Source Code
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These source-code files are part of a reconstructed copy of Luminary 173, the
second (unflown) release of the Apollo 14 Lunar Module (LM) Apollo Guidance
Computer (AGC) software.
The reconstruction began with reconstructed source code for Luminary 178. Changes
between revision 173 and 178 were backed out, as described by Luminary memo 167
(revision 1). The reconstruction was verified by matching memory-bank checksums
to those listed in drawing 2021152N. Note that page numbers in the reconstructed
code match those for the baseline log section mentioned in each file's changelog;
the page numbers for a real Luminary 173 listing would be different.
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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047935,000002: ## Copyright: Public domain.
047936,000003: ## Filename: PLANETARY_INERTIAL_ORIENTATION.agc
047937,000004: ## Purpose: A section of Luminary revision 173.
047938,000005: ## It is part of the reconstructed source code for the second
047939,000006: ## (unflown) release of the flight software for the Lunar
047940,000007: ## Module's (LM) Apollo Guidance Computer (AGC) for Apollo 14.
047941,000008: ## The code has been recreated from a reconstructed copy of
047942,000009: ## Luminary 178, as well as Luminary memo 167 (revision 1).
047943,000010: ## It has been adapted such that the resulting bugger words
047944,000011: ## exactly match those specified for Luminary 173 in NASA
047945,000012: ## drawing 2021152N, which gives relatively high confidence
047946,000013: ## that the reconstruction is correct.
047947,000014: ## Reference: pp. 1131-1139
047948,000015: ## Assembler: yaYUL
047949,000016: ## Contact: Ron Burkey <info@sandroid.org>.
047950,000017: ## Website: www.ibiblio.org/apollo/index.html
047951,000018: ## Mod history: 2019-09-18 MAS Created from Luminary 178.
047952,000019:
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Page 1131
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047954,000021: # ..... RP-TO-R SUBROUTINE .....
047955,000022: # SUBROUTINE TO CONVERT RP (VECTOR IN PLANETARY COORDINATE SYSTEM,EITHER
047956,000023: # EARTH-FIXED OR MOON-FIXED) TO R (SAME VECTOR IN THE BASIC REF. SYSTEM)
047957,000024:
047958,000025: # R=MT(T)*(RP+LPXRP) MT = M MATRIX TRANSPOSE
047959,000026:
047960,000027: # CALLING SEQUENCE
047961,000028: # L CALL
047962,000029: # L+1 RP-TO-R
047963,000030:
047964,000031: # SUBROUTINES USED
047965,000032: # EARTHMX,MOONMX,EARTHL
047966,000033:
047967,000034: # ITEMS AVAILABLE FROM LAUNCH DATA
047968,000035: # 504LM= THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL,EXPRESSED
047969,000036: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
047970,000037: # ITEMS NECESSARY FOR SUBR. USED (SEE DESCRIPTION OF SUBR.)
047971,000038:
047972,000039: # INPUT
047973,000040: # MPAC= 0 FOR EARTH,NON-ZERO FOR MOON
047974,000041: # 0-5D= RP VECTOR
047975,000042: # 6-7D= TIME
047976,000043:
047977,000044: # OUTPUT
047978,000045: # MPAC= R VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
047979,000046:
047980,000047: 26,2000 SETLOC PLANTIN1
047981,000048: 26,2000 BANK
047982,000049:
047983,000050: 26,3720 COUNT* $$/LUROT
047984,000051:
047985,000052: 26,3720 46020 RP-TO-R STQ BHIZ
047986,000053: 26,3721 00050 RPREXIT
047987,000054: 26,3722 55735 RPTORA
047988,000055: 26,3723 77624 CALL # COMPUTE M MATRIX FOR MOON
047989,000056: 26,3724 51672 MOONMX # LP=LM FOR MOON RADIANS B0
047990,000057: 26,3725 77775 VLOAD
047991,000058: 26,3726 02013 504LM
047992,000059: 26,3727 53235 RPTORB VXV VAD
047993,000060: 26,3730 00001 504RPR
047994,000061: 26,3731 00001 504RPR
047995,000062: 26,3732 52105 VXM GOTO
047996,000063: 26,3733 00025 MMATRIX # MPAC=R=MT(T)*(RP+LPXRP)
047997,000064: 26,3734 51660 RPRPXXXX # RESET PUSHLOC TO 0 BEFORE EXITING
047998,000065: 26,3735 77624 RPTORA CALL # EARTH COMPUTATIONS
047999,000066: 26,3736 55745 EARTHMX # M MATRIX B-1
048000,000067: 26,3737 77624 CALL
048001,000068: 26,3740 15761 EARTHL # L VECTOR RADIANS B0
048002,000069: 26,3741 76521 MXV VSL1 # LP=M(T)*L RAD B-0
048003,000070: 26,3742 00025 MMATRIX
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Page 1132
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048005,000072: 26,3743 77650 GOTO
048006,000073: 26,3744 55727 RPTORB
048007,000074: 24,2000 SETLOC PLANTIN
048008,000075: 24,2000 BANK
048009,000076: 24,3642 COUNT* $$/LUROT
048010,000077:
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Page 1133
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048012,000079: # ..... R-TO-RP SUBROUTINE .....
048013,000080: # SUBROUTINE TO CONVERT R (VECTOR IN REFERENCE COORD. SYSTEM) TO RP
048014,000081: # (VECTOR IN PLANETARY COORD SYSTEM) EITHER EARTH-FIXED OR MOON-FIXED
048015,000082:
048016,000083: # RP=M(T)*(R-LXR)
048017,000084:
048018,000085: # CALLING SEQUENCE
048019,000086: # L CALL
048020,000087: # L+1 R-TO-RP
048021,000088:
048022,000089: # SUBROUTINES USED
048023,000090: # EARTHMX,MOONMX,EARTHL
048024,000091:
048025,000092: # INPUT
048026,000093: # MPAC= 0 FOR EARTH,NON-ZERO FOR MOON
048027,000094: # 0-5D= R VECTOR
048028,000095: # 6-7D= TIME
048029,000096:
048030,000097: # ITEMS AVAILABLE FROM LAUNCH DATA
048031,000098: # 504LM= THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL,EXPRESSED
048032,000099: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
048033,000100: # ITEMS NECESSARY FOR SUBROUTINES USED (SEE DESCRIPTION OF SUBR.)
048034,000101:
048035,000102: # OUTPUT
048036,000103: # MPAC=RP VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
048037,000104:
048038,000105: 24,3642 46020 R-TO-RP STQ BHIZ
048039,000106: 24,3643 00050 RPREXIT
048040,000107: 24,3644 51664 RTORPA
048041,000108: 24,3645 77624 CALL
048042,000109: 24,3646 51672 MOONMX
048043,000110: 24,3647 61375 VLOAD VXM
048044,000111: 24,3650 02013 504LM # LP=LM
048045,000112: 24,3651 00025 MMATRIX
048046,000113: 24,3652 77772 VSL1 # L=MT(T)*LP RADIANS B0
048047,000114: 24,3653 51235 RTORPB VXV BVSU
048048,000115: 24,3654 00001 504RPR
048049,000116: 24,3655 00001 504RPR
048050,000117: 24,3656 77721 MXV # M(T)*(R-LXR) B-2
048051,000118: 24,3657 00025 MMATRIX
048052,000119: 24,3660 40372 RPRPXXXX VSL1 SETPD
048053,000120: 24,3661 00001 0D
048054,000121: 24,3662 77650 GOTO
048055,000122: 24,3663 00050 RPREXIT
048056,000123: 24,3664 77624 RTORPA CALL # EARTH COMPUTATIONS
048057,000124: 24,3665 55745 EARTHMX
048058,000125: 24,3666 77624 CALL
048059,000126: 24,3667 15761 EARTHL
048060,000127: 24,3670 77650 GOTO # MPAC=L=(-AX,-AY,0) RAD B-0
048061,000128: 24,3671 51653 RTORPB
048062,000129:
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Page 1134
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048064,000131: # ..... MOONMX SUBROUTINE .....
048065,000132: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE MOON
048066,000133:
048067,000134: # CALLING SEQUENCE
048068,000135: # L CALL
048069,000136: # L+1 MOONMX
048070,000137:
048071,000138: # SUBROUTINES USED
048072,000139: # NEWANGLE
048073,000140:
048074,000141: # INPUT
048075,000142: # 6-7D= TIME
048076,000143: # ITEMS AVAILABLE FROM LAUNCH DATA
048077,000144: # BSUBO,BDOT
048078,000145: # TIMSUBO,NODIO,NODDOT,FSUBO,FDOT
048079,000146: # COSI= COS(I) B-1
048080,000147: # SINI= SIN(I) B-1
048081,000148: # I IS THE ANGLE BETWEEN THE MEAN LUNAR EQUATORIAL PLANE AND THE
048082,000149: # PLANE OF THE ECLIPTIC (1 DEGREE 32.1 MINUTES)
048083,000150:
048084,000151: # OUTPUT
048085,000152: # MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
048086,000153:
048087,000154: 24,3672 40220 MOONMX STQ SETPD
048088,000155: 24,3673 00051 EARTHMXX
048089,000156: 24,3674 00011 8D
048090,000157: 24,3675 77770 AXT,1 # B REQUIRES SL 0, SL 5 IN NEWANGLE
048091,000158: 24,3676 00005 5
048092,000159: 24,3677 65345 DLOAD PDDL # PD 10D 8-9D=BSUBO
048093,000160: 24,3700 14017 BSUBO # 10-11D= BDOT
048094,000161: 24,3701 14011 BDOT
048095,000162: 24,3702 45006 PUSH CALL # PD 12D
048096,000163: 24,3703 51741 NEWANGLE # EXIT WITH PD 8D AND MPAC= B REVS B0
048097,000164: 24,3704 71406 PUSH COS # PD 10D
048098,000165: 24,3705 14041 STODL COB # PD 8D COS(B) B-1
048099,000166: 24,3706 77756 SIN # SIN(B) B-1
048100,000167: 24,3707 14043 STODL SOB # SETUP INPUT FOR NEWANGLE
048101,000168: 24,3710 14015 FSUBO # 8-9D=FSUBO
048102,000169: 24,3711 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=FDOT
048103,000170: 24,3712 14007 FDOT
048104,000171: 24,3713 45170 AXT,1 CALL # F REQUIRES SL 1, SL 6 IN NEWANGLE
048105,000172: 24,3714 00004 4
048106,000173: 24,3715 51741 NEWANGLE # EXIT WITH PD 8D AND MPAC= F REVS B0
048107,000174: 24,3716 14027 STODL AVECTR +2 # SAVE F TEMP
048108,000175: 24,3717 14013 NODIO # 8-9D=NODIO
048109,000176: 24,3720 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=NODDOT
048110,000177: 24,3721 14005 NODDOT # MPAC=T
048111,000178: 24,3722 45170 AXT,1 CALL # NODE REQUIRES SL 0, SL 5 IN NEWANGLE
048112,000179: 24,3723 00005 5
048113,000180: 24,3724 51741 NEWANGLE # EXIT WITH PD 8D AND MPAC= NODI REVS B0
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Page 1135
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048115,000182: 24,3725 71406 PUSH COS # PD 10D 8-9D= NODI REVS B0
048116,000183: 24,3726 77606 PUSH # PD 12D 10-11D= COS(NODI) B-1
048117,000184: 24,3727 00025 STORE AVECTR
048118,000185: 24,3730 76405 DMP SL1R
048119,000186: 24,3731 00041 COB # COS(NODI) B-1
048120,000187: 24,3732 14035 STODL BVECTR +2 # PD 10D 20-25D=AVECTR= COB*SIN(NODI)
048121,000188: 24,3733 76405 DMP SL1R # SOB*SIN(NODI)
048122,000189: 24,3734 00043 SOB
048123,000190: 24,3735 14037 STODL BVECTR +4 # PD 8D
048124,000191: 24,3736 41556 SIN PUSH # PD 10D -SIN(NODI) B-1
048125,000192: 24,3737 52076 DCOMP GOTO # 26-31D=BVECTR= COV*COS(NODI)
048126,000193: 24,3740 53703 MOONMXA
048127,000194: 25,3703 BANK 25
048128,000195: 25,2000 SETLOC PLANTIN3
048129,000196: 25,2000 BANK
048130,000197: 25,3703 COUNT* $$/LUROT
048131,000198:
048132,000199: 25,3703 14033 MOONMXA STODL BVECTR # PD 8D SOB*COS(NODI)
048133,000200: 25,3704 00027 AVECTR +2 # MOVE F FROM TEMP LOC. TO 504F
048134,000201: 25,3705 14007 STODL 504F
048135,000202: 25,3706 76405 DMP SL1R
048136,000203: 25,3707 00041 COB
048137,000204: 25,3710 14027 STODL AVECTR +2
048138,000205: 25,3711 00011 SINNODI # 8-9D=SIN(NODI) B-1
048139,000206: 25,3712 76405 DMP SL1R
048140,000207: 25,3713 00043 SOB
048141,000208: 25,3714 14031 STODL AVECTR +4 # 0
048142,000209: 25,3715 06520 HI6ZEROS # 8-13D= CVECTR= -SOB B-1
048143,000210: 25,3716 57525 PDDL DCOMP # PD 10D COB
048144,000211: 25,3717 00043 SOB
048145,000212: 25,3720 63325 PDDL PDVL # PD 12D THEN PD 14D
048146,000213: 25,3721 00041 COB
048147,000214: 25,3722 00033 BVECTR
048148,000215: 25,3723 63361 VXSC PDVL # PD 20D BVECTR*SINI B-2
048149,000216: 25,3724 14003 SINI
048150,000217: 25,3725 00011 CVECTR
048151,000218: 25,3726 53361 VXSC VAD # PD 14D CVECTR*COSI B-2
048152,000219: 25,3727 14001 COSI
048153,000220: 25,3730 77772 VSL1
048154,000221: 25,3731 24041 STOVL MMATRIX +12D # PD 8D M2=BVECTR*SINI+CVECTR*COSI B-1
048155,000222: 25,3732 63361 VXSC PDVL # PD 14D
048156,000223: 25,3733 14003 SINI # CVECTR*SINI B-2
048157,000224: 25,3734 00033 BVECTR
048158,000225: 25,3735 52361 VXSC VSU # PD 8D BVECTR*COSI B-2
048159,000226: 25,3736 14001 COSI
048160,000227: 25,3737 65372 VSL1 PDDL # PD 14D
048161,000228: 25,3740 00007 504F # 8-13D=DVECTR=BVECTR*COSI-CVECTR*SINI B-1
048162,000229: 25,3741 74346 COS VXSC
048163,000230: 25,3742 00011 DVECTR
048164,000231: 25,3743 73525 PDDL SIN # PD 20D 14-19D= DVECTR*COSF B-2
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Page 1136
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048166,000233: 25,3744 00007 504F
048167,000234: 25,3745 52361 VXSC VSU # PD 14D AVECTR*SINF B-2
048168,000235: 25,3746 00025 AVECTR
048169,000236: 25,3747 77772 VSL1
048170,000237: 25,3750 14033 STODL MMATRIX +6 # M1= AVECTR*SINF-DVECTR*COSF B-1
048171,000238: 25,3751 00007 504F
048172,000239: 25,3752 74356 SIN VXSC # PD 8D
048173,000240: 25,3753 71525 PDDL COS # PD 14D 8-13D=DVECTR*SINF B-2
048174,000241: 25,3754 00007 504F
048175,000242: 25,3755 53361 VXSC VAD # PD 8D AVECTR*COSF B-2
048176,000243: 25,3756 00025 AVECTR
048177,000244: 25,3757 57572 VSL1 VCOMP
048178,000245: 25,3760 34025 STCALL MMATRIX # M0= -(AVECTR*COSF+DVECTR*SINF) B-1
048179,000246: 25,3761 00051 EARTHMXX
048180,000247: # COMPUTE X=X0+(XDOT)(T+T0)
048181,000248: # 8-9D= XO (REVS B-0),PUSHLOC SET AT 12D
048182,000249: # 10-11D=XDOT (REVS/CSEC) SCALED B+23 FOR WEARTH,B+28 FOR NODDOT AND BDOT
048183,000250: # AND B+27 FOR FDOT
048184,000251: # X1=DIFFERENCE IN 23 AND SCALING OF XDOT,=0 FOR WEARTH,5 FOR NODDOT AND
048185,000252: # BDOT AND 4 FOR FDOT
048186,000253: # 6-7D=T (CSEC B-28), TIMSUBO= (CSEC B-42 TRIPLE PREC.)
048187,000254:
048188,000255: 24,3741 BANK 24
048189,000256: 24,2000 SETLOC PLANTIN
048190,000257: 24,2000 BANK
048191,000258:
048192,000259: 24,3741 54345 NEWANGLE DLOAD SR # ENTER PD 12D
048193,000260: 24,3742 00007 6D
048194,000261: 24,3743 20617 14D
048195,000262: 24,3744 72371 TAD TLOAD # CHANGE MODE TO TP
048196,000263: 24,3745 01707 TIMSUBO
048197,000264: 24,3746 00155 MPAC
048198,000265: 24,3747 14017 STODL TIMSUBM # T+T0 CSEC B-42
048199,000266: 24,3750 00020 TIMSUBM +1
048200,000267: 24,3751 77605 DMP # PD 10D MULT BY XDOT IN 10-11D
048201,000268: 24,3752 43257 SL* DAD # PD 8D ADD XO IN 8-9D AFTER SHIFTING
048202,000269: 24,3753 20206 5,1 # SUCH THAT SCALING IS B-0
048203,000270: 24,3754 67206 PUSH SLOAD # PD 10D SAVE PARTIAL (X0+XDOT*T) IN 8-9D
048204,000271: 24,3755 00017 TIMSUBM
048205,000272: 24,3756 41261 SL DMP
048206,000273: 24,3757 20212 9D
048207,000274: 24,3760 00013 10D # XDOT
048208,000275: 24,3761 43257 SL* DAD # PD 8D SHIFT SUCH THAT THIS PART OF X
048209,000276: 24,3762 20213 10D,1 # IS SCALED REVS/CSEC B-0
048210,000277: 24,3763 77600 BOV # TURN OFF OVERFLOW IF SET BY SHIFT
048211,000278: 24,3764 51765 +1 # INSTRUCTION BEFORE EXITING
048212,000279: 24,3765 77616 RVQ # MPAC=X= X0+(XDOT)(T+T0) REVS B0
048213,000280:
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Page 1137
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048215,000282: # ..... EARTHMX SUBROUTINE .....
048216,000283: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE EARTH
048217,000284:
048218,000285: # CALLING SEQUENCE
048219,000286: # L CALL
048220,000287: # L+1 EARTHMX
048221,000288:
048222,000289: # SUBROUTINES USED
048223,000290: # NEWANGLE
048224,000291:
048225,000292: # INPUT
048226,000293: # INPUT AVAILABLE FROM LAUNCH DATA AZO REVS B-0
048227,000294: # TEPHEM CSEC B-42
048228,000295: # 6-7D= TIME CSEC B-28
048229,000296:
048230,000297: # OUTPUT
048231,000298: # MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
048232,000299:
048233,000300: 26,3745 BANK 26
048234,000301: 26,2000 SETLOC PLANTIN1
048235,000302: 26,2000 BANK
048236,000303: 26,3745 COUNT* $$/LUROT
048237,000304:
048238,000305: 26,3745 40220 EARTHMX STQ SETPD # SET 8-9D=AZO
048239,000306: 26,3746 00051 EARTHMXX
048240,000307: 26,3747 00011 8D # 10-11D=WEARTH
048241,000308: 26,3750 77770 AXT,1 # FOR SL 5, AND SL 10 IN NEWANGLE
048242,000309: 26,3751 00000 0
048243,000310: 26,3752 65345 DLOAD PDDL # LEAVING PD SET AT 12D FOR NEWANGLE
048244,000311: 26,3753 14023 AZO
048245,000312: 26,3754 14021 WEARTH
048246,000313: 26,3755 45006 PUSH CALL
048247,000314: 26,3756 51741 NEWANGLE
048248,000315: 26,3757 41401 SETPD PUSH # 18-19D=504AZ
048249,000316: 26,3760 00023 18D # COS(AZ) SIN(AZ) 0
048250,000317: 26,3761 65346 COS PDDL # 20-37D= MMATRIX= -SIN(AZ) COS(AZ) 0 B-1
048251,000318: 26,3762 00023 504AZ # 0 0 1
048252,000319: 26,3763 65356 SIN PDDL
048253,000320: 26,3764 06520 HI6ZEROS
048254,000321: 26,3765 73525 PDDL SIN
048255,000322: 26,3766 00023 504AZ
048256,000323: 26,3767 65276 DCOMP PDDL
048257,000324: 26,3770 00023 504AZ
048258,000325: 26,3771 63346 COS PDVL
048259,000326: 26,3772 06520 HI6ZEROS
048260,000327: 26,3773 41525 PDDL PUSH
048261,000328: 26,3774 06516 HIDPHALF
048262,000329: 26,3775 77650 GOTO
048263,000330: 26,3776 00051 EARTHMXX
048264,000331:
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Page 1138
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048266,000333: # ..... EARTHL SUBROUTINE .....
048267,000334: # SUBROUTINE TO COMPUTE L VECTOR FOR EARTH
048268,000335:
048269,000336: # CALLING SEQUENCE
048270,000337: # L CALL
048271,000338: # L+1 EARTHL
048272,000339:
048273,000340: # INPUT
048274,000341: # AXO,AYO SET AT LAUNCH TIME WITH AYO IMMEDIATELY FOLLOWING AXO IN CORE
048275,000342:
048276,000343: # OUTPUT
048277,000344: # -AX
048278,000345: # MPAC= -AY RADIANS B-0
048279,000346: # 0
048280,000347:
048281,000348: 06,3761 BANK 06
048282,000349: 06,2000 SETLOC EARTHLOC
048283,000350: 06,2000 BANK
048284,000351: 06,3761 COUNT* $$/LUROT
048285,000352:
048286,000353: 06,3761 57545 EARTHL DLOAD DCOMP
048287,000354: 06,3762 01714 AXO
048288,000355: 06,3763 14017 STODL 504LPL
048289,000356: 06,3764 01712 -AYO
048290,000357: 06,3765 14021 STODL 504LPL +2
048291,000358: 06,3766 24007 LO6ZEROS
048292,000359: 06,3767 24023 STOVL 504LPL +4
048293,000360: 06,3770 00017 504LPL
048294,000361: 06,3771 77616 RVQ
048295,000362:
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Page 1139
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048297,000364: # CONSTANTS AND ERASABLE ASSIGNMENTS
048298,000365: 06,3772 12,2004 1B1 = DP1/2 # 1 SCALED B-1
048299,000366: 06,3772 0000050 RPREXIT = S1 # R-TO-RP AND RP-TO-R SUBR EXIT
048300,000367: 06,3772 0000051 EARTHMXX = S2 # EARTHMX,MOONMX SUBR. EXITS
048301,000368: 06,3772 504RPR = 0D # 6 REGS R OR RP VECTOR
048302,000369: 06,3772 SINNODI = 8D # 2 SIN(NODI)
048303,000370: 06,3772 DVECTR = 8D # 6 D VECTOR MOON
048304,000371: 06,3772 CVECTR = 8D # 6 C VECTR MOON
048305,000372: 06,3772 504AZ = 18D # 2 AZ
048306,000373: 06,3772 TIMSUBM = 14D # 3 TIME SUB M (MOON) T+T0 IN GETAZ
048307,000374: 06,3772 504LPL = 14D # 6 L OR LP VECTOR
048308,000375: 06,3772 AVECTR = 20D # 6 A VECTOR (MOON)
048309,000376: 06,3772 BVECTR = 26D # 6 B VECTOR (MOON)
048310,000377: 06,3772 MMATRIX = 20D # 18 M MATRIX
048311,000378: 06,3772 COB = 32D # 2 COS(B) B-1
048312,000379: 06,3772 SOB = 34D # 2 SIN(B) B-1
048313,000380: 06,3772 504F = 6D # 2 F(MOON)
End of include-file PLANETARY_INERTIAL_ORIENTATION.agc. Parent file is MAIN.agc