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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047948,000002: ## Copyright: Public domain.
047949,000003: ## Filename: PLANETARY_INERTIAL_ORIENTATION.agc
047950,000004: ## Purpose: A section of Luminary revision 173.
047951,000005: ## It is part of the reconstructed source code for the second
047952,000006: ## (unflown) release of the flight software for the Lunar
047953,000007: ## Module's (LM) Apollo Guidance Computer (AGC) for Apollo 14.
047954,000008: ## The code has been recreated from a reconstructed copy of
047955,000009: ## Luminary 178, as well as Luminary memo 167 (revision 1).
047956,000010: ## It has been adapted such that the resulting bugger words
047957,000011: ## exactly match those specified for Luminary 173 in NASA
047958,000012: ## drawing 2021152N, which gives relatively high confidence
047959,000013: ## that the reconstruction is correct.
047960,000014: ## Reference: pp. 1131-1139
047961,000015: ## Assembler: yaYUL
047962,000016: ## Contact: Ron Burkey <info@sandroid.org>.
047963,000017: ## Website: www.ibiblio.org/apollo/index.html
047964,000018: ## Mod history: 2019-09-18 MAS Created from Luminary 178.
047965,000019:
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Page 1131
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047967,000021: # ..... RP-TO-R SUBROUTINE .....
047968,000022: # SUBROUTINE TO CONVERT RP (VECTOR IN PLANETARY COORDINATE SYSTEM,EITHER
047969,000023: # EARTH-FIXED OR MOON-FIXED) TO R (SAME VECTOR IN THE BASIC REF. SYSTEM)
047970,000024:
047971,000025: # R=MT(T)*(RP+LPXRP) MT = M MATRIX TRANSPOSE
047972,000026:
047973,000027: # CALLING SEQUENCE
047974,000028: # L CALL
047975,000029: # L+1 RP-TO-R
047976,000030:
047977,000031: # SUBROUTINES USED
047978,000032: # EARTHMX,MOONMX,EARTHL
047979,000033:
047980,000034: # ITEMS AVAILABLE FROM LAUNCH DATA
047981,000035: # 504LM= THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL,EXPRESSED
047982,000036: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
047983,000037: # ITEMS NECESSARY FOR SUBR. USED (SEE DESCRIPTION OF SUBR.)
047984,000038:
047985,000039: # INPUT
047986,000040: # MPAC= 0 FOR EARTH,NON-ZERO FOR MOON
047987,000041: # 0-5D= RP VECTOR
047988,000042: # 6-7D= TIME
047989,000043:
047990,000044: # OUTPUT
047991,000045: # MPAC= R VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
047992,000046:
047993,000047: 26,2000 SETLOC PLANTIN1
047994,000048: 26,2000 BANK
047995,000049:
047996,000050: 26,3720 COUNT* $$/LUROT
047997,000051:
047998,000052: 26,3720 46020 RP-TO-R STQ BHIZ
047999,000053: 26,3721 00050 RPREXIT
048000,000054: 26,3722 55735 RPTORA
048001,000055: 26,3723 77624 CALL # COMPUTE M MATRIX FOR MOON
048002,000056: 26,3724 51672 MOONMX # LP=LM FOR MOON RADIANS B0
048003,000057: 26,3725 77775 VLOAD
048004,000058: 26,3726 02013 504LM
048005,000059: 26,3727 53235 RPTORB VXV VAD
048006,000060: 26,3730 00001 504RPR
048007,000061: 26,3731 00001 504RPR
048008,000062: 26,3732 52105 VXM GOTO
048009,000063: 26,3733 00025 MMATRIX # MPAC=R=MT(T)*(RP+LPXRP)
048010,000064: 26,3734 51660 RPRPXXXX # RESET PUSHLOC TO 0 BEFORE EXITING
048011,000065: 26,3735 77624 RPTORA CALL # EARTH COMPUTATIONS
048012,000066: 26,3736 55745 EARTHMX # M MATRIX B-1
048013,000067: 26,3737 77624 CALL
048014,000068: 26,3740 15761 EARTHL # L VECTOR RADIANS B0
048015,000069: 26,3741 76521 MXV VSL1 # LP=M(T)*L RAD B-0
048016,000070: 26,3742 00025 MMATRIX
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Page 1132
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048018,000072: 26,3743 77650 GOTO
048019,000073: 26,3744 55727 RPTORB
048020,000074: 24,2000 SETLOC PLANTIN
048021,000075: 24,2000 BANK
048022,000076: 24,3642 COUNT* $$/LUROT
048023,000077:
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Page 1133
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048025,000079: # ..... R-TO-RP SUBROUTINE .....
048026,000080: # SUBROUTINE TO CONVERT R (VECTOR IN REFERENCE COORD. SYSTEM) TO RP
048027,000081: # (VECTOR IN PLANETARY COORD SYSTEM) EITHER EARTH-FIXED OR MOON-FIXED
048028,000082:
048029,000083: # RP=M(T)*(R-LXR)
048030,000084:
048031,000085: # CALLING SEQUENCE
048032,000086: # L CALL
048033,000087: # L+1 R-TO-RP
048034,000088:
048035,000089: # SUBROUTINES USED
048036,000090: # EARTHMX,MOONMX,EARTHL
048037,000091:
048038,000092: # INPUT
048039,000093: # MPAC= 0 FOR EARTH,NON-ZERO FOR MOON
048040,000094: # 0-5D= R VECTOR
048041,000095: # 6-7D= TIME
048042,000096:
048043,000097: # ITEMS AVAILABLE FROM LAUNCH DATA
048044,000098: # 504LM= THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL,EXPRESSED
048045,000099: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
048046,000100: # ITEMS NECESSARY FOR SUBROUTINES USED (SEE DESCRIPTION OF SUBR.)
048047,000101:
048048,000102: # OUTPUT
048049,000103: # MPAC=RP VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
048050,000104:
048051,000105: 24,3642 46020 R-TO-RP STQ BHIZ
048052,000106: 24,3643 00050 RPREXIT
048053,000107: 24,3644 51664 RTORPA
048054,000108: 24,3645 77624 CALL
048055,000109: 24,3646 51672 MOONMX
048056,000110: 24,3647 61375 VLOAD VXM
048057,000111: 24,3650 02013 504LM # LP=LM
048058,000112: 24,3651 00025 MMATRIX
048059,000113: 24,3652 77772 VSL1 # L=MT(T)*LP RADIANS B0
048060,000114: 24,3653 51235 RTORPB VXV BVSU
048061,000115: 24,3654 00001 504RPR
048062,000116: 24,3655 00001 504RPR
048063,000117: 24,3656 77721 MXV # M(T)*(R-LXR) B-2
048064,000118: 24,3657 00025 MMATRIX
048065,000119: 24,3660 40372 RPRPXXXX VSL1 SETPD
048066,000120: 24,3661 00001 0D
048067,000121: 24,3662 77650 GOTO
048068,000122: 24,3663 00050 RPREXIT
048069,000123: 24,3664 77624 RTORPA CALL # EARTH COMPUTATIONS
048070,000124: 24,3665 55745 EARTHMX
048071,000125: 24,3666 77624 CALL
048072,000126: 24,3667 15761 EARTHL
048073,000127: 24,3670 77650 GOTO # MPAC=L=(-AX,-AY,0) RAD B-0
048074,000128: 24,3671 51653 RTORPB
048075,000129:
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Page 1134
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048077,000131: # ..... MOONMX SUBROUTINE .....
048078,000132: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE MOON
048079,000133:
048080,000134: # CALLING SEQUENCE
048081,000135: # L CALL
048082,000136: # L+1 MOONMX
048083,000137:
048084,000138: # SUBROUTINES USED
048085,000139: # NEWANGLE
048086,000140:
048087,000141: # INPUT
048088,000142: # 6-7D= TIME
048089,000143: # ITEMS AVAILABLE FROM LAUNCH DATA
048090,000144: # BSUBO,BDOT
048091,000145: # TIMSUBO,NODIO,NODDOT,FSUBO,FDOT
048092,000146: # COSI= COS(I) B-1
048093,000147: # SINI= SIN(I) B-1
048094,000148: # I IS THE ANGLE BETWEEN THE MEAN LUNAR EQUATORIAL PLANE AND THE
048095,000149: # PLANE OF THE ECLIPTIC (1 DEGREE 32.1 MINUTES)
048096,000150:
048097,000151: # OUTPUT
048098,000152: # MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
048099,000153:
048100,000154: 24,3672 40220 MOONMX STQ SETPD
048101,000155: 24,3673 00051 EARTHMXX
048102,000156: 24,3674 00011 8D
048103,000157: 24,3675 77770 AXT,1 # B REQUIRES SL 0, SL 5 IN NEWANGLE
048104,000158: 24,3676 00005 5
048105,000159: 24,3677 65345 DLOAD PDDL # PD 10D 8-9D=BSUBO
048106,000160: 24,3700 14017 BSUBO # 10-11D= BDOT
048107,000161: 24,3701 14011 BDOT
048108,000162: 24,3702 45006 PUSH CALL # PD 12D
048109,000163: 24,3703 51741 NEWANGLE # EXIT WITH PD 8D AND MPAC= B REVS B0
048110,000164: 24,3704 71406 PUSH COS # PD 10D
048111,000165: 24,3705 14041 STODL COB # PD 8D COS(B) B-1
048112,000166: 24,3706 77756 SIN # SIN(B) B-1
048113,000167: 24,3707 14043 STODL SOB # SETUP INPUT FOR NEWANGLE
048114,000168: 24,3710 14015 FSUBO # 8-9D=FSUBO
048115,000169: 24,3711 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=FDOT
048116,000170: 24,3712 14007 FDOT
048117,000171: 24,3713 45170 AXT,1 CALL # F REQUIRES SL 1, SL 6 IN NEWANGLE
048118,000172: 24,3714 00004 4
048119,000173: 24,3715 51741 NEWANGLE # EXIT WITH PD 8D AND MPAC= F REVS B0
048120,000174: 24,3716 14027 STODL AVECTR +2 # SAVE F TEMP
048121,000175: 24,3717 14013 NODIO # 8-9D=NODIO
048122,000176: 24,3720 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=NODDOT
048123,000177: 24,3721 14005 NODDOT # MPAC=T
048124,000178: 24,3722 45170 AXT,1 CALL # NODE REQUIRES SL 0, SL 5 IN NEWANGLE
048125,000179: 24,3723 00005 5
048126,000180: 24,3724 51741 NEWANGLE # EXIT WITH PD 8D AND MPAC= NODI REVS B0
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Page 1135
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048128,000182: 24,3725 71406 PUSH COS # PD 10D 8-9D= NODI REVS B0
048129,000183: 24,3726 77606 PUSH # PD 12D 10-11D= COS(NODI) B-1
048130,000184: 24,3727 00025 STORE AVECTR
048131,000185: 24,3730 76405 DMP SL1R
048132,000186: 24,3731 00041 COB # COS(NODI) B-1
048133,000187: 24,3732 14035 STODL BVECTR +2 # PD 10D 20-25D=AVECTR= COB*SIN(NODI)
048134,000188: 24,3733 76405 DMP SL1R # SOB*SIN(NODI)
048135,000189: 24,3734 00043 SOB
048136,000190: 24,3735 14037 STODL BVECTR +4 # PD 8D
048137,000191: 24,3736 41556 SIN PUSH # PD 10D -SIN(NODI) B-1
048138,000192: 24,3737 52076 DCOMP GOTO # 26-31D=BVECTR= COV*COS(NODI)
048139,000193: 24,3740 53703 MOONMXA
048140,000194: 25,3703 BANK 25
048141,000195: 25,2000 SETLOC PLANTIN3
048142,000196: 25,2000 BANK
048143,000197: 25,3703 COUNT* $$/LUROT
048144,000198:
048145,000199: 25,3703 14033 MOONMXA STODL BVECTR # PD 8D SOB*COS(NODI)
048146,000200: 25,3704 00027 AVECTR +2 # MOVE F FROM TEMP LOC. TO 504F
048147,000201: 25,3705 14007 STODL 504F
048148,000202: 25,3706 76405 DMP SL1R
048149,000203: 25,3707 00041 COB
048150,000204: 25,3710 14027 STODL AVECTR +2
048151,000205: 25,3711 00011 SINNODI # 8-9D=SIN(NODI) B-1
048152,000206: 25,3712 76405 DMP SL1R
048153,000207: 25,3713 00043 SOB
048154,000208: 25,3714 14031 STODL AVECTR +4 # 0
048155,000209: 25,3715 06520 HI6ZEROS # 8-13D= CVECTR= -SOB B-1
048156,000210: 25,3716 57525 PDDL DCOMP # PD 10D COB
048157,000211: 25,3717 00043 SOB
048158,000212: 25,3720 63325 PDDL PDVL # PD 12D THEN PD 14D
048159,000213: 25,3721 00041 COB
048160,000214: 25,3722 00033 BVECTR
048161,000215: 25,3723 63361 VXSC PDVL # PD 20D BVECTR*SINI B-2
048162,000216: 25,3724 14003 SINI
048163,000217: 25,3725 00011 CVECTR
048164,000218: 25,3726 53361 VXSC VAD # PD 14D CVECTR*COSI B-2
048165,000219: 25,3727 14001 COSI
048166,000220: 25,3730 77772 VSL1
048167,000221: 25,3731 24041 STOVL MMATRIX +12D # PD 8D M2=BVECTR*SINI+CVECTR*COSI B-1
048168,000222: 25,3732 63361 VXSC PDVL # PD 14D
048169,000223: 25,3733 14003 SINI # CVECTR*SINI B-2
048170,000224: 25,3734 00033 BVECTR
048171,000225: 25,3735 52361 VXSC VSU # PD 8D BVECTR*COSI B-2
048172,000226: 25,3736 14001 COSI
048173,000227: 25,3737 65372 VSL1 PDDL # PD 14D
048174,000228: 25,3740 00007 504F # 8-13D=DVECTR=BVECTR*COSI-CVECTR*SINI B-1
048175,000229: 25,3741 74346 COS VXSC
048176,000230: 25,3742 00011 DVECTR
048177,000231: 25,3743 73525 PDDL SIN # PD 20D 14-19D= DVECTR*COSF B-2
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Page 1136
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048179,000233: 25,3744 00007 504F
048180,000234: 25,3745 52361 VXSC VSU # PD 14D AVECTR*SINF B-2
048181,000235: 25,3746 00025 AVECTR
048182,000236: 25,3747 77772 VSL1
048183,000237: 25,3750 14033 STODL MMATRIX +6 # M1= AVECTR*SINF-DVECTR*COSF B-1
048184,000238: 25,3751 00007 504F
048185,000239: 25,3752 74356 SIN VXSC # PD 8D
048186,000240: 25,3753 71525 PDDL COS # PD 14D 8-13D=DVECTR*SINF B-2
048187,000241: 25,3754 00007 504F
048188,000242: 25,3755 53361 VXSC VAD # PD 8D AVECTR*COSF B-2
048189,000243: 25,3756 00025 AVECTR
048190,000244: 25,3757 57572 VSL1 VCOMP
048191,000245: 25,3760 34025 STCALL MMATRIX # M0= -(AVECTR*COSF+DVECTR*SINF) B-1
048192,000246: 25,3761 00051 EARTHMXX
048193,000247: # COMPUTE X=X0+(XDOT)(T+T0)
048194,000248: # 8-9D= XO (REVS B-0),PUSHLOC SET AT 12D
048195,000249: # 10-11D=XDOT (REVS/CSEC) SCALED B+23 FOR WEARTH,B+28 FOR NODDOT AND BDOT
048196,000250: # AND B+27 FOR FDOT
048197,000251: # X1=DIFFERENCE IN 23 AND SCALING OF XDOT,=0 FOR WEARTH,5 FOR NODDOT AND
048198,000252: # BDOT AND 4 FOR FDOT
048199,000253: # 6-7D=T (CSEC B-28), TIMSUBO= (CSEC B-42 TRIPLE PREC.)
048200,000254:
048201,000255: 24,3741 BANK 24
048202,000256: 24,2000 SETLOC PLANTIN
048203,000257: 24,2000 BANK
048204,000258:
048205,000259: 24,3741 54345 NEWANGLE DLOAD SR # ENTER PD 12D
048206,000260: 24,3742 00007 6D
048207,000261: 24,3743 20617 14D
048208,000262: 24,3744 72371 TAD TLOAD # CHANGE MODE TO TP
048209,000263: 24,3745 01707 TIMSUBO
048210,000264: 24,3746 00155 MPAC
048211,000265: 24,3747 14017 STODL TIMSUBM # T+T0 CSEC B-42
048212,000266: 24,3750 00020 TIMSUBM +1
048213,000267: 24,3751 77605 DMP # PD 10D MULT BY XDOT IN 10-11D
048214,000268: 24,3752 43257 SL* DAD # PD 8D ADD XO IN 8-9D AFTER SHIFTING
048215,000269: 24,3753 20206 5,1 # SUCH THAT SCALING IS B-0
048216,000270: 24,3754 67206 PUSH SLOAD # PD 10D SAVE PARTIAL (X0+XDOT*T) IN 8-9D
048217,000271: 24,3755 00017 TIMSUBM
048218,000272: 24,3756 41261 SL DMP
048219,000273: 24,3757 20212 9D
048220,000274: 24,3760 00013 10D # XDOT
048221,000275: 24,3761 43257 SL* DAD # PD 8D SHIFT SUCH THAT THIS PART OF X
048222,000276: 24,3762 20213 10D,1 # IS SCALED REVS/CSEC B-0
048223,000277: 24,3763 77600 BOV # TURN OFF OVERFLOW IF SET BY SHIFT
048224,000278: 24,3764 51765 +1 # INSTRUCTION BEFORE EXITING
048225,000279: 24,3765 77616 RVQ # MPAC=X= X0+(XDOT)(T+T0) REVS B0
048226,000280:
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Page 1137
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048228,000282: # ..... EARTHMX SUBROUTINE .....
048229,000283: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE EARTH
048230,000284:
048231,000285: # CALLING SEQUENCE
048232,000286: # L CALL
048233,000287: # L+1 EARTHMX
048234,000288:
048235,000289: # SUBROUTINES USED
048236,000290: # NEWANGLE
048237,000291:
048238,000292: # INPUT
048239,000293: # INPUT AVAILABLE FROM LAUNCH DATA AZO REVS B-0
048240,000294: # TEPHEM CSEC B-42
048241,000295: # 6-7D= TIME CSEC B-28
048242,000296:
048243,000297: # OUTPUT
048244,000298: # MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
048245,000299:
048246,000300: 26,3745 BANK 26
048247,000301: 26,2000 SETLOC PLANTIN1
048248,000302: 26,2000 BANK
048249,000303: 26,3745 COUNT* $$/LUROT
048250,000304:
048251,000305: 26,3745 40220 EARTHMX STQ SETPD # SET 8-9D=AZO
048252,000306: 26,3746 00051 EARTHMXX
048253,000307: 26,3747 00011 8D # 10-11D=WEARTH
048254,000308: 26,3750 77770 AXT,1 # FOR SL 5, AND SL 10 IN NEWANGLE
048255,000309: 26,3751 00000 0
048256,000310: 26,3752 65345 DLOAD PDDL # LEAVING PD SET AT 12D FOR NEWANGLE
048257,000311: 26,3753 14023 AZO
048258,000312: 26,3754 14021 WEARTH
048259,000313: 26,3755 45006 PUSH CALL
048260,000314: 26,3756 51741 NEWANGLE
048261,000315: 26,3757 41401 SETPD PUSH # 18-19D=504AZ
048262,000316: 26,3760 00023 18D # COS(AZ) SIN(AZ) 0
048263,000317: 26,3761 65346 COS PDDL # 20-37D= MMATRIX= -SIN(AZ) COS(AZ) 0 B-1
048264,000318: 26,3762 00023 504AZ # 0 0 1
048265,000319: 26,3763 65356 SIN PDDL
048266,000320: 26,3764 06520 HI6ZEROS
048267,000321: 26,3765 73525 PDDL SIN
048268,000322: 26,3766 00023 504AZ
048269,000323: 26,3767 65276 DCOMP PDDL
048270,000324: 26,3770 00023 504AZ
048271,000325: 26,3771 63346 COS PDVL
048272,000326: 26,3772 06520 HI6ZEROS
048273,000327: 26,3773 41525 PDDL PUSH
048274,000328: 26,3774 06516 HIDPHALF
048275,000329: 26,3775 77650 GOTO
048276,000330: 26,3776 00051 EARTHMXX
048277,000331:
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Page 1138
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048279,000333: # ..... EARTHL SUBROUTINE .....
048280,000334: # SUBROUTINE TO COMPUTE L VECTOR FOR EARTH
048281,000335:
048282,000336: # CALLING SEQUENCE
048283,000337: # L CALL
048284,000338: # L+1 EARTHL
048285,000339:
048286,000340: # INPUT
048287,000341: # AXO,AYO SET AT LAUNCH TIME WITH AYO IMMEDIATELY FOLLOWING AXO IN CORE
048288,000342:
048289,000343: # OUTPUT
048290,000344: # -AX
048291,000345: # MPAC= -AY RADIANS B-0
048292,000346: # 0
048293,000347:
048294,000348: 06,3761 BANK 06
048295,000349: 06,2000 SETLOC EARTHLOC
048296,000350: 06,2000 BANK
048297,000351: 06,3761 COUNT* $$/LUROT
048298,000352:
048299,000353: 06,3761 57545 EARTHL DLOAD DCOMP
048300,000354: 06,3762 01714 AXO
048301,000355: 06,3763 14017 STODL 504LPL
048302,000356: 06,3764 01712 -AYO
048303,000357: 06,3765 14021 STODL 504LPL +2
048304,000358: 06,3766 24007 LO6ZEROS
048305,000359: 06,3767 24023 STOVL 504LPL +4
048306,000360: 06,3770 00017 504LPL
048307,000361: 06,3771 77616 RVQ
048308,000362:
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Page 1139
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048310,000364: # CONSTANTS AND ERASABLE ASSIGNMENTS
048311,000365: 06,3772 12,2004 1B1 = DP1/2 # 1 SCALED B-1
048312,000366: 06,3772 0000050 RPREXIT = S1 # R-TO-RP AND RP-TO-R SUBR EXIT
048313,000367: 06,3772 0000051 EARTHMXX = S2 # EARTHMX,MOONMX SUBR. EXITS
048314,000368: 06,3772 504RPR = 0D # 6 REGS R OR RP VECTOR
048315,000369: 06,3772 SINNODI = 8D # 2 SIN(NODI)
048316,000370: 06,3772 DVECTR = 8D # 6 D VECTOR MOON
048317,000371: 06,3772 CVECTR = 8D # 6 C VECTR MOON
048318,000372: 06,3772 504AZ = 18D # 2 AZ
048319,000373: 06,3772 TIMSUBM = 14D # 3 TIME SUB M (MOON) T+T0 IN GETAZ
048320,000374: 06,3772 504LPL = 14D # 6 L OR LP VECTOR
048321,000375: 06,3772 AVECTR = 20D # 6 A VECTOR (MOON)
048322,000376: 06,3772 BVECTR = 26D # 6 B VECTOR (MOON)
048323,000377: 06,3772 MMATRIX = 20D # 18 M MATRIX
048324,000378: 06,3772 COB = 32D # 2 COS(B) B-1
048325,000379: 06,3772 SOB = 34D # 2 SIN(B) B-1
048326,000380: 06,3772 504F = 6D # 2 F(MOON)
End of include-file PLANETARY_INERTIAL_ORIENTATION.agc. Parent file is MAIN.agc