AT ALOADED BY INTEGRVS.
056146,000561: # THE ROUTINE SETS UP A-MEMORY IF ENTERED AT INTEGRV,1 AND SETS THE INTEG.
056147,000562: # PROGRAM FOR PRECISION OR CONIC
056148,000563:
056149,000564: # THE CALLER MUST FIRST CALL INTSTALL TO CHECK IF INTEG. IS IN USE BEFORE
056150,000565: # SETTING ANY FLAGS.
056151,000566:
056152,000567: # THE FLAGS WHICH SHOULD BE SET OR CLEARED ARE
056153,000568: # VINTFLAG (IGNORED WHEN ENTERED FROM INTEGRVS)
056154,000569: # INTYPFLG
056155,000570: # DIM0FLAG
056156,000571: # D6OR9FLG
056157,000572:
056158,000573: # CALLING SEQUENCE
056159,000574: # L-X CALL
056160,000575: # L-Y INTSTALL
056161,000576: # L-1 SET OR CLEAR ALL FOUR FLAGS. ALSO CAN SET STATEFLG IF DESIRED
056162,000577: # AND DIM0FLAG IS CLEAR.
056163,000578: # L CALL
056164,000579: # L+1 INTEGRV
056165,000580:
056166,000581: # INITIALIZATION
056167,000582: # FLAGS AS ABOVE
056168,000583: # STORE TIME TO INTEGRATE TO IN TDEC1
056169,000584:
|
|
Page 1320
|
056171,000586: # OUTPUT
056172,000587: # RATT AS
056173,000588: # VATT DEFINED
056174,000589: # TAT BEFORE
056175,000590:
056176,000591: 13,3162 77620 INTEGRV STQ
056177,000592: 13,3163 02214 IRETURN
056178,000593: 13,3164 43014 INTEGRV1 SET SET
056179,000594: 13,3165 04060 RPQFLAG
056180,000595: 13,3166 04062 NEWIFLG
056181,000596: 13,3167 77731 INTEGRV2 SSP
056182,000597: 13,3170 00053 QPRET
056183,000598: 13,3171 22363 ALOADED
056184,000599: 13,3172 52014 BON GOTO
056185,000600: 13,3173 01714 VINTFLAG
056186,000601: 13,3174 26731 PTOACSM
056187,000602: 13,3175 27004 PTOALEM
056188,000603: 11,2000 SETLOC INTINIT1
056189,000604: 11,2000 BANK
056190,000605: 11,2363 77745 ALOADED DLOAD
056191,000606: 11,2364 00041 TDEC1
056192,000607: 11,2365 01101 STORE TDEC
056193,000608: 11,2366 52014 BOFF GOTO
056194,000609: 11,2367 01753 INTYPFLG
056195,000610: 11,2370 27305 TESTLOOP
056196,000611: 11,2371 27271 RVCON
056197,000612: 13,2000 SETLOC INTINIT
056198,000613: 13,2000 BANK
056199,000614: 13,3176 45014 A-PCHK BOF CALL
056200,000615: 13,3177 00342 MIDFLAG
056201,000616: 13,3200 27205 ANDOUT # DONT MAKE ORIGIN CHANGE CHECK
056202,000617: 13,3201 23320 CHKSWTCH
056203,000618: 13,3202 45044 BPL CALL
056204,000619: 13,3203 27205 ANDOUT # NO ORIGIN CHANGE
056205,000620: 13,3204 23361 ORIGCHNG # MAKE THE SWITCH
056206,000621: 13,3205 77414 ANDOUT BOFCLR EXIT
056207,000622: 13,3206 01652 STATEFLG
056208,000623: 13,3207 27226 RECTOUT
056209,000624: 13,3210 05412 TC PHASCHNG
056210,000625: 13,3211 04022 OCT 04022
056211,000626: 13,3212 05546 TC UPFLAG # PHASE CHANGE HAS OCCURRED BETWEEN
056212,000627: 13,3213 00236 ADRES REINTFLG # INTSTALL AND INTWAKE
056213,000628: 13,3214 06006 TC INTPRET
056214,000629: 13,3215 77731 SSP
056215,000630: 13,3216 00053 QPRET
056216,000631: 13,3217 27224 PHEXIT
056217,000632: 13,3220 52014 BON GOTO
056218,000633: 13,3221 01714 VINTFLAG
056219,000634: 13,3222 26705 ATOPCSM
|
|
Page 1321
|
056221,000636: 13,3223 26760 ATOPLEM
056222,000637: 13,3224 77624 PHEXIT CALL
056223,000638: 13,3225 56750 GRP2PC
056224,000639: 13,3226 45001 RECTOUT SETPD CALL
056225,000640: 13,3227 00001 0
056226,000641: 13,3230 23421 RECTIFY
056227,000642: 13,3231 53775 VLOAD VSL*
056228,000643: 13,3232 01503 RRECT
056229,000644: 13,3233 57576 0,2
056230,000645: 13,3234 53715 PDVL VSL* # RATT TO PD0
056231,000646: 13,3235 01511 VRECT
056232,000647: 13,3236 57576 0,2
056233,000648: 13,3237 63325 PDDL PDVL # VATT TO PD6 TAT TO PD12
056234,000649: 13,3240 01517 TET
056235,000650: 13,3241 01503 RRECT
056236,000651: 13,3242 64715 PDVL PDDL*
056237,000652: 13,3243 01511 VRECT
056238,000653: 13,3244 50042 MUEARTH,2
056239,000654: 13,3245 76006 PUSH AXT,1
056240,000655: 13,3246 77765 DEC -10 B-14
056241,000656: 13,3247 76014 BON AXT,1
056242,000657: 13,3250 00303 MOONFLAG
056243,000658: 13,3251 27253 +2
056244,000659: 13,3252 77775 DEC -2 B-14
056245,000660: 13,3253 40001 INTEXIT SETPD BOV
056246,000661: 13,3254 00001 0
056247,000662: 13,3255 27256 +1
056248,000663: 13,3256 77614 CLEAR
056249,000664: 13,3257 04675 MIDAVFLG
056250,000665: 13,3260 43014 CLEAR CLEAR
056251,000666: 13,3261 04676 AVEMIDSW # ALLOW UPDATE OF DOWNLINK STATE VECTOR
056252,000667: 13,3262 01667 PRECIFLG
056253,000668: 13,3263 77535 SLOAD EXIT
056254,000669: 13,3264 02215 IRETURN
056255,000670: 13,3265 30154 CA MPAC
056256,000671: 13,3266 50120 INDEX FIXLOC
056257,000672: 13,3267 54052 TS QPRET
056258,000673: 13,3270 03457 TC INTWAKE
056259,000674:
056260,000675: # RVCON SETS UP ORBIT INTEGRATION TO DO A CONIC SOLUTION FOR POSITION AND
056261,000676: # VELOCITY FOR THE INTERVAL (TET-TDEC)
056262,000677:
056263,000678: 13,3271 45345 RVCON DLOAD DSU
056264,000679: 13,3272 01101 TDEC
056265,000680: 13,3273 01517 TET
056266,000681: 13,3274 36312 STCALL TAU.
056267,000682: 13,3275 23421 RECTIFY
056268,000683: 13,3276 77624 CALL
056269,000684: 13,3277 22372 KEPPREP
056270,000685: 13,3300 43345 DLOAD DAD
056271,000686: 13,3301 01551 TC
|
|
Page 1322
|
056273,000688: 13,3302 01517 TET
056274,000689: 13,3303 35517 STCALL TET
056275,000690: 13,3304 27226 RECTOUT
056276,000691:
|
|
Page 1323
|
056278,000693: # TESTLOOP
056279,000694:
056280,000695: 13,3305 43014 TESTLOOP BOF CLRGO
056281,000696: 13,3306 04752 QUITFLAG
056282,000697: 13,3307 27312 +3
056283,000698: 13,3310 01632 STATEFLG
056284,000699: 13,3311 27253 INTEXIT # STOP INTEGRATION
056285,000700: 13,3312 73001 +3 SETPD LXA,2
056286,000701: 13,3313 00013 10D
056287,000702: 13,3314 02150 PBODY
056288,000703: 13,3315 51575 VLOAD ABVAL
056289,000704: 13,3316 01535 RCV
056290,000705: 13,3317 43006 PUSH CLEAR # RC TO 10D
056291,000706: 13,3320 00262 MIDFLAG
056292,000707: 13,3321 50023 DSU* BMN # MIDFLAG=0 IF R G.T. RMP
056293,000708: 13,3322 67212 RME,2
056294,000709: 13,3323 27326 +3
056295,000710: 13,3324 77614 SET
056296,000711: 13,3325 00062 MIDFLAG
056297,000712: 13,3326 41345 NORFINAL DLOAD DMP
056298,000713: 13,3327 00013 10D
056299,000714: 13,3330 00043 34D
056300,000715: 13,3331 55762 SR1R DDV*
056301,000716: 13,3332 50042 MUEARTH,2
056302,000717: 13,3333 41366 SQRT DMP
056303,000718: 13,3334 23752 .3D
056304,000719: 13,3335 40442 SR3 SR4 # DT IS TRUNCATED TO A MULTIPLE
056305,000720: 13,3336 54345 DLOAD SL
056306,000721: 13,3337 00155 MPAC
056307,000722: 13,3340 20220 15D # OF 128 CSECS.
056308,000723: 13,3341 40006 PUSH BOV
056309,000724: 13,3342 27367 MAXDT
056310,000725: 13,3343 50021 BDSU BMN
056311,000726: 13,3344 27441 DT/2MAX
056312,000727: 13,3345 27367 MAXDT
056313,000728: 13,3346 45345 DT/2COMP DLOAD DSU
056314,000729: 13,3347 01101 TDEC
056315,000730: 13,3350 01517 TET
056316,000731: 13,3351 54234 RTB SL
056317,000732: 13,3352 45544 SGNAGREE
056318,000733: 13,3353 20211 8D
056319,000734: 13,3354 02314 STORE DT/2 # B-19
056320,000735: 13,3355 51400 BOV ABS
056321,000736: 13,3356 27373 GETMAXDT
056322,000737: 13,3357 50025 DSU BMN # IS TIME TO INTEG. TO GR THAN MAXTIME
056323,000738: 13,3360 00015 12D
056324,000739: 13,3361 27377 P00HCHK
056325,000740: 13,3362 75345 USEMAXDT DLOAD SIGN
056326,000741: 13,3363 00015 12D
056327,000742: 13,3364 02314 DT/2
|
|
Page 1324
|
056329,000744: 13,3365 36314 STCALL DT/2
056330,000745: 13,3366 27377 P00HCHK
056331,000746: 13,3367 65345 MAXDT DLOAD PDDL # EXCHANGE DT/2MAX WITH COMPUTED MAX.
056332,000747: 13,3370 27441 DT/2MAX
056333,000748: 13,3371 77650 GOTO
056334,000749: 13,3372 27346 DT/2COMP
056335,000750: 13,3373 77634 GETMAXDT RTB
056336,000751: 13,3374 45712 SIGNMPAC
056337,000752: 13,3375 36314 STCALL DT/2
056338,000753: 13,3376 27362 USEMAXDT
056339,000754: 13,3377 51545 P00HCHK DLOAD ABS
056340,000755: 13,3400 02314 DT/2
056341,000756: 13,3401 50025 DSU BMN
056342,000757: 13,3402 27437 DT/2MIN
056343,000758: 13,3403 27176 A-PCHK
056344,000759: 13,3404 46135 SLOAD BHIZ
056345,000760: 13,3405 01012 MODREG
056346,000761: 13,3406 27411 +3
056347,000762: 13,3407 77650 GOTO
056348,000763: 13,3410 23240 TIMESTEP
056349,000764: 13,3411 77614 BON # WAS THIS CALL VIA CSM(LEM)PREC
056350,000765: 13,3412 01707 PRECIFLG
056351,000766: 13,3413 23240 TIMESTEP # YES
056352,000767: 13,3414 45345 DLOAD DSU
056353,000768: 13,3415 02314 DT/2
056354,000769: 13,3416 00015 12D
056355,000770: 13,3417 43040 BMN BOFCLR
056356,000771: 13,3420 27176 A-PCHK
056357,000772: 13,3421 04242 NEWIFLG
056358,000773: 13,3422 23240 TIMESTEP
056359,000774: 13,3423 45345 DLOAD DSU
056360,000775: 13,3424 01101 TDEC
056361,000776: 13,3425 01517 TET
056362,000777: 13,3426 77640 BMN # NO BACKWARD INTEGRATION
056363,000778: 13,3427 27253 INTEXIT
056364,000779: 13,3430 40525 PDDL SR4
056365,000780: 13,3431 02314 DT/2 # IS 4(DT) LS (TDEC - TET)
056366,000781: 13,3432 44322 SR2R BDSU # NO
056367,000782: 13,3433 52040 BMN GOTO
056368,000783: 13,3434 27253 INTEXIT
056369,000784: 13,3435 23240 TIMESTEP
056370,000785: 13,3436 00000 01400 DT/2MIN 2DEC 3 B-20
056371,000786:
056372,000787: 13,3440 14152 00000 DT/2MAX 2DEC 4000 E2 B-20
056373,000788:
056374,000789: 13,3442 77776 INTSTALL EXIT
056375,000790: 13,3443 35021 CAF ZERO
056376,000791: 13,3444 54001 ALLSTALL TS L
056377,000792: 13,3445 30106 CA RASFLAG
056378,000793: 13,3446 50001 INDEX L
|
|
Page 1325
|
056380,000795: 13,3447 73540 MASK INTBITAB # IS THIS STALL AREA FREE
056381,000796: 13,3450 00006 EXTEND
056382,000797: 13,3451 13516 BZF OKTOGRAB # YES
056383,000798: 13,3452 50001 INDEX L
056384,000799: 13,3453 33535 CAF WAKESTAL
056385,000800: 13,3454 05175 TC JOBSLEEP
056386,000801: 13,3455 77776 INTWAKE0 EXIT
056387,000802: 13,3456 13477 TCF INTWAKE1
056388,000803:
056389,000804: 13,3457 40106 INTWAKE CS RASFLAG # IS THIS INTSTALLED ROUTINE TO BE
056390,000805: 13,3460 75011 MASK REINTBIT # RESTARTED
056391,000806: 13,3461 10000 CCS A
056392,000807: 13,3462 03477 TC INTWAKE1 # NO
056393,000808:
056394,000809: 13,3463 50120 INDEX FIXLOC
056395,000810: 13,3464 30052 CA QPRET
056396,000811: 13,3465 55055 TS TBASE2 # YES, DONT RESTART WITH SOMEONE ELSES Q
056397,000812:
056398,000813: 13,3466 05412 TC PHASCHNG
056399,000814: 13,3467 04022 OCT 04022
056400,000815:
056401,000816: 13,3470 31055 CA TBASE2
056402,000817: 13,3471 50120 INDEX FIXLOC
056403,000818: 13,3472 54052 TS QPRET
056404,000819:
056405,000820: 13,3473 35011 CAF REINTBIT
056406,000821: 13,3474 70106 MASK RASFLAG
056407,000822: 13,3475 00006 EXTEND
056408,000823: 13,3476 13521 BZF GOBAC # DONT INTWAKE IF WE CAME HERE VIA RESTART
056409,000824:
056410,000825: 13,3477 35021 INTWAKE1 CAF ZERO
056411,000826: 13,3500 54154 WAKE TS STALTEM # INDEX OF ANY STALL USER
056412,000827: 13,3501 50154 WAKE1 INDEX STALTEM
056413,000828: 13,3502 33535 CAF WAKESTAL
056414,000829: 13,3503 00004 INHINT
056415,000830: 13,3504 05201 TC JOBWAKE
056416,000831: 13,3505 10064 CCS LOCCTR
056417,000832: 13,3506 13501 TCF WAKE1 # MAY BE MORE TO WAKE UP
056418,000833: 13,3507 00051 FORTYONE DEC 41 B-14
056419,000834: 13,3510 50154 INDEX STALTEM
056420,000835: 13,3511 43540 CS INTBITAB
056421,000836: 13,3512 70106 MASK RASFLAG
056422,000837: 13,3513 54106 TS RASFLAG # RELEASE STALL AREA
056423,000838: 13,3514 00003 RELINT
056424,000839: 13,3515 13521 TCF GOBAC
056425,000840: 13,3516 50001 OKTOGRAB INDEX L # NO, WAIT UNTIL AVAILABLE
056426,000841: 13,3517 35002 CAF INTFLBIT
056427,000842: 13,3520 26106 ADS RASFLAG
056428,000843: 13,3521 06006 GOBAC TC INTPRET
056429,000844: 13,3522 77616 RVQ
|
|
Page 1326
|
056431,000846: 13,3523 77776 ERASTAL1 EXIT
056432,000847: 13,3524 35017 CAF ONE
056433,000848: 13,3525 13444 TCF ALLSTALL
056434,000849: 13,3526 77776 ERASTAL2 EXIT
056435,000850: 13,3527 35016 CAF TWO
056436,000851: 13,3530 13444 TCF ALLSTALL
056437,000852: 13,3531 35017 ERASWAK1 CAF ONE
056438,000853: 13,3532 13500 TCF WAKE
056439,000854: 13,3533 35016 ERASWAK2 CAF TWO
056440,000855: 13,3534 13500 TCF WAKE
056441,000856: 13,3535 27443 WAKESTAL CADR INTSTALL +1
056442,000857: 13,3536 27524 CADR ERASTAL1 +1
056443,000858: 13,3537 27527 CADR ERASTAL2 +1
056444,000859: 13,3540 0154 STALTEM EQUALS MPAC
056445,000860: 13,3540 20100 INTBITAB OCT 20100
056446,000861: 13,3541 10040 OCT 10040
056447,000862: 13,3542 04020 OCT 04020
056448,000863:
|
|
Page 1327
|
056450,000865: # AVETOMID
056451,000866:
056452,000867: # THIS ROUTINE PERFORMS THE TRANSITION FROM A THRUSTING PHASE TO THE COAST
056453,000868: # PHASE BY INITIALIZING THIS VEHICLES PERMANENT STATE VECTOR WITH THE
056454,000869: # VALUES LEFT BY THE AVERAGEG ROUTINE IN RN,VN,PIPTIME.
056455,000870:
056456,000871: # BEFORE THIS IS DONE THE W-MATRIX, IF ITS VALID (ORWFLAG OR RENDWFLG IS
056457,000872: # SET) IS INTEGRATED FORWARD TO PIPTIME WITH THE PRE-THRUST STATE VECTOR.
056458,000873:
056459,000874: # IN ADDITION, THE OTHER VEHICLE IS INTEGRATED (PERMANENT) TO PIPTIME.
056460,000875:
056461,000876: # FINALLY TRKMKCNT IS ZEROED
056462,000877:
056463,000878: 35,2000 SETLOC INTINIT2
056464,000879: 35,2000 BANK
056465,000880:
056466,000881: 35,3675 COUNT* $$/INTIN
056467,000882: 35,3675 43020 AVETOMID STQ BON
056468,000883: 35,3676 02317 EGRESS
056469,000884: 35,3677 02716 RENDWFLG
056470,000885: 35,3700 73753 INT/W # W-MATRIX VALID, GO INTEGRATE IT
056471,000886: 35,3701 77614 BON
056472,000887: 35,3702 01711 ORBWFLAG
056473,000888: 35,3703 73753 INT/W # W-MATRIX VALID, GO INTEGRATE IT
056474,000889:
056475,000890: 35,3704 45174 SETCOAST AXT,2 CALL # NOW MOVE PROPERLY SCALED RN,VN AND
056476,000891: 35,3705 00002 2 # PIPTIME TO INTEGRATION ERASABLES.
056477,000892: 35,3706 27442 INTSTALL
056478,000893: 35,3707 77014 BON AXT,2
056479,000894: 35,3710 00315 AMOONFLG
056480,000895: 35,3711 73713 +2
056481,000896: 35,3712 00000 0
056482,000897: 35,3713 53775 VLOAD VSR*
056483,000898: 35,3714 01171 RN
056484,000899: 35,3715 57176 0,2
056485,000900: 35,3716 01503 STORE RRECT
056486,000901: 35,3717 15535 STODL RCV
056487,000902: 35,3720 01205 PIPTIME
056488,000903: 35,3721 25517 STOVL TET
056489,000904: 35,3722 01177 VN
056490,000905: 35,3723 45057 VSR* CALL
056491,000906: 35,3724 57176 0,2
056492,000907: 35,3725 23435 MINIRECT # FINISH SETTING UP STATE VECTOR
056493,000908: 35,3726 66234 RTB SSP
056494,000909: 35,3727 26720 MOVATHIS # PUT TEMP STATE VECTOR INTO PERMANENT
056495,000910: 35,3730 01127 TRKMKCNT
056496,000911: 35,3731 00000 0
056497,000912: 35,3732 43014 SET BON
056498,000913: 35,3733 04063 CMOONFLG
|
|
Page 1328
|
056500,000915: 35,3734 00315 AMOONFLG
056501,000916: 35,3735 73740 +3
056502,000917: 35,3736 77614 CLEAR
056503,000918: 35,3737 04263 CMOONFLG
056504,000919:
056505,000920: 35,3740 71214 BON DLOAD # NOW DO LM
056506,000921: 35,3741 04307 SURFFLAG
056507,000922: 35,3742 75751 FAZAB5 # NO COASTING LM
056508,000923: 35,3743 01205 PIPTIME
056509,000924: 35,3744 34041 STCALL TDEC1
056510,000925: 35,3745 26670 SETIFLGS
056511,000926: 35,3746 45014 CLEAR CALL
056512,000927: 35,3747 01674 VINTFLAG
056513,000928: 35,3750 27162 INTEGRV
056514,000929: 35,3751 77650 GOTO
056515,000930: 35,3752 02317 EGRESS
056516,000931: 35,3753 45145 INT/W DLOAD CALL
056517,000932: 35,3754 01205 PIPTIME # INTEGRATE W THRU BURN
056518,000933: 35,3755 27442 INTSTALL
056519,000934: 35,3756 43014 SET SET
056520,000935: 35,3757 01476 DIM0FLAG # DO W-MATRIX
056521,000936: 35,3760 04476 AVEMIDSW # SO WONT CLOBBER RN,VN,PIPTIME
056522,000937: 35,3761 43014 CLEAR SET
056523,000938: 35,3762 01675 D6OR9FLG
056524,000939: 35,3763 01474 VINTFLAG
056525,000940: 35,3764 34041 STCALL TDEC1
056526,000941: 35,3765 27162 INTEGRV
056527,000942: 35,3766 77650 GOTO
056528,000943: 35,3767 73704 SETCOAST
056529,000944:
|
|
Page 1329
|
056531,000946: # MIDTOAV1
056532,000947:
056533,000948: # THIS ROUTINE INTEGRATES (PRECISION) TO THE TIME SPECIFIED IN TDEC1.
056534,000949: # IF, AT THE END OF AN INTEGRATION TIME STEP, CURRENT TIME PLUS A DELTA
056535,000950: # TIME (SEE TIMEDELT.....BASED ON THE COMPUTATUON TIME FOR ONE TIME STEP)
056536,000951: # IS GREATER THAN THE DESIRED TIME, ALARM 1703 IS SET AND THE INTEGRATION
056537,000952: # IS DONE AS IT IS FOR MIDTOAV2.
056538,000953: # RETURN IS IN BASIC TO THE RETURN ADDRESS PLUS ONE.
056539,000954:
056540,000955: # IF THE INTEGRATION IS FINISHED TO THE DESIRED TIME, RETURN IS IN BASIC
056541,000956: # TO THE RETURN ADDRESS
056542,000957:
056543,000958: # IN EITHER CASE, BEFORE RETURNING, THE EXTRAPOLATED STATE VECTOR IS TRAN
056544,000959: # FERRED FROM R,VATT TO R,VN1-PIPTIME1 IS SET TO THE FINISHING INTEGRA-
056545,000960: # TION TIME AND MPAC IS SET TO THE DELTA TIME---
056546,000961: # TAT MINUS CURRENT TIME.
056547,000962:
056548,000963: # MIDTOAV2
056549,000964:
056550,000965: # THIS ROUTINE INTEGRATES THE CSM STATE VECTOR TO CURRENT TIME PLUS
056551,000966: # INCREMENTS OF TIMEDELT SUCH THAT THE DIFFERENCE BETWEEN CURRENT TIME
056552,000967: # AND THE STATE VECTOR TIME AT THE END OF THE LAST STEP IS AT LEAST 5.6
056553,000968: # SECS.
056554,000969: # NO INPUTS ARE REQUIRED OF THE CALLER. RETURN IS IN BASIC TO THE RETURN
056555,000970: # ADDRESS WITH THE ABOVE TRANSFERS TO R,VN1-PIPTIME1-AND MPAC DONE
056556,000971:
056557,000972: 13,2000 SETLOC INTINIT
056558,000973: 13,2000 BANK
056559,000974: 13,3543 1127 EBANK= IRETURN1
056560,000975: 13,3543 45020 MIDTOAV2 STQ CALL
056561,000976: 13,3544 01127 IRETURN1
056562,000977: 13,3545 27442 INTSTALL
056563,000978: 13,3546 43145 DLOAD CLEAR
056564,000979: 13,3547 27711 TIMEDELT
056565,000980: 13,3550 04674 MID1FLAG
056566,000981: 13,3551 37732 STCALL T-TO-ADD
056567,000982: 13,3552 27567 ENTMID2
056568,000983:
056569,000984: 13,3553 45020 MIDTOAV1 STQ CALL
056570,000985: 13,3554 01127 IRETURN1
056571,000986: 13,3555 27442 INTSTALL
056572,000987: 13,3556 47014 SET RTB
056573,000988: 13,3557 04474 MID1FLAG
056574,000989: 13,3560 45510 LOADTIME
056575,000990: 13,3561 44215 DAD BDSU # INITIAL CHECK, IS TDEC1 IN THE FUTURE.
056576,000991: 13,3562 27711 TIMEDELT
056577,000992: 13,3563 00041 TDEC1
056578,000993: 13,3564 45044 BPL CALL
056579,000994: 13,3565 27573 ENTMID1
|
|
Page 1330
|
056581,000996: 13,3566 27674 NOTIME # NO SET ALARM.SWITCH TO MIDTOAV2
056582,000997:
056583,000998: 13,3567 43234 ENTMID2 RTB DAD
056584,000999: 13,3570 45510 LOADTIME
056585,001000: 13,3571 03732 T-TO-ADD
056586,001001: 13,3572 00041 STORE TDEC1
056587,001002:
056588,001003: 13,3573 45014 ENTMID1 CLEAR CALL
056589,001004: 13,3574 01676 DIM0FLAG # NO W-MATRIX
056590,001005: 13,3575 26034 THISVINT
056591,001006: 13,3576 43014 CLEAR SET
056592,001007: 13,3577 01673 INTYPFLG
056593,001008: 13,3600 04475 MIDAVFLG # LET INTEG. KNOW THE CALL IS FOR MIDTOAV.
056594,001009: 13,3601 77624 CALL
056595,001010: 13,3602 27162 INTEGRV # GO INTEGRATE
056596,001011: 13,3603 66134 SXA,2 SXA,1
056597,001012: 13,3604 03746 RTX2
056598,001013: 13,3605 03745 RTX1
056599,001014: 13,3606 67214 CLEAR SLOAD
056600,001015: 13,3607 00275 AMOONFLG
056601,001016: 13,3610 03747 RTX2
056602,001017: 13,3611 43054 BZE SET
056603,001018: 13,3612 27614 +2
056604,001019: 13,3613 00075 AMOONFLG
056605,001020: 13,3614 77775 VLOAD
056606,001021: 13,3615 00001 RATT
056607,001022: 13,3616 25232 STOVL RN1
056608,001023: 13,3617 00007 VATT
056609,001024: 13,3620 15240 STODL VN1
056610,001025: 13,3621 00015 TAT
056611,001026: 13,3622 01246 STORE PIPTIME1
056612,001027: 13,3623 77776 EXIT
056613,001028:
056614,001029: 13,3624 00004 INHINT
056615,001030: 13,3625 00006 EXTEND
056616,001031: 13,3626 40025 DCS TIME2
056617,001032: 13,3627 20155 DAS MPAC
056618,001033: 13,3630 07226 TC TPAGREE
056619,001034:
056620,001035: 13,3631 31127 CA IRETURN1
056621,001036: 13,3632 04704 TC BANKJUMP
056622,001037: 13,3633 47014 CKMID2 BOF RTB
056623,001038: 13,3634 04754 MID1FLAG
056624,001039: 13,3635 27652 MID2
056625,001040: 13,3636 45510 LOADTIME
056626,001041: 13,3637 44215 DAD BDSU
056627,001042: 13,3640 27711 TIMEDELT
056628,001043: 13,3641 01101 TDEC
056629,001044: 13,3642 45044 BPL CALL
056630,001045: 13,3643 27305 TESTLOOP # YES
|
|
Page 1331
|
056632,001047: 13,3644 27674 NOTIME
056633,001048:
056634,001049: 13,3645 43234 TIMEINC RTB DAD
056635,001050: 13,3646 45510 LOADTIME
056636,001051: 13,3647 03732 T-TO-ADD
056637,001052: 13,3650 35101 STCALL TDEC
056638,001053: 13,3651 27305 TESTLOOP
056639,001054:
056640,001055: 13,3652 45345 MID2 DLOAD DSU
056641,001056: 13,3653 01101 TDEC
056642,001057: 13,3654 01517 TET
056643,001058: 13,3655 45246 ABS DSU
056644,001059: 13,3656 27707 3CSECS
056645,001060: 13,3657 77644 BPL
056646,001061: 13,3660 27645 TIMEINC
056647,001062:
056648,001063: 13,3661 44234 RTB BDSU # SEE IF 5.6 SECS. AVAILABLE TO CALLER.
056649,001064: 13,3662 45510 LOADTIME
056650,001065: 13,3663 01517 TET
056651,001066: 13,3664 51025 DSU BPL
056652,001067: 13,3665 27713 5.6SECS
056653,001068: 13,3666 27176 A-PCHK # YES,GET OUT.
056654,001069:
056655,001070: 13,3667 43345 DLOAD DAD # NO,ADD TIMEDELT TO T-TO-ADD AND TRY
056656,001071: 13,3670 03732 T-TO-ADD # AGAIN.
056657,001072: 13,3671 27711 TIMEDELT
056658,001073: 13,3672 37732 STCALL T-TO-ADD
056659,001074: 13,3673 27645 TIMEINC
056660,001075: 13,3674 77414 NOTIME CLEAR EXIT # TOO LATE
056661,001076: 13,3675 04674 MID1FLAG
056662,001077: 13,3676 25127 INCR IRETURN1 # SET ERROR EXIT (CALLOC +2)
056663,001078: 13,3677 05650 TC ALARM # INSUFFICIENT TIME FOR INTEGRATION --
056664,001079: 13,3700 01703 OCT 1703 # TIG WILL BE SLIPPED...
056665,001080: 13,3701 06006 TC INTPRET
056666,001081: 13,3702 77745 DLOAD
056667,001082: 13,3703 27711 TIMEDELT
056668,001083: 13,3704 03732 STORE T-TO-ADD
056669,001084: 13,3705 77616 RVQ
056670,001085:
056671,001086: 13,3706 00000 00003 3CSECS 2DEC 3 B-28
056672,001087:
056673,001088: 13,3710 00000 02342 TIMEDELT 2DEC 1250 B-28
056674,001089:
056675,001090: 13,3712 00000 01060 5.6SECS 2DEC 560 B-28
056676,001091:
056677,001092: 27,2671 BANK 27
056678,001093: 27,2000 SETLOC UPDATE2
056679,001094: 27,2000 BANK
056680,001095: 27,2671 0330 EBANK= INTWAKUQ
056681,001096:
|
|
Page 1332
|
056683,001098: 27,2671 COUNT* $$/INTIN
056684,001099:
056685,001100: 27,2671 0330 INTWAKUQ = INTWAK1Q # TEMPORARY UNTIL NAME OF INTWAK1Q IS CHNG
056686,001101:
056687,001102: 27,2671 00003 INTWAKEU RELINT
056688,001103: 27,2672 00006 EXTEND
056689,001104: 27,2673 22330 QXCH INTWAKUQ # SAVE Q FOR RETURN
056690,001105:
056691,001106: 27,2674 06006 TC INTPRET
056692,001107:
056693,001108: 27,2675 53135 SLOAD BZE # IS THIS A CSM/LEM STATE VECTOR UPDATE
056694,001109: 27,2676 01502 UPSVFLAG # REQUEST. IF NOT GO TO INTWAKUP.
056695,001110: 27,2677 56736 INTWAKUP
056696,001111:
056697,001112: 27,2700 77775 VLOAD # MOVE RRECT(6) AND VRECT(6) INTO
056698,001113: 27,2701 01503 RRECT # RCV(6) AND VCV(6) RESPECTIVELY.
056699,001114: 27,2702 25535 STOVL RCV
056700,001115: 27,2703 01511 VRECT # NOW GO TO 'RECTIFY +13D' TO
056701,001116: 27,2704 77624 CALL # STORE VRECT INTO VCV AND ZERO OUT
056702,001117: 27,2705 23436 RECTIFY +13D # TDELTAV(6),TNUV(6),TC(2) AND XKEP(2)
056703,001118: 27,2706 51535 SLOAD ABS # COMPARE ABSOLUTE VALUE OF 'UPSVFLAG'
056704,001119: 27,2707 01502 UPSVFLAG # TO 'UPDATE MOON STATE VECTOR CODE'
056705,001120: 27,2710 53025 DSU BZE # TO DETERMINE WHETHER THE STATE VECTOR TO
056706,001121: 27,2711 16747 UPMNSVCD # BE UPDATED IS IN THE EARTH OR LUNAR
056707,001122: 27,2712 56717 INTWAKEM # SPHERE OF INFLUENCE.........
056708,001123: 27,2713 43174 AXT,2 CLRGO # EARTH SPHERE OF INFLUENCE.
056709,001124: 27,2714 00000 DEC 0 B-14
056710,001125: 27,2715 00223 MOONFLAG
056711,001126: 27,2716 56722 INTWAKEC
056712,001127: 27,2717 43174 INTWAKEM AXT,2 SET # LUNAR SPHERE OF INFLUENCE.
056713,001128: 27,2720 00002 DEC 2 B-14
056714,001129: 27,2721 00063 MOONFLAG
056715,001130: 27,2722 50135 INTWAKEC SLOAD BMN # COMMON CODING AFTER X2 INITIALIZED AND
056716,001131: # MOONFLAG SET (OR CLEARED).
056717,001132: 27,2723 01502 UPSVFLAG # IS THIS A REQUEST FOR A LEM OR CSM
056718,001133: 27,2724 56732 INTWAKLM # STATE VECTOR UPDATE......
056719,001134: 27,2725 77624 CALL # UPDATE CSM STATE VECTOR
056720,001135: 27,2726 26705 ATOPCSM
056721,001136:
056722,001137: 27,2727 52014 CLEAR GOTO
056723,001138: 27,2730 01671 ORBWFLAG
056724,001139: 27,2731 56734 INTWAKEX
056725,001140:
056726,001141: 27,2732 77624 INTWAKLM CALL # UPDATE LM STATE VECTOR
056727,001142: 27,2733 26760 ATOPLEM
056728,001143:
056729,001144: 27,2734 77614 INTWAKEX CLEAR
056730,001145: 27,2735 02676 RENDWFLG
056731,001146:
056732,001147: 27,2736 45131 INTWAKUP SSP CALL # REMOVE :UPDATE STATE VECTOR INDICATOR:
|
|
Page 1333
|
056734,001149: 27,2737 01502 UPSVFLAG
056735,001150: 27,2740 00000 0
056736,001151: 27,2741 27455 INTWAKE0 # RELEASE :GRAB: OF ORBIT INTEG
056737,001152: 27,2742 77776 EXIT
056738,001153:
056739,001154: 27,2743 05412 TC PHASCHNG
056740,001155: 27,2744 04026 OCT 04026
056741,001156: 27,2745 00330 TC INTWAKUQ
056742,001157:
056743,001158: 27,2746 00002 UPMNSVCD OCT 2
056744,001159: 27,2747 00000 OCT 0
056745,001160:
056746,001161: 27,2750 77420 GRP2PC STQ EXIT
056747,001162: 27,2751 03536 GRP2SVQ
056748,001163: 27,2752 05412 TC PHASCHNG
056749,001164: 27,2753 04022 OCT 04022
056750,001165: 27,2754 06006 TC INTPRET
056751,001166: 27,2755 77650 GOTO
056752,001167: 27,2756 03536 GRP2SVQ
056753,001168:
056754,001169:
056755,001170:
End of include-file INTEGRATION_INITIALIZATION.agc. Parent file is MAIN.agc