Source Code
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These source-code files are part of a reconstructed copy of Luminary 97, the
original release of the Apollo 11 Lunar Module (LM) Apollo Guidance Computer
(AGC) software.
The reconstruction began with source code of Luminary 99 revision 1 previously
transcribed from a digitized copy of that program. The code was then updated
by undoing changes described in original Luminary memos 83 and 85, using asterisks
indicating changed lines in the listing as a guide. The reconstruction was
verified by matching memory-bank checksums to those listed in drawing 2021152D.
Note that page numbers in the reconstructed code match those on the Luminary 099
revision 001 printout, although the added code would likely have changed page
numbers for a real Luminary 97 listing.
Comments from 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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047696,000002: ## Copyright: Public domain.
047697,000003: ## Filename: PLANETARY_INERTIAL_ORIENTATION.agc
047698,000004: ## Purpose: A section of Luminary revision 97.
047699,000005: ## It is part of the reconstructed source code for the
047700,000006: ## original release of the flight software for the Lunar
047701,000007: ## Module's (LM) Apollo Guidance Computer (AGC) for Apollo 11.
047702,000008: ## The code has been recreated from a copy of Luminary 99
047703,000009: ## revision 001, using asterisks indicating changed lines in
047704,000010: ## the listing and Luminary Memos #83 and #85, which list
047705,000011: ## changes between Luminary 97 and 98, and 98 and 99. The
047706,000012: ## code has been adapted such that the resulting bugger words
047707,000013: ## exactly match those specified for Luminary 97 in NASA drawing
047708,000014: ## 2021152D, which gives relatively high confidence that the
047709,000015: ## reconstruction is correct.
047710,000016: ## Reference: pp. 1140-1148
047711,000017: ## Assembler: yaYUL
047712,000018: ## Contact: Ron Burkey <info@sandroid.org>.
047713,000019: ## Website: www.ibiblio.org/apollo/index.html
047714,000020: ## Mod history: 2019-07-28 MAS Created from Luminary 99.
047715,000021:
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Page 1140
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047717,000023: # ..... RP-TO-R SUBROUTINE .....
047718,000024: # SUBROUTINE TO CONVERT RP (VECTOR IN PLANETARY COORDINATE SYSTEM, EITHER
047719,000025: # EARTH-FIXED OR MOON-FIXED) TO R (SAME VECTOR IN THE BASIC REF. SYSTEM)
047720,000026:
047721,000027: # R = MT(T) * (RP + LP X RP) MT = M MATRIX TRANSPOSE
047722,000028:
047723,000029: # CALLING SEQUENCE
047724,000030: # L CALL
047725,000031: # L+1 RP-TO-R
047726,000032:
047727,000033: # SUBROUTINES USED
047728,000034: # EARTHMX, MOONMX, EARTHL
047729,000035:
047730,000036: # ITEMS AVAILABLE FROM LAUNCH DATA
047731,000037: # 504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
047732,000038: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
047733,000039:
047734,000040: # ITEMS NECESSARY FOR SUBR. USED (SEE DESCRIPTION OF SUBR.)
047735,000041:
047736,000042: # INPUT
047737,000043: # MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
047738,000044: # 0-5D = RP VECTOR
047739,000045: # 6-7D = TIME
047740,000046:
047741,000047: # OUTPUT
047742,000048: # MPAC = R VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
047743,000049:
047744,000050: 26,2000 SETLOC PLANTIN1
047745,000051: 26,2000 BANK
047746,000052:
047747,000053: 26,3716 COUNT* $$/LUROT
047748,000054:
047749,000055: 26,3716 46020 RP-TO-R STQ BHIZ
047750,000056: 26,3717 00050 RPREXIT
047751,000057: 26,3720 55733 RPTORA
047752,000058: 26,3721 77624 CALL # COMPUTE M MATRIX FOR MOON
047753,000059: 26,3722 51720 MOONMX # LP=LM FOR MOON RADIANS B0
047754,000060: 26,3723 77775 VLOAD
047755,000061: 26,3724 02013 504LM
047756,000062: 26,3725 53235 RPTORB VXV VAD
047757,000063: 26,3726 00001 504RPR
047758,000064: 26,3727 00001 504RPR
047759,000065: 26,3730 52105 VXM GOTO
047760,000066: 26,3731 00025 MMATRIX # MPAC=R=MT(T)*(RP+LPXRP)
047761,000067: 26,3732 51706 RPRPXXXX # RESET PUSHLOC TO 0 BEFORE EXITING
047762,000068: 26,3733 77624 RPTORA CALL # EARTH COMPUTATIONS
047763,000069: 26,3734 55743 EARTHMX # M MATRIX B-1
047764,000070: 26,3735 77624 CALL
047765,000071: 26,3736 15753 EARTHL # L VECTOR RADIANS B0
047766,000072: 26,3737 76521 MXV VSL1 # LP=M(T)*L RAD B-0
047767,000073: 26,3740 00025 MMATRIX
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Page 1141
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047769,000075: 26,3741 77650 GOTO
047770,000076: 26,3742 55725 RPTORB
047771,000077: 24,2000 SETLOC PLANTIN
047772,000078: 24,2000 BANK
047773,000079: 24,3670 COUNT* $$/LUROT
047774,000080:
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Page 1142
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047776,000082: # ..... R-TO-RP SUBROUTINE .....
047777,000083: # SUBROUTINE TO CONVERT R (VECTOR IN REFERENCE COORD. SYSTEM) TO RP
047778,000084: # (VECTOR IN PLANETARY COORD SYSTEM) EITHER EARTH-FIXED OR MOON-FIXED
047779,000085:
047780,000086: # RP = M(T) * (R - L X R)
047781,000087:
047782,000088: # CALLING SEQUENCE
047783,000089: # L CALL
047784,000090: # L+1 R-TO-RP
047785,000091:
047786,000092: # SUBROUTINES USED
047787,000093: # EARTHMX, MOONMX, EARTHL
047788,000094:
047789,000095: # INPUT
047790,000096: # MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
047791,000097: # 0-5D = R VECTOR
047792,000098: # 6-7D = TIME
047793,000099:
047794,000100: # ITEMS AVAILABLE FROM LAUNCH DATA
047795,000101: # 504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
047796,000102: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
047797,000103:
047798,000104: # ITEMS NECESSARY FOR SUBROUTINES USED (SEE DESCRIPTION OF SUBR.)
047799,000105:
047800,000106: # OUTPUT
047801,000107: # MPAC = RP VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
047802,000108:
047803,000109: 24,3670 46020 R-TO-RP STQ BHIZ
047804,000110: 24,3671 00050 RPREXIT
047805,000111: 24,3672 51712 RTORPA
047806,000112: 24,3673 77624 CALL
047807,000113: 24,3674 51720 MOONMX
047808,000114: 24,3675 61375 VLOAD VXM
047809,000115: 24,3676 02013 504LM # LP=LM
047810,000116: 24,3677 00025 MMATRIX
047811,000117: 24,3700 77772 VSL1 # L = MT(T)*LP RADIANS B0
047812,000118: 24,3701 51235 RTORPB VXV BVSU
047813,000119: 24,3702 00001 504RPR
047814,000120: 24,3703 00001 504RPR
047815,000121: 24,3704 77721 MXV # M(T)*(R-LXR) B-2
047816,000122: 24,3705 00025 MMATRIX
047817,000123: 24,3706 40372 RPRPXXXX VSL1 SETPD
047818,000124: 24,3707 00001 0D
047819,000125: 24,3710 77650 GOTO
047820,000126: 24,3711 00050 RPREXIT
047821,000127: 24,3712 77624 RTORPA CALL # EARTH COMPUTATIONS
047822,000128: 24,3713 55743 EARTHMX
047823,000129: 24,3714 77624 CALL
047824,000130: 24,3715 15753 EARTHL
047825,000131: 24,3716 77650 GOTO # MPAC=L=(-AX,-AY,0) RAD B-0
047826,000132: 24,3717 51701 RTORPB
047827,000133:
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Page 1143
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047829,000135: # ..... MOONMX SUBROUTINE .....
047830,000136: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE MOON
047831,000137:
047832,000138: # CALLING SEQUENCE
047833,000139: # L CALL
047834,000140: # L+1 MOONMX
047835,000141:
047836,000142: # SUBROUTINES USED
047837,000143: # NEWANGLE
047838,000144:
047839,000145: # INPUT
047840,000146: # 6-7D = TIME
047841,000147:
047842,000148: # ITEMS AVAILABLE FROM LAUNCH DATA
047843,000149: # BSUBO, BDOT
047844,000150: # TIMSUBO, NODIO, NODDOT, FSUBO, FDOT
047845,000151: # COSI = COS(I) B-1
047846,000152: # SINI = SIN(I) B-1
047847,000153: # I IS THE ANGLE BETWEEN THE MEAN LUNAR EQUATORIAL PLANE AND THE
047848,000154: # PLANE OF THE ECLIPTIC (1 DEGREE 32.1 MINUTES)
047849,000155:
047850,000156: # OUTPUT
047851,000157: # MMATRIX = 3X3 M MATRIX B-1 (STORED IN VAC AREA)
047852,000158:
047853,000159: 24,3720 40220 MOONMX STQ SETPD
047854,000160: 24,3721 00051 EARTHMXX
047855,000161: 24,3722 00011 8D
047856,000162: 24,3723 77770 AXT,1 # B REQUIRES SL 0, SL 5 IN NEWANGLE
047857,000163: 24,3724 00005 5
047858,000164: 24,3725 65345 DLOAD PDDL # PD 10D 8-9D=BSUBO
047859,000165: 24,3726 14017 BSUBO # 10-11D=BDOT
047860,000166: 24,3727 14011 BDOT
047861,000167: 24,3730 45006 PUSH CALL # PD 12D
047862,000168: 24,3731 53743 NEWANGLE # EXIT WITH PD 8D AND MPAC= B REVS B0
047863,000169: 24,3732 71406 PUSH COS # PD 10D
047864,000170: 24,3733 14041 STODL COB # PD 8D COS(B) B-1
047865,000171: 24,3734 77756 SIN # SIN(B) B-1
047866,000172: 24,3735 14043 STODL SOB # SETUP INPUT FOR NEWANGLE
047867,000173: 24,3736 14015 FSUBO # 8-9D=FSUBO
047868,000174: 24,3737 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=FDOT
047869,000175: 24,3740 14007 FDOT
047870,000176: 24,3741 45170 AXT,1 CALL # F REQUIRES SL 1, SL 6 IN NEWANGLE
047871,000177: 24,3742 00004 4
047872,000178: 24,3743 53743 NEWANGLE # EXIT WITH PD 8D AND MPAC= F REVS B0
047873,000179: 24,3744 14027 STODL AVECTR +2 # SAVE F TEMP
047874,000180: 24,3745 14013 NODIO # 8-9D=NODIO
047875,000181: 24,3746 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=NODDOT
047876,000182: 24,3747 14005 NODDOT # MPAC=T
047877,000183: 24,3750 45170 AXT,1 CALL # NODE REQUIRES SL 0, SL 5 IN NEWANGLE
047878,000184: 24,3751 00005 5
047879,000185: 24,3752 53743 NEWANGLE # EXIT WITH PD 8D AND MPAC= NODI REVS B0
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Page 1144
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047881,000187: 24,3753 71406 PUSH COS # PD 10D 8-9D= NODI REVS B0
047882,000188: 24,3754 77606 PUSH # PD 12D 10-11D= COS(NODI) B-1
047883,000189: 24,3755 00025 STORE AVECTR
047884,000190: 24,3756 76405 DMP SL1R
047885,000191: 24,3757 00041 COB # COS(NODI) B-1
047886,000192: 24,3760 14035 STODL BVECTR +2 # PD 10D 20-25D=AVECTR= COB*SIN(NODI)
047887,000193: 24,3761 76405 DMP SL1R # SOB*SIN(NODI)
047888,000194: 24,3762 00043 SOB
047889,000195: 24,3763 14037 STODL BVECTR +4 # PD 8D
047890,000196: 24,3764 41556 SIN PUSH # PD 10D -SIN(NODI) B-1
047891,000197: 24,3765 77676 DCOMP # 26-31D=BVECTR= COB*COS(NODI)
047892,000198: 24,3766 14033 STODL BVECTR # PD 8D SOB*COS(NODI)
047893,000199: 24,3767 00027 AVECTR +2 # MOVE F FROM TEMP LOC. TO 504F
047894,000200: 24,3770 14007 STODL 504F
047895,000201: 24,3771 76405 DMP SL1R
047896,000202: 24,3772 00041 COB
047897,000203: 24,3773 77650 GOTO
047898,000204: 24,3774 53671 MOONMXA
047899,000205:
047900,000206: 25,3671 BANK 25
047901,000207: 25,2000 SETLOC PLANTIN3
047902,000208: 25,2000 BANK
047903,000209: 25,3671 COUNT* $$/LUROT
047904,000210:
047905,000211: 25,3671 14027 MOONMXA STODL AVECTR +2
047906,000212: 25,3672 00011 SINNODI # 8-9D=SIN(NODI) B-1
047907,000213: 25,3673 76405 DMP SL1R
047908,000214: 25,3674 00043 SOB
047909,000215: 25,3675 14031 STODL AVECTR +4 # 0
047910,000216: 25,3676 06522 HI6ZEROS # 8-13D= CVECTR= -SOB B-1
047911,000217: 25,3677 57525 PDDL DCOMP # PD 10D COB
047912,000218: 25,3700 00043 SOB
047913,000219: 25,3701 63325 PDDL PDVL # PD 12D THEN PD 14D
047914,000220: 25,3702 00041 COB
047915,000221: 25,3703 00033 BVECTR
047916,000222: 25,3704 63361 VXSC PDVL # PD 20D BVECTR*SINI B-2
047917,000223: 25,3705 14003 SINI
047918,000224: 25,3706 00011 CVECTR
047919,000225: 25,3707 53361 VXSC VAD # PD 14D CVECTR*COSI B-2
047920,000226: 25,3710 14001 COSI
047921,000227: 25,3711 77772 VSL1
047922,000228: 25,3712 24041 STOVL MMATRIX +12D # PD 8D M2=BVECTR*SINI+CVECTR*COSI B-1
047923,000229: 25,3713 63361 VXSC PDVL # PD 14D
047924,000230: 25,3714 14003 SINI # CVECTR*SINI B-2
047925,000231: 25,3715 00033 BVECTR
047926,000232: 25,3716 52361 VXSC VSU # PD 8D BVECTR*COSI B-2
047927,000233: 25,3717 14001 COSI
047928,000234: 25,3720 65372 VSL1 PDDL # PD 14D
047929,000235: 25,3721 00007 504F # 8-13D=DVECTR=BVECTR*COSI-CVECTR*SINI B-1
047930,000236: 25,3722 74346 COS VXSC
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Page 1145
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047932,000238: 25,3723 00011 DVECTR
047933,000239: 25,3724 73525 PDDL SIN # PD 20D 14-19D= DVECTR*COSF B-2
047934,000240: 25,3725 00007 504F
047935,000241: 25,3726 52361 VXSC VSU # PD 14D AVECTR*SINF B-2
047936,000242: 25,3727 00025 AVECTR
047937,000243: 25,3730 77772 VSL1
047938,000244: 25,3731 14033 STODL MMATRIX +6 # M1= AVECTR*SINF-DVECTR*COSF B-1
047939,000245: 25,3732 00007 504F
047940,000246: 25,3733 74356 SIN VXSC # PD 8D
047941,000247: 25,3734 71525 PDDL COS # PD 14D 8-13D=DVECTR*SINF B-2
047942,000248: 25,3735 00007 504F
047943,000249: 25,3736 53361 VXSC VAD # PD 8D AVECTR*COSF B-2
047944,000250: 25,3737 00025 AVECTR
047945,000251: 25,3740 57572 VSL1 VCOMP
047946,000252: 25,3741 34025 STCALL MMATRIX # M0= -(AVECTR*COSF+DVECTR*SINF) B-1
047947,000253: 25,3742 00051 EARTHMXX
047948,000254:
047949,000255: # COMPUTE X=X0+(XDOT)(T+T0)
047950,000256: # 8-9D= XO (REVS B-0), PUSHLOC SET AT 12D
047951,000257: # 10-11D=XDOT (REVS/CSEC) SCALED B+23 FOR WEARTH,B+28 FOR NODDOT AND BDOT
047952,000258: # AND B+27 FOR FDOT
047953,000259: # X1=DIFFERENCE IN 23 AND SCALING OF XDOT, =0 FOR WEARTH, 5 FOR NODDOT AND
047954,000260: # BDOT AND 4 FOR FDOT
047955,000261: # 6-7D=T (CSEC B-28), TIMSUBO= (CSEC B-42 TRIPLE PREC.)
047956,000262:
047957,000263: 25,3743 54345 NEWANGLE DLOAD SR # ENTER PD 12D
047958,000264: 25,3744 00007 6D
047959,000265: 25,3745 20617 14D
047960,000266: 25,3746 72371 TAD TLOAD # CHANGE MODE TO TP
047961,000267: 25,3747 01707 TIMSUBO
047962,000268: 25,3750 00155 MPAC
047963,000269: 25,3751 14017 STODL TIMSUBM # T+T0 CSEC B-42
047964,000270: 25,3752 00020 TIMSUBM +1
047965,000271: 25,3753 77605 DMP # PD 10D MULT BY XDOT IN 10-11D
047966,000272: 25,3754 43257 SL* DAD # PD 8D ADD XO IN 8-9D AFTER SHIFTING
047967,000273: 25,3755 20206 5,1 # SUCH THAT SCALING IS B-0
047968,000274: 25,3756 67206 PUSH SLOAD # PD 10D SAVE PARTIAL (X0+XDOT*T) IN 8-9D
047969,000275: 25,3757 00017 TIMSUBM
047970,000276: 25,3760 41261 SL DMP
047971,000277: 25,3761 20212 9D
047972,000278: 25,3762 00013 10D # XDOT
047973,000279: 25,3763 43257 SL* DAD # PD 8D SHIFT SUCH THAT THIS PART OF X
047974,000280: 25,3764 20213 10D,1 # IS SCALED REVS/CSEC B-0
047975,000281: 25,3765 77600 BOV # TURN OFF OVERFLOW IF SET BY SHIFT
047976,000282: 25,3766 53767 +1 # INSTRUCTION BEFORE EXITING
047977,000283: 25,3767 77616 RVQ # MPAC=X= X0+(XDOT)(T+T0) REVS B0
047978,000284:
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Page 1146
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047980,000286: # ..... EARTHMX SUBROUTINE .....
047981,000287: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE EARTH
047982,000288:
047983,000289: # CALLING SEQUENCE
047984,000290: # L CALL
047985,000291: # L+1 EARTHMX
047986,000292:
047987,000293: # SUBROUTINES USED
047988,000294: # NEWANGLE
047989,000295:
047990,000296: # INPUT
047991,000297: # INPUT AVAILABLE FROM LAUNCH DATA AZO REVS B-0
047992,000298: # TEPHEM CSEC B-42
047993,000299: # 6-7D= TIME CSEC B-28
047994,000300:
047995,000301: # OUTPUT
047996,000302: # MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
047997,000303:
047998,000304: 26,3743 BANK 26
047999,000305: 26,2000 SETLOC PLANTIN1
048000,000306: 26,2000 BANK
048001,000307: 26,3743 COUNT* $$/LUROT
048002,000308:
048003,000309: 26,3743 40220 EARTHMX STQ SETPD # SET 8-9D=AZO
048004,000310: 26,3744 00051 EARTHMXX
048005,000311: 26,3745 00011 8D # 10-11D=WEARTH
048006,000312: 26,3746 77770 AXT,1 # FOR SL 5, AND SL 10 IN NEWANGLE
048007,000313: 26,3747 00000 0
048008,000314: 26,3750 65345 DLOAD PDDL # LEAVING PD SET AT 12D FOR NEWANGLE
048009,000315: 26,3751 01712 AZO
048010,000316: 26,3752 14021 WEARTH
048011,000317: 26,3753 45006 PUSH CALL
048012,000318: 26,3754 53743 NEWANGLE
048013,000319: 26,3755 41401 SETPD PUSH # 18-19D=504AZ
048014,000320: 26,3756 00023 18D # COS(AZ) SIN(AZ) 0
048015,000321: 26,3757 65346 COS PDDL # 20-37D= MMATRIX= -SIN(AZ) COS(AZ) 0 B-1
048016,000322: 26,3760 00023 504AZ # 0 0 1
048017,000323: 26,3761 65356 SIN PDDL
048018,000324: 26,3762 06522 HI6ZEROS
048019,000325: 26,3763 73525 PDDL SIN
048020,000326: 26,3764 00023 504AZ
048021,000327: 26,3765 65276 DCOMP PDDL
048022,000328: 26,3766 00023 504AZ
048023,000329: 26,3767 63346 COS PDVL
048024,000330: 26,3770 06522 HI6ZEROS
048025,000331: 26,3771 41525 PDDL PUSH
048026,000332: 26,3772 06520 HIDPHALF
048027,000333: 26,3773 77650 GOTO
048028,000334: 26,3774 00051 EARTHMXX
048029,000335:
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Page 1147
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048031,000337: # ..... EARTHL SUBROUTINE .....
048032,000338: # SUBROUTINE TO COMPUTE L VECTOR FOR EARTH
048033,000339:
048034,000340: # CALLING SEQUENCE
048035,000341: # L CALL
048036,000342: # L+1 EARTHL
048037,000343:
048038,000344: # INPUT
048039,000345: # AXO,AYO SET AT LAUNCH TIME WITH AYO IMMEDIATELY FOLLOWING AXO IN CORE
048040,000346:
048041,000347: # OUTPUT
048042,000348: # -AX
048043,000349: # MPAC= -AY RADIANS B-0
048044,000350: # 0
048045,000351:
048046,000352: 06,3753 BANK 06
048047,000353: 06,2000 SETLOC EARTHLOC
048048,000354: 06,2000 BANK
048049,000355: 06,3753 COUNT* $$/LUROT
048050,000356:
048051,000357: 06,3753 57545 EARTHL DLOAD DCOMP
048052,000358: 06,3754 01716 AXO
048053,000359: 06,3755 14017 STODL 504LPL
048054,000360: 06,3756 01714 -AYO
048055,000361: 06,3757 14021 STODL 504LPL +2
048056,000362: 06,3760 24007 LO6ZEROS
048057,000363: 06,3761 24023 STOVL 504LPL +4
048058,000364: 06,3762 00017 504LPL
048059,000365: 06,3763 77616 RVQ
048060,000366:
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Page 1148
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048062,000368: # CONSTANTS AND ERASABLE ASSIGNMENTS
048063,000369:
048064,000370: 06,3764 12,2004 1B1 = DP1/2 # 1 SCALED B-1
048065,000371: 06,3764 0000050 RPREXIT = S1 # R-TO-RP AND RP-TO-R SUBR EXIT
048066,000372: 06,3764 0000051 EARTHMXX = S2 # EARTHMX, MOONMX SUBR. EXITS
048067,000373: 06,3764 504RPR = 0D # 6 REGS R OR RP VECTOR
048068,000374: 06,3764 SINNODI = 8D # 2 SIN(NODI)
048069,000375: 06,3764 DVECTR = 8D # 6 D VECTOR MOON
048070,000376: 06,3764 CVECTR = 8D # 6 C VECTR MOON
048071,000377: 06,3764 504AZ = 18D # 2 AZ
048072,000378: 06,3764 TIMSUBM = 14D # 3 TIME SUB M (MOON) T+T0 IN GETAZ
048073,000379: 06,3764 504LPL = 14D # 6 L OR LP VECTOR
048074,000380: 06,3764 AVECTR = 20D # 6 A VECTOR (MOON)
048075,000381: 06,3764 BVECTR = 26D # 6 B VECTOR (MOON)
048076,000382: 06,3764 MMATRIX = 20D # 18 M MATRIX
048077,000383: 06,3764 COB = 32D # 2 COS(B) B-1
048078,000384: 06,3764 SOB = 34D # 2 SIN(B) B-1
048079,000385: 06,3764 504F = 6D # 2 F(MOON)
048080,000386:
End of include-file PLANETARY_INERTIAL_ORIENTATION.agc. Parent file is MAIN.agc