Source Code
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These source-code files are part of a reconstructed copy of Luminary 178, the
final release of the Apollo 14 Lunar Module (LM) Apollo Guidance Computer
(AGC) software.
The reconstruction began with source code of Zerlina 56, Luminary 210, and
Luminary 131, previously transcribed from digitized copies of those programs.
The code was created by combining the three, using Zerlina 56 as a base, since
it was based off of Luminary 183. The differences between the three were
carefully merged using the Luminary memos as a guide, with all changes made
after Luminary 178 being backed out. 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 178 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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048029,000002: ## Copyright: Public domain.
048030,000003: ## Filename: PLANETARY_INERTIAL_ORIENTATION.agc
048031,000004: ## Purpose: A section of Luminary revision 178.
048032,000005: ## It is part of the reconstructed source code for the final
048033,000006: ## release of the flight software for the Lunar Module's
048034,000007: ## (LM) Apollo Guidance Computer (AGC) for Apollo 14. The
048035,000008: ## code has been recreated from copies of Zerlina 56, Luminary
048036,000009: ## 210, and Luminary 131, as well as many Luminary memos.
048037,000010: ## It has been adapted such that the resulting bugger words
048038,000011: ## exactly match those specified for Luminary 178 in NASA
048039,000012: ## drawing 2021152N, which gives relatively high confidence
048040,000013: ## that the reconstruction is correct.
048041,000014: ## Reference: pp. 1131-1139
048042,000015: ## Assembler: yaYUL
048043,000016: ## Contact: Ron Burkey <info@sandroid.org>.
048044,000017: ## Website: www.ibiblio.org/apollo/index.html
048045,000018: ## Mod history: 2019-08-14 MAS Created from Zerlina 56.
048046,000019:
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Page 1131
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048048,000021: # ..... RP-TO-R SUBROUTINE .....
048049,000022: # SUBROUTINE TO CONVERT RP (VECTOR IN PLANETARY COORDINATE SYSTEM,EITHER
048050,000023: # EARTH-FIXED OR MOON-FIXED) TO R (SAME VECTOR IN THE BASIC REF. SYSTEM)
048051,000024:
048052,000025: # R=MT(T)*(RP+LPXRP) MT = M MATRIX TRANSPOSE
048053,000026:
048054,000027: # CALLING SEQUENCE
048055,000028: # L CALL
048056,000029: # L+1 RP-TO-R
048057,000030:
048058,000031: # SUBROUTINES USED
048059,000032: # EARTHMX,MOONMX,EARTHL
048060,000033:
048061,000034: # ITEMS AVAILABLE FROM LAUNCH DATA
048062,000035: # 504LM= THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL,EXPRESSED
048063,000036: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
048064,000037: # ITEMS NECESSARY FOR SUBR. USED (SEE DESCRIPTION OF SUBR.)
048065,000038:
048066,000039: # INPUT
048067,000040: # MPAC= 0 FOR EARTH,NON-ZERO FOR MOON
048068,000041: # 0-5D= RP VECTOR
048069,000042: # 6-7D= TIME
048070,000043:
048071,000044: # OUTPUT
048072,000045: # MPAC= R VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
048073,000046:
048074,000047: 26,2000 SETLOC PLANTIN1
048075,000048: 26,2000 BANK
048076,000049:
048077,000050: 26,3720 COUNT* $$/LUROT
048078,000051:
048079,000052: 26,3720 46020 RP-TO-R STQ BHIZ
048080,000053: 26,3721 00050 RPREXIT
048081,000054: 26,3722 55735 RPTORA
048082,000055: 26,3723 77624 CALL # COMPUTE M MATRIX FOR MOON
048083,000056: 26,3724 51672 MOONMX # LP=LM FOR MOON RADIANS B0
048084,000057: 26,3725 77775 VLOAD
048085,000058: 26,3726 02013 504LM
048086,000059: 26,3727 53235 RPTORB VXV VAD
048087,000060: 26,3730 00001 504RPR
048088,000061: 26,3731 00001 504RPR
048089,000062: 26,3732 52105 VXM GOTO
048090,000063: 26,3733 00025 MMATRIX # MPAC=R=MT(T)*(RP+LPXRP)
048091,000064: 26,3734 51660 RPRPXXXX # RESET PUSHLOC TO 0 BEFORE EXITING
048092,000065: 26,3735 77624 RPTORA CALL # EARTH COMPUTATIONS
048093,000066: 26,3736 55745 EARTHMX # M MATRIX B-1
048094,000067: 26,3737 77624 CALL
048095,000068: 26,3740 15761 EARTHL # L VECTOR RADIANS B0
048096,000069: 26,3741 76521 MXV VSL1 # LP=M(T)*L RAD B-0
048097,000070: 26,3742 00025 MMATRIX
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Page 1132
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048099,000072: 26,3743 77650 GOTO
048100,000073: 26,3744 55727 RPTORB
048101,000074: 24,2000 SETLOC PLANTIN
048102,000075: 24,2000 BANK
048103,000076: 24,3642 COUNT* $$/LUROT
048104,000077:
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Page 1133
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048106,000079: # ..... R-TO-RP SUBROUTINE .....
048107,000080: # SUBROUTINE TO CONVERT R (VECTOR IN REFERENCE COORD. SYSTEM) TO RP
048108,000081: # (VECTOR IN PLANETARY COORD SYSTEM) EITHER EARTH-FIXED OR MOON-FIXED
048109,000082:
048110,000083: # RP=M(T)*(R-LXR)
048111,000084:
048112,000085: # CALLING SEQUENCE
048113,000086: # L CALL
048114,000087: # L+1 R-TO-RP
048115,000088:
048116,000089: # SUBROUTINES USED
048117,000090: # EARTHMX,MOONMX,EARTHL
048118,000091:
048119,000092: # INPUT
048120,000093: # MPAC= 0 FOR EARTH,NON-ZERO FOR MOON
048121,000094: # 0-5D= R VECTOR
048122,000095: # 6-7D= TIME
048123,000096:
048124,000097: # ITEMS AVAILABLE FROM LAUNCH DATA
048125,000098: # 504LM= THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL,EXPRESSED
048126,000099: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
048127,000100: # ITEMS NECESSARY FOR SUBROUTINES USED (SEE DESCRIPTION OF SUBR.)
048128,000101:
048129,000102: # OUTPUT
048130,000103: # MPAC=RP VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
048131,000104:
048132,000105: 24,3642 46020 R-TO-RP STQ BHIZ
048133,000106: 24,3643 00050 RPREXIT
048134,000107: 24,3644 51664 RTORPA
048135,000108: 24,3645 77624 CALL
048136,000109: 24,3646 51672 MOONMX
048137,000110: 24,3647 61375 VLOAD VXM
048138,000111: 24,3650 02013 504LM # LP=LM
048139,000112: 24,3651 00025 MMATRIX
048140,000113: 24,3652 77772 VSL1 # L=MT(T)*LP RADIANS B0
048141,000114: 24,3653 51235 RTORPB VXV BVSU
048142,000115: 24,3654 00001 504RPR
048143,000116: 24,3655 00001 504RPR
048144,000117: 24,3656 77721 MXV # M(T)*(R-LXR) B-2
048145,000118: 24,3657 00025 MMATRIX
048146,000119: 24,3660 40372 RPRPXXXX VSL1 SETPD
048147,000120: 24,3661 00001 0D
048148,000121: 24,3662 77650 GOTO
048149,000122: 24,3663 00050 RPREXIT
048150,000123: 24,3664 77624 RTORPA CALL # EARTH COMPUTATIONS
048151,000124: 24,3665 55745 EARTHMX
048152,000125: 24,3666 77624 CALL
048153,000126: 24,3667 15761 EARTHL
048154,000127: 24,3670 77650 GOTO # MPAC=L=(-AX,-AY,0) RAD B-0
048155,000128: 24,3671 51653 RTORPB
048156,000129:
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Page 1134
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048158,000131: # ..... MOONMX SUBROUTINE .....
048159,000132: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE MOON
048160,000133:
048161,000134: # CALLING SEQUENCE
048162,000135: # L CALL
048163,000136: # L+1 MOONMX
048164,000137:
048165,000138: # SUBROUTINES USED
048166,000139: # NEWANGLE
048167,000140:
048168,000141: # INPUT
048169,000142: # 6-7D= TIME
048170,000143: # ITEMS AVAILABLE FROM LAUNCH DATA
048171,000144: # BSUBO,BDOT
048172,000145: # TIMSUBO,NODIO,NODDOT,FSUBO,FDOT
048173,000146: # COSI= COS(I) B-1
048174,000147: # SINI= SIN(I) B-1
048175,000148: # I IS THE ANGLE BETWEEN THE MEAN LUNAR EQUATORIAL PLANE AND THE
048176,000149: # PLANE OF THE ECLIPTIC (1 DEGREE 32.1 MINUTES)
048177,000150:
048178,000151: # OUTPUT
048179,000152: # MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
048180,000153:
048181,000154: 24,3672 40220 MOONMX STQ SETPD
048182,000155: 24,3673 00051 EARTHMXX
048183,000156: 24,3674 00011 8D
048184,000157: 24,3675 77770 AXT,1 # B REQUIRES SL 0, SL 5 IN NEWANGLE
048185,000158: 24,3676 00005 5
048186,000159: 24,3677 65345 DLOAD PDDL # PD 10D 8-9D=BSUBO
048187,000160: 24,3700 14017 BSUBO # 10-11D= BDOT
048188,000161: 24,3701 14011 BDOT
048189,000162: 24,3702 45006 PUSH CALL # PD 12D
048190,000163: 24,3703 51741 NEWANGLE # EXIT WITH PD 8D AND MPAC= B REVS B0
048191,000164: 24,3704 71406 PUSH COS # PD 10D
048192,000165: 24,3705 14041 STODL COB # PD 8D COS(B) B-1
048193,000166: 24,3706 77756 SIN # SIN(B) B-1
048194,000167: 24,3707 14043 STODL SOB # SETUP INPUT FOR NEWANGLE
048195,000168: 24,3710 14015 FSUBO # 8-9D=FSUBO
048196,000169: 24,3711 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=FDOT
048197,000170: 24,3712 14007 FDOT
048198,000171: 24,3713 45170 AXT,1 CALL # F REQUIRES SL 1, SL 6 IN NEWANGLE
048199,000172: 24,3714 00004 4
048200,000173: 24,3715 51741 NEWANGLE # EXIT WITH PD 8D AND MPAC= F REVS B0
048201,000174: 24,3716 14027 STODL AVECTR +2 # SAVE F TEMP
048202,000175: 24,3717 14013 NODIO # 8-9D=NODIO
048203,000176: 24,3720 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=NODDOT
048204,000177: 24,3721 14005 NODDOT # MPAC=T
048205,000178: 24,3722 45170 AXT,1 CALL # NODE REQUIRES SL 0, SL 5 IN NEWANGLE
048206,000179: 24,3723 00005 5
048207,000180: 24,3724 51741 NEWANGLE # EXIT WITH PD 8D AND MPAC= NODI REVS B0
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Page 1135
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048209,000182: 24,3725 71406 PUSH COS # PD 10D 8-9D= NODI REVS B0
048210,000183: 24,3726 77606 PUSH # PD 12D 10-11D= COS(NODI) B-1
048211,000184: 24,3727 00025 STORE AVECTR
048212,000185: 24,3730 76405 DMP SL1R
048213,000186: 24,3731 00041 COB # COS(NODI) B-1
048214,000187: 24,3732 14035 STODL BVECTR +2 # PD 10D 20-25D=AVECTR= COB*SIN(NODI)
048215,000188: 24,3733 76405 DMP SL1R # SOB*SIN(NODI)
048216,000189: 24,3734 00043 SOB
048217,000190: 24,3735 14037 STODL BVECTR +4 # PD 8D
048218,000191: 24,3736 41556 SIN PUSH # PD 10D -SIN(NODI) B-1
048219,000192: 24,3737 52076 DCOMP GOTO # 26-31D=BVECTR= COV*COS(NODI)
048220,000193: 24,3740 53703 MOONMXA
048221,000194: 25,3703 BANK 25
048222,000195: 25,2000 SETLOC PLANTIN3
048223,000196: 25,2000 BANK
048224,000197: 25,3703 COUNT* $$/LUROT
048225,000198:
048226,000199: 25,3703 14033 MOONMXA STODL BVECTR # PD 8D SOB*COS(NODI)
048227,000200: 25,3704 00027 AVECTR +2 # MOVE F FROM TEMP LOC. TO 504F
048228,000201: 25,3705 14007 STODL 504F
048229,000202: 25,3706 76405 DMP SL1R
048230,000203: 25,3707 00041 COB
048231,000204: 25,3710 14027 STODL AVECTR +2
048232,000205: 25,3711 00011 SINNODI # 8-9D=SIN(NODI) B-1
048233,000206: 25,3712 76405 DMP SL1R
048234,000207: 25,3713 00043 SOB
048235,000208: 25,3714 14031 STODL AVECTR +4 # 0
048236,000209: 25,3715 06470 HI6ZEROS # 8-13D= CVECTR= -SOB B-1
048237,000210: 25,3716 57525 PDDL DCOMP # PD 10D COB
048238,000211: 25,3717 00043 SOB
048239,000212: 25,3720 63325 PDDL PDVL # PD 12D THEN PD 14D
048240,000213: 25,3721 00041 COB
048241,000214: 25,3722 00033 BVECTR
048242,000215: 25,3723 63361 VXSC PDVL # PD 20D BVECTR*SINI B-2
048243,000216: 25,3724 14003 SINI
048244,000217: 25,3725 00011 CVECTR
048245,000218: 25,3726 53361 VXSC VAD # PD 14D CVECTR*COSI B-2
048246,000219: 25,3727 14001 COSI
048247,000220: 25,3730 77772 VSL1
048248,000221: 25,3731 24041 STOVL MMATRIX +12D # PD 8D M2=BVECTR*SINI+CVECTR*COSI B-1
048249,000222: 25,3732 63361 VXSC PDVL # PD 14D
048250,000223: 25,3733 14003 SINI # CVECTR*SINI B-2
048251,000224: 25,3734 00033 BVECTR
048252,000225: 25,3735 52361 VXSC VSU # PD 8D BVECTR*COSI B-2
048253,000226: 25,3736 14001 COSI
048254,000227: 25,3737 65372 VSL1 PDDL # PD 14D
048255,000228: 25,3740 00007 504F # 8-13D=DVECTR=BVECTR*COSI-CVECTR*SINI B-1
048256,000229: 25,3741 74346 COS VXSC
048257,000230: 25,3742 00011 DVECTR
048258,000231: 25,3743 73525 PDDL SIN # PD 20D 14-19D= DVECTR*COSF B-2
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Page 1136
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048260,000233: 25,3744 00007 504F
048261,000234: 25,3745 52361 VXSC VSU # PD 14D AVECTR*SINF B-2
048262,000235: 25,3746 00025 AVECTR
048263,000236: 25,3747 77772 VSL1
048264,000237: 25,3750 14033 STODL MMATRIX +6 # M1= AVECTR*SINF-DVECTR*COSF B-1
048265,000238: 25,3751 00007 504F
048266,000239: 25,3752 74356 SIN VXSC # PD 8D
048267,000240: 25,3753 71525 PDDL COS # PD 14D 8-13D=DVECTR*SINF B-2
048268,000241: 25,3754 00007 504F
048269,000242: 25,3755 53361 VXSC VAD # PD 8D AVECTR*COSF B-2
048270,000243: 25,3756 00025 AVECTR
048271,000244: 25,3757 57572 VSL1 VCOMP
048272,000245: 25,3760 34025 STCALL MMATRIX # M0= -(AVECTR*COSF+DVECTR*SINF) B-1
048273,000246: 25,3761 00051 EARTHMXX
048274,000247: # COMPUTE X=X0+(XDOT)(T+T0)
048275,000248: # 8-9D= XO (REVS B-0),PUSHLOC SET AT 12D
048276,000249: # 10-11D=XDOT (REVS/CSEC) SCALED B+23 FOR WEARTH,B+28 FOR NODDOT AND BDOT
048277,000250: # AND B+27 FOR FDOT
048278,000251: # X1=DIFFERENCE IN 23 AND SCALING OF XDOT,=0 FOR WEARTH,5 FOR NODDOT AND
048279,000252: # BDOT AND 4 FOR FDOT
048280,000253: # 6-7D=T (CSEC B-28), TIMSUBO= (CSEC B-42 TRIPLE PREC.)
048281,000254:
048282,000255: 24,3741 BANK 24
048283,000256: 24,2000 SETLOC PLANTIN
048284,000257: 24,2000 BANK
048285,000258:
048286,000259: 24,3741 54345 NEWANGLE DLOAD SR # ENTER PD 12D
048287,000260: 24,3742 00007 6D
048288,000261: 24,3743 20617 14D
048289,000262: 24,3744 72371 TAD TLOAD # CHANGE MODE TO TP
048290,000263: 24,3745 01707 TIMSUBO
048291,000264: 24,3746 00155 MPAC
048292,000265: 24,3747 14017 STODL TIMSUBM # T+T0 CSEC B-42
048293,000266: 24,3750 00020 TIMSUBM +1
048294,000267: 24,3751 77605 DMP # PD 10D MULT BY XDOT IN 10-11D
048295,000268: 24,3752 43257 SL* DAD # PD 8D ADD XO IN 8-9D AFTER SHIFTING
048296,000269: 24,3753 20206 5,1 # SUCH THAT SCALING IS B-0
048297,000270: 24,3754 67206 PUSH SLOAD # PD 10D SAVE PARTIAL (X0+XDOT*T) IN 8-9D
048298,000271: 24,3755 00017 TIMSUBM
048299,000272: 24,3756 41261 SL DMP
048300,000273: 24,3757 20212 9D
048301,000274: 24,3760 00013 10D # XDOT
048302,000275: 24,3761 43257 SL* DAD # PD 8D SHIFT SUCH THAT THIS PART OF X
048303,000276: 24,3762 20213 10D,1 # IS SCALED REVS/CSEC B-0
048304,000277: 24,3763 77600 BOV # TURN OFF OVERFLOW IF SET BY SHIFT
048305,000278: 24,3764 51765 +1 # INSTRUCTION BEFORE EXITING
048306,000279: 24,3765 77616 RVQ # MPAC=X= X0+(XDOT)(T+T0) REVS B0
048307,000280:
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Page 1137
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048309,000282: # ..... EARTHMX SUBROUTINE .....
048310,000283: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE EARTH
048311,000284:
048312,000285: # CALLING SEQUENCE
048313,000286: # L CALL
048314,000287: # L+1 EARTHMX
048315,000288:
048316,000289: # SUBROUTINES USED
048317,000290: # NEWANGLE
048318,000291:
048319,000292: # INPUT
048320,000293: # INPUT AVAILABLE FROM LAUNCH DATA AZO REVS B-0
048321,000294: # TEPHEM CSEC B-42
048322,000295: # 6-7D= TIME CSEC B-28
048323,000296:
048324,000297: # OUTPUT
048325,000298: # MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
048326,000299:
048327,000300: 26,3745 BANK 26
048328,000301: 26,2000 SETLOC PLANTIN1
048329,000302: 26,2000 BANK
048330,000303: 26,3745 COUNT* $$/LUROT
048331,000304:
048332,000305: 26,3745 40220 EARTHMX STQ SETPD # SET 8-9D=AZO
048333,000306: 26,3746 00051 EARTHMXX
048334,000307: 26,3747 00011 8D # 10-11D=WEARTH
048335,000308: 26,3750 77770 AXT,1 # FOR SL 5, AND SL 10 IN NEWANGLE
048336,000309: 26,3751 00000 0
048337,000310: 26,3752 65345 DLOAD PDDL # LEAVING PD SET AT 12D FOR NEWANGLE
048338,000311: 26,3753 14023 AZO
048339,000312: 26,3754 14021 WEARTH
048340,000313: 26,3755 45006 PUSH CALL
048341,000314: 26,3756 51741 NEWANGLE
048342,000315: 26,3757 41401 SETPD PUSH # 18-19D=504AZ
048343,000316: 26,3760 00023 18D # COS(AZ) SIN(AZ) 0
048344,000317: 26,3761 65346 COS PDDL # 20-37D= MMATRIX= -SIN(AZ) COS(AZ) 0 B-1
048345,000318: 26,3762 00023 504AZ # 0 0 1
048346,000319: 26,3763 65356 SIN PDDL
048347,000320: 26,3764 06470 HI6ZEROS
048348,000321: 26,3765 73525 PDDL SIN
048349,000322: 26,3766 00023 504AZ
048350,000323: 26,3767 65276 DCOMP PDDL
048351,000324: 26,3770 00023 504AZ
048352,000325: 26,3771 63346 COS PDVL
048353,000326: 26,3772 06470 HI6ZEROS
048354,000327: 26,3773 41525 PDDL PUSH
048355,000328: 26,3774 06466 HIDPHALF
048356,000329: 26,3775 77650 GOTO
048357,000330: 26,3776 00051 EARTHMXX
048358,000331:
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Page 1138
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048360,000333: # ..... EARTHL SUBROUTINE .....
048361,000334: # SUBROUTINE TO COMPUTE L VECTOR FOR EARTH
048362,000335:
048363,000336: # CALLING SEQUENCE
048364,000337: # L CALL
048365,000338: # L+1 EARTHL
048366,000339:
048367,000340: # INPUT
048368,000341: # AXO,AYO SET AT LAUNCH TIME WITH AYO IMMEDIATELY FOLLOWING AXO IN CORE
048369,000342:
048370,000343: # OUTPUT
048371,000344: # -AX
048372,000345: # MPAC= -AY RADIANS B-0
048373,000346: # 0
048374,000347:
048375,000348: 06,3761 BANK 06
048376,000349: 06,2000 SETLOC EARTHLOC
048377,000350: 06,2000 BANK
048378,000351: 06,3761 COUNT* $$/LUROT
048379,000352:
048380,000353: 06,3761 57545 EARTHL DLOAD DCOMP
048381,000354: 06,3762 01714 AXO
048382,000355: 06,3763 14017 STODL 504LPL
048383,000356: 06,3764 01712 -AYO
048384,000357: 06,3765 14021 STODL 504LPL +2
048385,000358: 06,3766 24007 LO6ZEROS
048386,000359: 06,3767 24023 STOVL 504LPL +4
048387,000360: 06,3770 00017 504LPL
048388,000361: 06,3771 77616 RVQ
048389,000362:
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Page 1139
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048391,000364: # CONSTANTS AND ERASABLE ASSIGNMENTS
048392,000365: 06,3772 12,2004 1B1 = DP1/2 # 1 SCALED B-1
048393,000366: 06,3772 0000050 RPREXIT = S1 # R-TO-RP AND RP-TO-R SUBR EXIT
048394,000367: 06,3772 0000051 EARTHMXX = S2 # EARTHMX,MOONMX SUBR. EXITS
048395,000368: 06,3772 504RPR = 0D # 6 REGS R OR RP VECTOR
048396,000369: 06,3772 SINNODI = 8D # 2 SIN(NODI)
048397,000370: 06,3772 DVECTR = 8D # 6 D VECTOR MOON
048398,000371: 06,3772 CVECTR = 8D # 6 C VECTR MOON
048399,000372: 06,3772 504AZ = 18D # 2 AZ
048400,000373: 06,3772 TIMSUBM = 14D # 3 TIME SUB M (MOON) T+T0 IN GETAZ
048401,000374: 06,3772 504LPL = 14D # 6 L OR LP VECTOR
048402,000375: 06,3772 AVECTR = 20D # 6 A VECTOR (MOON)
048403,000376: 06,3772 BVECTR = 26D # 6 B VECTOR (MOON)
048404,000377: 06,3772 MMATRIX = 20D # 18 M MATRIX
048405,000378: 06,3772 COB = 32D # 2 COS(B) B-1
048406,000379: 06,3772 SOB = 34D # 2 SIN(B) B-1
048407,000380: 06,3772 504F = 6D # 2 F(MOON)
End of include-file PLANETARY_INERTIAL_ORIENTATION.agc. Parent file is MAIN.agc