Source Code
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These source-code files were transcribed from a printout in Don Eyles's personal
collection, scanned by archive.org, and financially sponsored by Linden Sims.
A team of volunteers performed the transcription and proof-reading. The scanned
page images are available at
the Virtual AGC Project website, as well as higher-quality (but much larger)
images at
the Virtual AGC Project's collection in the Internet Archive. Report any problems by creating
"issues" at
the Virtual AGC Project's GitHub Repository. Notations on the program listing read, in part: GAP: ASSEMBLE REVISION 56 OF AGC PROGRAM ZERLINA BY ZOROASTER 9:12 OCT. 21,1970Note that the date is the date of the printout, not the date of the program revision. |
049261,000002: ## Copyright: Public domain.
049262,000003: ## Filename: PLANETARY_INERTIAL_ORIENTATION.agc
049263,000004: ## Purpose: A log section of Zerlina 56, the final revision of
049264,000005: ## Don Eyles's offline development program for the variable
049265,000006: ## guidance period servicer. It also includes a new P66 with LPD
049266,000007: ## (Landing Point Designator) capability, based on an idea of John
049267,000008: ## Young's. Neither of these advanced features were actually flown,
049268,000009: ## but Zerlina was also the birthplace of other big improvements to
049269,000010: ## Luminary including the terrain model and new (Luminary 1E)
049270,000011: ## analog display programs. Zerlina was branched off of Luminary 145,
049271,000012: ## and revision 56 includes all changes up to and including Luminary
049272,000013: ## 183. It is therefore quite close to the Apollo 14 program,
049273,000014: ## Luminary 178, where not modified with new features.
049274,000015: ## Reference: pp. 1131-1139
049275,000016: ## Assembler: yaYUL
049276,000017: ## Contact: Ron Burkey <info@sandroid.org>.
049277,000018: ## Website: www.ibiblio.org/apollo/index.html
049278,000019: ## Mod history: 2017-07-28 MAS Created from Luminary 210.
049279,000020: ## 2017-08-28 MAS Updated for Zerlina 56.
049280,000021:
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Page 1131 |
049282,000023: # ..... RP-TO-R SUBROUTINE .....
049283,000024: # SUBROUTINE TO CONVERT RP (VECTOR IN PLANETARY COORDINATE SYSTEM,EITHER
049284,000025: # EARTH-FIXED OR MOON-FIXED) TO R (SAME VECTOR IN THE BASIC REF. SYSTEM)
049285,000026:
049286,000027: # R=MT(T)*(RP+LPXRP) MT = M MATRIX TRANSPOSE
049287,000028:
049288,000029: # CALLING SEQUENCE
049289,000030: # L CALL
049290,000031: # L+1 RP-TO-R
049291,000032:
049292,000033: # SUBROUTINES USED
049293,000034: # EARTHMX,MOONMX,EARTHL
049294,000035:
049295,000036: # ITEMS AVAILABLE FROM LAUNCH DATA
049296,000037: # 504LM= THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL,EXPRESSED
049297,000038: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
049298,000039: # ITEMS NECESSARY FOR SUBR. USED (SEE DESCRIPTION OF SUBR.)
049299,000040:
049300,000041: # INPUT
049301,000042: # MPAC= 0 FOR EARTH,NON-ZERO FOR MOON
049302,000043: # 0-5D= RP VECTOR
049303,000044: # 6-7D= TIME
049304,000045:
049305,000046: # OUTPUT
049306,000047: # MPAC= R VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
049307,000048:
049308,000049: 26,2000 SETLOC PLANTIN1
049309,000050: 26,2000 BANK
049310,000051:
049311,000052: 26,3720 COUNT* $$/LUROT
049312,000053:
049313,000054: 26,3720 46020 RP-TO-R STQ BHIZ
049314,000055: 26,3721 00050 RPREXIT
049315,000056: 26,3722 55735 RPTORA
049316,000057: 26,3723 77624 CALL # COMPUTE M MATRIX FOR MOON
049317,000058: 26,3724 51674 MOONMX # LP=LM FOR MOON RADIANS B0
049318,000059: 26,3725 77775 VLOAD
049319,000060: 26,3726 02013 504LM
049320,000061: 26,3727 53235 RPTORB VXV VAD
049321,000062: 26,3730 00001 504RPR
049322,000063: 26,3731 00001 504RPR
049323,000064: 26,3732 52105 VXM GOTO
049324,000065: 26,3733 00025 MMATRIX # MPAC=R=MT(T)*(RP+LPXRP)
049325,000066: 26,3734 51662 RPRPXXXX # RESET PUSHLOC TO 0 BEFORE EXITING
049326,000067: 26,3735 77624 RPTORA CALL # EARTH COMPUTATIONS
049327,000068: 26,3736 55745 EARTHMX # M MATRIX B-1
049328,000069: 26,3737 77624 CALL
049329,000070: 26,3740 15761 EARTHL # L VECTOR RADIANS B0
049330,000071: 26,3741 76521 MXV VSL1 # LP=M(T)*L RAD B-0
049331,000072: 26,3742 00025 MMATRIX
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Page 1132 |
049333,000074: 26,3743 77650 GOTO
049334,000075: 26,3744 55727 RPTORB
049335,000076: 24,2000 SETLOC PLANTIN
049336,000077: 24,2000 BANK
049337,000078: 24,3644 COUNT* $$/LUROT
049338,000079:
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Page 1133 |
049340,000081: # ..... R-TO-RP SUBROUTINE .....
049341,000082: # SUBROUTINE TO CONVERT R (VECTOR IN REFERENCE COORD. SYSTEM) TO RP
049342,000083: # (VECTOR IN PLANETARY COORD SYSTEM) EITHER EARTH-FIXED OR MOON-FIXED
049343,000084:
049344,000085: # RP=M(T)*(R-LXR)
049345,000086:
049346,000087: # CALLING SEQUENCE
049347,000088: # L CALL
049348,000089: # L+1 R-TO-RP
049349,000090:
049350,000091: # SUBROUTINES USED
049351,000092: # EARTHMX,MOONMX,EARTHL
049352,000093:
049353,000094: # INPUT
049354,000095: # MPAC= 0 FOR EARTH,NON-ZERO FOR MOON
049355,000096: # 0-5D= R VECTOR
049356,000097: # 6-7D= TIME
049357,000098:
049358,000099: # ITEMS AVAILABLE FROM LAUNCH DATA
049359,000100: # 504LM= THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL,EXPRESSED
049360,000101: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
049361,000102: # ITEMS NECESSARY FOR SUBROUTINES USED (SEE DESCRIPTION OF SUBR.)
049362,000103:
049363,000104: # OUTPUT
049364,000105: # MPAC=RP VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
049365,000106:
049366,000107: 24,3644 46020 R-TO-RP STQ BHIZ
049367,000108: 24,3645 00050 RPREXIT
049368,000109: 24,3646 51666 RTORPA
049369,000110: 24,3647 77624 CALL
049370,000111: 24,3650 51674 MOONMX
049371,000112: 24,3651 61375 VLOAD VXM
049372,000113: 24,3652 02013 504LM # LP=LM
049373,000114: 24,3653 00025 MMATRIX
049374,000115: 24,3654 77772 VSL1 # L=MT(T)*LP RADIANS B0
049375,000116: 24,3655 51235 RTORPB VXV BVSU
049376,000117: 24,3656 00001 504RPR
049377,000118: 24,3657 00001 504RPR
049378,000119: 24,3660 77721 MXV # M(T)*(R-LXR) B-2
049379,000120: 24,3661 00025 MMATRIX
049380,000121: 24,3662 40372 RPRPXXXX VSL1 SETPD
049381,000122: 24,3663 00001 0D
049382,000123: 24,3664 77650 GOTO
049383,000124: 24,3665 00050 RPREXIT
049384,000125: 24,3666 77624 RTORPA CALL # EARTH COMPUTATIONS
049385,000126: 24,3667 55745 EARTHMX
049386,000127: 24,3670 77624 CALL
049387,000128: 24,3671 15761 EARTHL
049388,000129: 24,3672 77650 GOTO # MPAC=L=(-AX,-AY,0) RAD B-0
049389,000130: 24,3673 51655 RTORPB
049390,000131:
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Page 1134 |
049392,000133: # ..... MOONMX SUBROUTINE .....
049393,000134: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE MOON
049394,000135:
049395,000136: # CALLING SEQUENCE
049396,000137: # L CALL
049397,000138: # L+1 MOONMX
049398,000139:
049399,000140: # SUBROUTINES USED
049400,000141: # NEWANGLE
049401,000142:
049402,000143: # INPUT
049403,000144: # 6-7D= TIME
049404,000145: # ITEMS AVAILABLE FROM LAUNCH DATA
049405,000146: # BSUBO,BDOT
049406,000147: # TIMSUBO,NODIO,NODDOT,FSUBO,FDOT
049407,000148: # COSI= COS(I) B-1
049408,000149: # SINI= SIN(I) B-1
049409,000150: # I IS THE ANGLE BETWEEN THE MEAN LUNAR EQUATORIAL PLANE AND THE
049410,000151: # PLANE OF THE ECLIPTIC (1 DEGREE 32.1 MINUTES)
049411,000152:
049412,000153: # OUTPUT
049413,000154: # MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
049414,000155:
049415,000156: 24,3674 40220 MOONMX STQ SETPD
049416,000157: 24,3675 00051 EARTHMXX
049417,000158: 24,3676 00011 8D
049418,000159: 24,3677 77770 AXT,1 # B REQUIRES SL 0, SL 5 IN NEWANGLE
049419,000160: 24,3700 00005 5
049420,000161: 24,3701 65345 DLOAD PDDL # PD 10D 8-9D=BSUBO
049421,000162: 24,3702 14017 BSUBO # 10-11D= BDOT
049422,000163: 24,3703 14011 BDOT
049423,000164: 24,3704 45006 PUSH CALL # PD 12D
049424,000165: 24,3705 51743 NEWANGLE # EXIT WITH PD 8D AND MPAC= B REVS B0
049425,000166: 24,3706 71406 PUSH COS # PD 10D
049426,000167: 24,3707 14041 STODL COB # PD 8D COS(B) B-1
049427,000168: 24,3710 77756 SIN # SIN(B) B-1
049428,000169: 24,3711 14043 STODL SOB # SETUP INPUT FOR NEWANGLE
049429,000170: 24,3712 14015 FSUBO # 8-9D=FSUBO
049430,000171: 24,3713 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=FDOT
049431,000172: 24,3714 14007 FDOT
049432,000173: 24,3715 45170 AXT,1 CALL # F REQUIRES SL 1, SL 6 IN NEWANGLE
049433,000174: 24,3716 00004 4
049434,000175: 24,3717 51743 NEWANGLE # EXIT WITH PD 8D AND MPAC= F REVS B0
049435,000176: 24,3720 14027 STODL AVECTR +2 # SAVE F TEMP
049436,000177: 24,3721 14013 NODIO # 8-9D=NODIO
049437,000178: 24,3722 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=NODDOT
049438,000179: 24,3723 14005 NODDOT # MPAC=T
049439,000180: 24,3724 45170 AXT,1 CALL # NODE REQUIRES SL 0, SL 5 IN NEWANGLE
049440,000181: 24,3725 00005 5
049441,000182: 24,3726 51743 NEWANGLE # EXIT WITH PD 8D AND MPAC= NODI REVS B0
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Page 1135 |
049443,000184: 24,3727 71406 PUSH COS # PD 10D 8-9D= NODI REVS B0
049444,000185: 24,3730 77606 PUSH # PD 12D 10-11D= COS(NODI) B-1
049445,000186: 24,3731 00025 STORE AVECTR
049446,000187: 24,3732 76405 DMP SL1R
049447,000188: 24,3733 00041 COB # COS(NODI) B-1
049448,000189: 24,3734 14035 STODL BVECTR +2 # PD 10D 20-25D=AVECTR= COB*SIN(NODI)
049449,000190: 24,3735 76405 DMP SL1R # SOB*SIN(NODI)
049450,000191: 24,3736 00043 SOB
049451,000192: 24,3737 14037 STODL BVECTR +4 # PD 8D
049452,000193: 24,3740 41556 SIN PUSH # PD 10D -SIN(NODI) B-1
049453,000194: 24,3741 52076 DCOMP GOTO # 26-31D=BVECTR= COV*COS(NODI)
049454,000195: 24,3742 53710 MOONMXA
049455,000196: 25,3710 BANK 25
049456,000197: 25,2000 SETLOC PLANTIN3
049457,000198: 25,2000 BANK
049458,000199: 25,3710 COUNT* $$/LUROT
049459,000200:
049460,000201: 25,3710 14033 MOONMXA STODL BVECTR # PD 8D SOB*COS(NODI)
049461,000202: 25,3711 00027 AVECTR +2 # MOVE F FROM TEMP LOC. TO 504F
049462,000203: 25,3712 14007 STODL 504F
049463,000204: 25,3713 76405 DMP SL1R
049464,000205: 25,3714 00041 COB
049465,000206: 25,3715 14027 STODL AVECTR +2
049466,000207: 25,3716 00011 SINNODI # 8-9D=SIN(NODI) B-1
049467,000208: 25,3717 76405 DMP SL1R
049468,000209: 25,3720 00043 SOB
049469,000210: 25,3721 14031 STODL AVECTR +4 # 0
049470,000211: 25,3722 06520 HI6ZEROS # 8-13D= CVECTR= -SOB B-1
049471,000212: 25,3723 57525 PDDL DCOMP # PD 10D COB
049472,000213: 25,3724 00043 SOB
049473,000214: 25,3725 63325 PDDL PDVL # PD 12D THEN PD 14D
049474,000215: 25,3726 00041 COB
049475,000216: 25,3727 00033 BVECTR
049476,000217: 25,3730 63361 VXSC PDVL # PD 20D BVECTR*SINI B-2
049477,000218: 25,3731 14003 SINI
049478,000219: 25,3732 00011 CVECTR
049479,000220: 25,3733 53361 VXSC VAD # PD 14D CVECTR*COSI B-2
049480,000221: 25,3734 14001 COSI
049481,000222: 25,3735 77772 VSL1
049482,000223: 25,3736 24041 STOVL MMATRIX +12D # PD 8D M2=BVECTR*SINI+CVECTR*COSI B-1
049483,000224: 25,3737 63361 VXSC PDVL # PD 14D
049484,000225: 25,3740 14003 SINI # CVECTR*SINI B-2
049485,000226: 25,3741 00033 BVECTR
049486,000227: 25,3742 52361 VXSC VSU # PD 8D BVECTR*COSI B-2
049487,000228: 25,3743 14001 COSI
049488,000229: 25,3744 65372 VSL1 PDDL # PD 14D
049489,000230: 25,3745 00007 504F # 8-13D=DVECTR=BVECTR*COSI-CVECTR*SINI B-1
049490,000231: 25,3746 74346 COS VXSC
049491,000232: 25,3747 00011 DVECTR
049492,000233: 25,3750 73525 PDDL SIN # PD 20D 14-19D= DVECTR*COSF B-2
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Page 1136 |
049494,000235: 25,3751 00007 504F
049495,000236: 25,3752 52361 VXSC VSU # PD 14D AVECTR*SINF B-2
049496,000237: 25,3753 00025 AVECTR
049497,000238: 25,3754 77772 VSL1
049498,000239: 25,3755 14033 STODL MMATRIX +6 # M1= AVECTR*SINF-DVECTR*COSF B-1
049499,000240: 25,3756 00007 504F
049500,000241: 25,3757 74356 SIN VXSC # PD 8D
049501,000242: 25,3760 71525 PDDL COS # PD 14D 8-13D=DVECTR*SINF B-2
049502,000243: 25,3761 00007 504F
049503,000244: 25,3762 53361 VXSC VAD # PD 8D AVECTR*COSF B-2
049504,000245: 25,3763 00025 AVECTR
049505,000246: 25,3764 57572 VSL1 VCOMP
049506,000247: 25,3765 34025 STCALL MMATRIX # M0= -(AVECTR*COSF+DVECTR*SINF) B-1
049507,000248: 25,3766 00051 EARTHMXX
049508,000249: # COMPUTE X=X0+(XDOT)(T+T0)
049509,000250: # 8-9D= XO (REVS B-0),PUSHLOC SET AT 12D
049510,000251: # 10-11D=XDOT (REVS/CSEC) SCALED B+23 FOR WEARTH,B+28 FOR NODDOT AND BDOT
049511,000252: # AND B+27 FOR FDOT
049512,000253: # X1=DIFFERENCE IN 23 AND SCALING OF XDOT,=0 FOR WEARTH,5 FOR NODDOT AND
049513,000254: # BDOT AND 4 FOR FDOT
049514,000255: # 6-7D=T (CSEC B-28), TIMSUBO= (CSEC B-42 TRIPLE PREC.)
049515,000256:
049516,000257: 24,3743 BANK 24
049517,000258: 24,2000 SETLOC PLANTIN
049518,000259: 24,2000 BANK
049519,000260:
049520,000261: 24,3743 54345 NEWANGLE DLOAD SR # ENTER PD 12D
049521,000262: 24,3744 00007 6D
049522,000263: 24,3745 20617 14D
049523,000264: 24,3746 72371 TAD TLOAD # CHANGE MODE TO TP
049524,000265: 24,3747 01707 TIMSUBO
049525,000266: 24,3750 00155 MPAC
049526,000267: 24,3751 14017 STODL TIMSUBM # T+T0 CSEC B-42
049527,000268: 24,3752 00020 TIMSUBM +1
049528,000269: 24,3753 77605 DMP # PD 10D MULT BY XDOT IN 10-11D
049529,000270: 24,3754 43257 SL* DAD # PD 8D ADD XO IN 8-9D AFTER SHIFTING
049530,000271: 24,3755 20206 5,1 # SUCH THAT SCALING IS B-0
049531,000272: 24,3756 67206 PUSH SLOAD # PD 10D SAVE PARTIAL (X0+XDOT*T) IN 8-9D
049532,000273: 24,3757 00017 TIMSUBM
049533,000274: 24,3760 41261 SL DMP
049534,000275: 24,3761 20212 9D
049535,000276: 24,3762 00013 10D # XDOT
049536,000277: 24,3763 43257 SL* DAD # PD 8D SHIFT SUCH THAT THIS PART OF X
049537,000278: 24,3764 20213 10D,1 # IS SCALED REVS/CSEC B-0
049538,000279: 24,3765 77600 BOV # TURN OFF OVERFLOW IF SET BY SHIFT
049539,000280: 24,3766 51767 +1 # INSTRUCTION BEFORE EXITING
049540,000281: 24,3767 77616 RVQ # MPAC=X= X0+(XDOT)(T+T0) REVS B0
049541,000282:
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Page 1137 |
049543,000284: # ..... EARTHMX SUBROUTINE .....
049544,000285: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE EARTH
049545,000286:
049546,000287: # CALLING SEQUENCE
049547,000288: # L CALL
049548,000289: # L+1 EARTHMX
049549,000290:
049550,000291: # SUBROUTINES USED
049551,000292: # NEWANGLE
049552,000293:
049553,000294: # INPUT
049554,000295: # INPUT AVAILABLE FROM LAUNCH DATA AZO REVS B-0
049555,000296: # TEPHEM CSEC B-42
049556,000297: # 6-7D= TIME CSEC B-28
049557,000298:
049558,000299: # OUTPUT
049559,000300: # MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
049560,000301:
049561,000302: 26,3745 BANK 26
049562,000303: 26,2000 SETLOC PLANTIN1
049563,000304: 26,2000 BANK
049564,000305: 26,3745 COUNT* $$/LUROT
049565,000306:
049566,000307: 26,3745 40220 EARTHMX STQ SETPD # SET 8-9D=AZO
049567,000308: 26,3746 00051 EARTHMXX
049568,000309: 26,3747 00011 8D # 10-11D=WEARTH
049569,000310: 26,3750 77770 AXT,1 # FOR SL 5, AND SL 10 IN NEWANGLE
049570,000311: 26,3751 00000 0
049571,000312: 26,3752 65345 DLOAD PDDL # LEAVING PD SET AT 12D FOR NEWANGLE
049572,000313: 26,3753 14023 AZO
049573,000314: 26,3754 14021 WEARTH
049574,000315: 26,3755 45006 PUSH CALL
049575,000316: 26,3756 51743 NEWANGLE
049576,000317: 26,3757 41401 SETPD PUSH # 18-19D=504AZ
049577,000318: 26,3760 00023 18D # COS(AZ) SIN(AZ) 0
049578,000319: 26,3761 65346 COS PDDL # 20-37D= MMATRIX= -SIN(AZ) COS(AZ) 0 B-1
049579,000320: 26,3762 00023 504AZ # 0 0 1
049580,000321: 26,3763 65356 SIN PDDL
049581,000322: 26,3764 06520 HI6ZEROS
049582,000323: 26,3765 73525 PDDL SIN
049583,000324: 26,3766 00023 504AZ
049584,000325: 26,3767 65276 DCOMP PDDL
049585,000326: 26,3770 00023 504AZ
049586,000327: 26,3771 63346 COS PDVL
049587,000328: 26,3772 06520 HI6ZEROS
049588,000329: 26,3773 41525 PDDL PUSH
049589,000330: 26,3774 06516 HIDPHALF
049590,000331: 26,3775 77650 GOTO
049591,000332: 26,3776 00051 EARTHMXX
049592,000333:
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Page 1138 |
049594,000335: # ..... EARTHL SUBROUTINE .....
049595,000336: # SUBROUTINE TO COMPUTE L VECTOR FOR EARTH
049596,000337:
049597,000338: # CALLING SEQUENCE
049598,000339: # L CALL
049599,000340: # L+1 EARTHL
049600,000341:
049601,000342: # INPUT
049602,000343: # AXO,AYO SET AT LAUNCH TIME WITH AYO IMMEDIATELY FOLLOWING AXO IN CORE
049603,000344:
049604,000345: # OUTPUT
049605,000346: # -AX
049606,000347: # MPAC= -AY RADIANS B-0
049607,000348: # 0
049608,000349:
049609,000350: 06,3761 BANK 06
049610,000351: 06,2000 SETLOC EARTHLOC
049611,000352: 06,2000 BANK
049612,000353: 06,3761 COUNT* $$/LUROT
049613,000354:
049614,000355: 06,3761 57545 EARTHL DLOAD DCOMP
049615,000356: 06,3762 01714 AXO
049616,000357: 06,3763 14017 STODL 504LPL
049617,000358: 06,3764 01712 -AYO
049618,000359: 06,3765 14021 STODL 504LPL +2
049619,000360: 06,3766 24007 LO6ZEROS
049620,000361: 06,3767 24023 STOVL 504LPL +4
049621,000362: 06,3770 00017 504LPL
049622,000363: 06,3771 77616 RVQ
049623,000364:
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Page 1139 |
049625,000366: # CONSTANTS AND ERASABLE ASSIGNMENTS
049626,000367: 06,3772 12,2004 1B1 = DP1/2 # 1 SCALED B-1
049627,000368: 06,3772 0000050 RPREXIT = S1 # R-TO-RP AND RP-TO-R SUBR EXIT
049628,000369: 06,3772 0000051 EARTHMXX = S2 # EARTHMX,MOONMX SUBR. EXITS
049629,000370: 06,3772 504RPR = 0D # 6 REGS R OR RP VECTOR
049630,000371: 06,3772 SINNODI = 8D # 2 SIN(NODI)
049631,000372: 06,3772 DVECTR = 8D # 6 D VECTOR MOON
049632,000373: 06,3772 CVECTR = 8D # 6 C VECTR MOON
049633,000374: 06,3772 504AZ = 18D # 2 AZ
049634,000375: 06,3772 TIMSUBM = 14D # 3 TIME SUB M (MOON) T+T0 IN GETAZ
049635,000376: 06,3772 504LPL = 14D # 6 L OR LP VECTOR
049636,000377: 06,3772 AVECTR = 20D # 6 A VECTOR (MOON)
049637,000378: 06,3772 BVECTR = 26D # 6 B VECTOR (MOON)
049638,000379: 06,3772 MMATRIX = 20D # 18 M MATRIX
049639,000380: 06,3772 COB = 32D # 2 COS(B) B-1
049640,000381: 06,3772 SOB = 34D # 2 SIN(B) B-1
049641,000382: 06,3772 504F = 6D # 2 F(MOON)
End of include-file PLANETARY_INERTIAL_ORIENTATION.agc. Parent file is MAIN.agc