Source Code
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This is a reconstructed version of Luminary 130, the initial AGC program released
in November 1969 for the Apollo 13 LM. Three more releases
followed before the flown revision was finally manufactured in February 1970.
This reconstruction was created from a previous transcription of the original listing of
Luminary 131, combined with Luminary memo #129 which describes the small difference
between the Luminary 130 and 131. The reconstructed source code was verified by
matching memory-bank checksums to those listed for Luminary 130 in drawing 2021152G.
In this source code, program comments from the original (Luminary 131) code are
prefixed with '#', while those added later by the Virtual AGC project are prefixed
with '##'.
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047757,000002: ## Copyright: Public domain.
047758,000003: ## Filename: PLANETARY_INERTIAL_ORIENTATION.agc
047759,000004: ## Purpose: A section of the reconstructed source code for Luminary 130.
047760,000005: ## This was the original program released for the Apollo 13 LM,
047761,000006: ## although several more revisions would follow. It has been
047762,000007: ## reconstructed from a listing of Luminary 131, from which it
047763,000008: ## differs on only two lines in P70-P71. The difference is
047764,000009: ## described in detail in Luminary memo #129, which was used
047765,000010: ## to perform the reconstruction. This file is intended to be a
047766,000011: ## faithful reconstruction, except that the code format has been
047767,000012: ## changed to conform to the requirements of the yaYUL assembler
047768,000013: ## rather than the original YUL assembler.
047769,000014: ## Reference: pp. 1134-1142
047770,000015: ## Contact: Ron Burkey <info@sandroid.org>.
047771,000016: ## Website: www.ibiblio.org/apollo/index.html
047772,000017: ## Mod history: 06/01/03 RSB. Began transcribing.
047773,000018: ## 05/14/05 RSB Corrected website reference above.
047774,000019: ## 2017-01-06 RSB Page numbers now agree with those on the
047775,000020: ## original hardcopy, as opposed to the PDF page
047776,000021: ## numbers in 1701.pdf.
047777,000022: ## 2017-02-27 RSB Proofed comment text using octopus/ProoferComments.
047778,000023: ## 2017-03-14 RSB Comment-text fixes noted in proofing Luminary 116.
047779,000024: ## 2017-03-16 RSB Comment-text fixes identified in 5-way
047780,000025: ## side-by-side diff of Luminary 69/99/116/131/210.
047781,000026: ## 2018-09-04 MAS Copied from Luminary 131 for Luminary 130.
047782,000027:
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Page 1134
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047784,000029: # ..... RP-TO-R SUBROUTINE .....
047785,000030: # SUBROUTINE TO CONVERT RP (VECTOR IN PLANETARY COORDINATE SYSTEM, EITHER
047786,000031: # EARTH-FIXED OR MOON-FIXED) TO R (SAME VECTOR IN THE BASIC REF. SYSTEM)
047787,000032: # R = MT(T) * (RP + LP X RP) MT = M MATRIX TRANSPOSE
047788,000033:
047789,000034: # CALLING SEQUENCE
047790,000035: # L CALL
047791,000036: # L+1 RP-TO-R
047792,000037:
047793,000038: # SUBROUTINES USED
047794,000039: # EARTHMX, MOONMX, EARTHL
047795,000040:
047796,000041: # ITEMS AVAILABLE FROM LAUNCH DATA
047797,000042: # 504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
047798,000043: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
047799,000044:
047800,000045: # ITEMS NECESSARY FOR SUBR. USED (SEE DESCRIPTION OF SUBR.)
047801,000046:
047802,000047: # INPUT
047803,000048: # MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
047804,000049: # 0-5D = RP VECTOR
047805,000050: # 6-7D = TIME
047806,000051:
047807,000052: # OUTPUT
047808,000053: # MPAC = R VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
047809,000054:
047810,000055: 26,2000 SETLOC PLANTIN1
047811,000056: 26,2000 BANK
047812,000057:
047813,000058: 26,3716 COUNT* $$/LUROT
047814,000059:
047815,000060: 26,3716 46020 RP-TO-R STQ BHIZ
047816,000061: 26,3717 00050 RPREXIT
047817,000062: 26,3720 55733 RPTORA
047818,000063: 26,3721 77624 CALL # COMPUTE M MATRIX FOR MOON
047819,000064: 26,3722 51730 MOONMX # LP=LM FOR MOON RADIANS B0
047820,000065: 26,3723 77775 VLOAD
047821,000066: 26,3724 02013 504LM
047822,000067: 26,3725 53235 RPTORB VXV VAD
047823,000068: 26,3726 00001 504RPR
047824,000069: 26,3727 00001 504RPR
047825,000070: 26,3730 52105 VXM GOTO
047826,000071: 26,3731 00025 MMATRIX # MPAC=R=MT(T)*(RP+LPXRP)
047827,000072: 26,3732 51716 RPRPXXXX # RESET PUSHLOC TO 0 BEFORE EXITING
047828,000073: 26,3733 77624 RPTORA CALL # EARTH COMPUTATIONS
047829,000074: 26,3734 55743 EARTHMX # M MATRIX B-1
047830,000075: 26,3735 77624 CALL
047831,000076: 26,3736 15761 EARTHL # L VECTOR RADIANS B0
047832,000077: 26,3737 76521 MXV VSL1 # LP=M(T)*L RAD B-0
047833,000078: 26,3740 00025 MMATRIX
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Page 1135
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047835,000080: 26,3741 77650 GOTO
047836,000081: 26,3742 55725 RPTORB
047837,000082: 24,2000 SETLOC PLANTIN
047838,000083: 24,2000 BANK
047839,000084: 24,3700 COUNT* $$/LUROT
047840,000085:
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Page 1136
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047842,000087: # ..... R-TO-RP SUBROUTINE .....
047843,000088: # SUBROUTINE TO CONVERT R (VECTOR IN REFERENCE COORD. SYSTEM) TO RP
047844,000089: # (VECTOR IN PLANETARY COORD SYSTEM) EITHER EARTH-FIXED OR MOON-FIXED
047845,000090: # RP = M(T) * (R - L X R)
047846,000091:
047847,000092: # CALLING SEQUENCE
047848,000093: # L CALL
047849,000094: # L+1 R-TO-RP
047850,000095:
047851,000096: # SUBROUTINES USED
047852,000097: # EARTHMX, MOONMX, EARTHL
047853,000098:
047854,000099: # INPUT
047855,000100: # MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
047856,000101: # 0-5D = R VECTOR
047857,000102: # 6-7D = TIME
047858,000103:
047859,000104: # ITEMS AVAILABLE FROM LAUNCH DATA
047860,000105: # 504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
047861,000106: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
047862,000107:
047863,000108: # ITEMS NECESSARY FOR SUBROUTINES USED (SEE DESCRIPTION OF SUBR.)
047864,000109:
047865,000110: # OUTPUT
047866,000111: # MPAC = RP VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
047867,000112:
047868,000113: 24,3700 46020 R-TO-RP STQ BHIZ
047869,000114: 24,3701 00050 RPREXIT
047870,000115: 24,3702 51722 RTORPA
047871,000116: 24,3703 77624 CALL
047872,000117: 24,3704 51730 MOONMX
047873,000118: 24,3705 61375 VLOAD VXM
047874,000119: 24,3706 02013 504LM # LP=LM
047875,000120: 24,3707 00025 MMATRIX
047876,000121: 24,3710 77772 VSL1 # L = MT(T)*LP RADIANS B0
047877,000122: 24,3711 51235 RTORPB VXV BVSU
047878,000123: 24,3712 00001 504RPR
047879,000124: 24,3713 00001 504RPR
047880,000125: 24,3714 77721 MXV # M(T)*(R-LXR) B-2
047881,000126: 24,3715 00025 MMATRIX
047882,000127: 24,3716 40372 RPRPXXXX VSL1 SETPD
047883,000128: 24,3717 00001 0D
047884,000129: 24,3720 77650 GOTO
047885,000130: 24,3721 00050 RPREXIT
047886,000131: 24,3722 77624 RTORPA CALL # EARTH COMPUTATIONS
047887,000132: 24,3723 55743 EARTHMX
047888,000133: 24,3724 77624 CALL
047889,000134: 24,3725 15761 EARTHL
047890,000135: 24,3726 77650 GOTO # MPAC=L=(-AX,-AY,0) RAD B-0
047891,000136: 24,3727 51711 RTORPB
047892,000137:
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Page 1137
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047894,000139: # ..... MOONMX SUBROUTINE .....
047895,000140: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE MOON
047896,000141:
047897,000142: # CALLING SEQUENCE
047898,000143: # L CALL
047899,000144: # L+1 MOONMX
047900,000145:
047901,000146: # SUBROUTINES USED
047902,000147: # NEWANGLE
047903,000148:
047904,000149: # INPUT
047905,000150: # 6-7D = TIME
047906,000151:
047907,000152: # ITEMS AVAILABLE FROM LAUNCH DATA
047908,000153: # BSUBO, BDOT
047909,000154: # TIMSUBO, NODIO, NODDOT, FSUBO, FDOT
047910,000155: # COSI = COS(I) B-1
047911,000156: # SINI = SIN(I) B-1
047912,000157: # I IS THE ANGLE BETWEEN THE MEAN LUNAR EQUATORIAL PLANE AND THE
047913,000158: # PLANE OF THE ECLIPTIC (1 DEGREE 32.1 MINUTES)
047914,000159:
047915,000160: # OUTPUT
047916,000161: # MMATRIX = 3X3 M MATRIX B-1 (STORED IN VAC AREA)
047917,000162:
047918,000163: 24,3730 40220 MOONMX STQ SETPD
047919,000164: 24,3731 00051 EARTHMXX
047920,000165: 24,3732 00011 8D
047921,000166: 24,3733 77770 AXT,1 # B REQUIRES SL 0, SL 5 IN NEWANGLE
047922,000167: 24,3734 00005 5
047923,000168: 24,3735 65345 DLOAD PDDL # PD 10D 8-9D=BSUBO
047924,000169: 24,3736 14017 BSUBO # 10-11D=BDOT
047925,000170: 24,3737 14011 BDOT
047926,000171: 24,3740 45006 PUSH CALL # PD 12D
047927,000172: 24,3741 53732 NEWANGLE # EXIT WITH PD 8D AND MPAC= B REVS B0
047928,000173: 24,3742 71406 PUSH COS # PD 10D
047929,000174: 24,3743 14041 STODL COB # PD 8D COS(B) B-1
047930,000175: 24,3744 77756 SIN # SIN(B) B-1
047931,000176: 24,3745 14043 STODL SOB # SETUP INPUT FOR NEWANGLE
047932,000177: 24,3746 14015 FSUBO # 8-9D=FSUBO
047933,000178: 24,3747 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=FDOT
047934,000179: 24,3750 14007 FDOT
047935,000180: 24,3751 45170 AXT,1 CALL # F REQUIRES SL 1, SL 6 IN NEWANGLE
047936,000181: 24,3752 00004 4
047937,000182: 24,3753 53732 NEWANGLE # EXIT WITH PD 8D AND MPAC= F REVS B0
047938,000183: 24,3754 14027 STODL AVECTR +2 # SAVE F TEMP
047939,000184: 24,3755 14013 NODIO # 8-9D=NODIO
047940,000185: 24,3756 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=NODDOT
047941,000186: 24,3757 14005 NODDOT # MPAC=T
047942,000187: 24,3760 45170 AXT,1 CALL # NODE REQUIRES SL 0, SL 5 IN NEWANGLE
047943,000188: 24,3761 00005 5
047944,000189: 24,3762 53732 NEWANGLE # EXIT WITH PD 8D AND MPAC= NODI REVS B0
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Page 1138
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047946,000191: 24,3763 71406 PUSH COS # PD 10D 8-9D= NODI REVS B0
047947,000192: 24,3764 77606 PUSH # PD 12D 10-11D= COS(NODI) B-1
047948,000193: 24,3765 00025 STORE AVECTR
047949,000194: 24,3766 76405 DMP SL1R
047950,000195: 24,3767 00041 COB # COS(NODI) B-1
047951,000196: 24,3770 14035 STODL BVECTR +2 # PD 10D 20-25D=AVECTR=COB*SIN(NODI)
047952,000197: 24,3771 76405 DMP SL1R # SOB*SIN(NODI)
047953,000198: 24,3772 00043 SOB
047954,000199: 24,3773 14037 STODL BVECTR +4 # PD 8D
047955,000200: 24,3774 41556 SIN PUSH # PD 10D -SIN(NODI) B-1
047956,000201: 24,3775 52076 DCOMP GOTO # 26-31D=BVECTR=COV*COS(NODI)
047957,000202: 24,3776 53653 MOONMXA
047958,000203:
047959,000204: 25,3653 BANK 25
047960,000205: 25,2000 SETLOC PLANTIN3
047961,000206: 25,2000 BANK
047962,000207: 25,3653 COUNT* $$/LUROT
047963,000208:
047964,000209: 25,3653 14033 MOONMXA STODL BVECTR # PD 8D SOB*COS(NODI)
047965,000210: 25,3654 00027 AVECTR +2 # MOVE F FROM TEMP LOC. TO 504F
047966,000211: 25,3655 14007 STODL 504F
047967,000212: 25,3656 76405 DMP SL1R
047968,000213: 25,3657 00041 COB
047969,000214: 25,3660 14027 STODL AVECTR +2
047970,000215: 25,3661 00011 SINNODI # 8-9D=SIN(NODI) B-1
047971,000216: 25,3662 76405 DMP SL1R
047972,000217: 25,3663 00043 SOB
047973,000218: 25,3664 14031 STODL AVECTR +4 # 0
047974,000219: 25,3665 06524 HI6ZEROS # 8-13D= CVECTR= -SOB B-1
047975,000220: 25,3666 57525 PDDL DCOMP # PD 10D COB
047976,000221: 25,3667 00043 SOB
047977,000222: 25,3670 63325 PDDL PDVL # PD 12D THEN PD 14D
047978,000223: 25,3671 00041 COB
047979,000224: 25,3672 00033 BVECTR
047980,000225: 25,3673 63361 VXSC PDVL # PD 20D BVECTR*SINI B-2
047981,000226: 25,3674 14003 SINI
047982,000227: 25,3675 00011 CVECTR
047983,000228: 25,3676 53361 VXSC VAD # PD 14D CVECTR*COSI B-2
047984,000229: 25,3677 14001 COSI
047985,000230: 25,3700 77772 VSL1
047986,000231: 25,3701 24041 STOVL MMATRIX +12D # PD 8D M2=BVECTR*SINI+CVECTR*COSI B-1
047987,000232: 25,3702 63361 VXSC PDVL # PD 14D
047988,000233: 25,3703 14003 SINI # CVECTR*SINI B-2
047989,000234: 25,3704 00033 BVECTR
047990,000235: 25,3705 52361 VXSC VSU # PD 8D BVECTR*COSI B-2
047991,000236: 25,3706 14001 COSI
047992,000237: 25,3707 65372 VSL1 PDDL # PD 14D
047993,000238: 25,3710 00007 504F # 8-13D=DVECTR=BVECTR*COSI-CVECTR*SINI B-1
047994,000239: 25,3711 74346 COS VXSC
047995,000240: 25,3712 00011 DVECTR
047996,000241: 25,3713 73525 PDDL SIN # PD 20D 14-19D= DVECTR*COSF B-2
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Page 1139
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047998,000243: 25,3714 00007 504F
047999,000244: 25,3715 52361 VXSC VSU # PD 14D AVECTR*SINF B-2
048000,000245: 25,3716 00025 AVECTR
048001,000246: 25,3717 77772 VSL1
048002,000247: 25,3720 14033 STODL MMATRIX +6 # M1= AVECTR*SINF-DVECTR*COSF B-1
048003,000248: 25,3721 00007 504F
048004,000249: 25,3722 74356 SIN VXSC # PD 8D
048005,000250: 25,3723 71525 PDDL COS # PD 14D 8-13D=DVECTR*SINF B-2
048006,000251: 25,3724 00007 504F
048007,000252: 25,3725 53361 VXSC VAD # PD 8D AVECTR*COSF B-2
048008,000253: 25,3726 00025 AVECTR
048009,000254: 25,3727 57572 VSL1 VCOMP
048010,000255: 25,3730 34025 STCALL MMATRIX # M0= -(AVECTR*COSF+DVECTR*SINF) B-1
048011,000256: 25,3731 00051 EARTHMXX
048012,000257:
048013,000258: # COMPUTE X=X0+(XDOT)(T+T0)
048014,000259: # 8-9D= XO (REVS B-0), PUSHLOC SET AT 12D
048015,000260: # 10-11D=XDOT (REVS/CSEC) SCALED B+23 FOR WEARTH,B+28 FOR NODDOT AND BDOT
048016,000261: # AND B+27 FOR FDOT
048017,000262: # X1=DIFFERENCE IN 23 AND SCALING OF XDOT, =0 FOR WEARTH,5 FOR NODDOT AND
048018,000263: # BDOT AND 4 FOR FDOT
048019,000264: # 6-7D=T (CSEC B-28), TIMSUBO= (CSEC B-42 TRIPLE PREC.)
048020,000265:
048021,000266: 25,3732 54345 NEWANGLE DLOAD SR # ENTER PD 12D
048022,000267: 25,3733 00007 6D
048023,000268: 25,3734 20617 14D
048024,000269: 25,3735 72371 TAD TLOAD # CHANGE MODE TO TP
048025,000270: 25,3736 01707 TIMSUBO
048026,000271: 25,3737 00155 MPAC
048027,000272: 25,3740 14017 STODL TIMSUBM # T+T0 CSEC B-42
048028,000273: 25,3741 00020 TIMSUBM +1
048029,000274: 25,3742 77605 DMP # PD 10D MULT BY XDOT IN 10-11D
048030,000275: 25,3743 43257 SL* DAD # PD 8D ADD XO IN 8-9D AFTER SHIFTING
048031,000276: 25,3744 20206 5,1 # SUCH THAT SCALING IS B-0
048032,000277: 25,3745 67206 PUSH SLOAD # PD 10D SAVE PARTIAL (X0+XDOT*T) IN 8-9D
048033,000278: 25,3746 00017 TIMSUBM
048034,000279: 25,3747 41261 SL DMP
048035,000280: 25,3750 20212 9D
048036,000281: 25,3751 00013 10D # XDOT
048037,000282: 25,3752 43257 SL* DAD # PD 8D SHIFT SUCH THAT THIS PART OF X
048038,000283: 25,3753 20213 10D,1 # IS SCALED REVS/CSEC B-0
048039,000284: 25,3754 77600 BOV # TURN OFF OVERFLOW IF SET BY SHIFT
048040,000285: 25,3755 53756 +1 # INSTRUCTION BEFORE EXITING
048041,000286: 25,3756 77616 RVQ # MPAC=X= X0+(XDOT)(T+T0) REVS B0
048042,000287:
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Page 1140
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048044,000289: # ..... EARTHMX SUBROUTINE .....
048045,000290: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE EARTH
048046,000291:
048047,000292: # CALLING SEQUENCE
048048,000293: # L CALL
048049,000294: # L+1 EARTHMX
048050,000295:
048051,000296: # SUBROUTINES USED
048052,000297: # NEWANGLE
048053,000298:
048054,000299: # INPUT
048055,000300: # INPUT AVAILABLE FROM LAUNCH DATA AZO REVS B-0
048056,000301: # TEPHEM CSEC B-42
048057,000302: # 6-7D= TIME CSEC B-28
048058,000303:
048059,000304: # OUTPUT
048060,000305: # MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
048061,000306:
048062,000307: 26,3743 BANK 26
048063,000308: 26,2000 SETLOC PLANTIN1
048064,000309: 26,2000 BANK
048065,000310: 26,3743 COUNT* $$/LUROT
048066,000311:
048067,000312: 26,3743 40220 EARTHMX STQ SETPD # SET 8-9D=AZO
048068,000313: 26,3744 00051 EARTHMXX
048069,000314: 26,3745 00011 8D # 10-11D=WEARTH
048070,000315: 26,3746 77770 AXT,1 # FOR SL 5, AND SL 10 IN NEWANGLE
048071,000316: 26,3747 00000 0
048072,000317: 26,3750 65345 DLOAD PDDL # LEAVING PD SET AT 12D FOR NEWANGLE
048073,000318: 26,3751 01712 AZO
048074,000319: 26,3752 14021 WEARTH
048075,000320: 26,3753 45006 PUSH CALL
048076,000321: 26,3754 53732 NEWANGLE
048077,000322: 26,3755 41401 SETPD PUSH # 18-19D=504AZ
048078,000323: 26,3756 00023 18D # COS(AZ) SIN(AZ) 0
048079,000324: 26,3757 65346 COS PDDL # 20-37D= MMATRIX= -SIN(AZ) COS(AZ) 0 B-1
048080,000325: 26,3760 00023 504AZ # 0 0 1
048081,000326: 26,3761 65356 SIN PDDL
048082,000327: 26,3762 06524 HI6ZEROS
048083,000328: 26,3763 73525 PDDL SIN
048084,000329: 26,3764 00023 504AZ
048085,000330: 26,3765 65276 DCOMP PDDL
048086,000331: 26,3766 00023 504AZ
048087,000332: 26,3767 63346 COS PDVL
048088,000333: 26,3770 06524 HI6ZEROS
048089,000334: 26,3771 41525 PDDL PUSH
048090,000335: 26,3772 06522 HIDPHALF
048091,000336: 26,3773 77650 GOTO
048092,000337: 26,3774 00051 EARTHMXX
048093,000338:
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Page 1141
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048095,000340: # ..... EARTHL SUBROUTINE .....
048096,000341: # SUBROUTINE TO COMPUTE L VECTOR FOR EARTH
048097,000342:
048098,000343: # CALLING SEQUENCE
048099,000344: # L CALL
048100,000345: # L+1 EARTHL
048101,000346:
048102,000347: # INPUT
048103,000348: # AXO,AYO SET AT LAUNCH TIME WITH AYO IMMEDIATELY FOLLOWING AXO IN CORE
048104,000349:
048105,000350: # OUTPUT
048106,000351: # -AX
048107,000352: # MPAC= -AY RADIANS B-0
048108,000353: # 0
048109,000354:
048110,000355: 06,3761 BANK 06
048111,000356: 06,2000 SETLOC EARTHLOC
048112,000357: 06,2000 BANK
048113,000358: 06,3761 COUNT* $$/LUROT
048114,000359:
048115,000360: 06,3761 57545 EARTHL DLOAD DCOMP
048116,000361: 06,3762 01716 AXO
048117,000362: 06,3763 14017 STODL 504LPL
048118,000363: 06,3764 01714 -AYO
048119,000364: 06,3765 14021 STODL 504LPL +2
048120,000365: 06,3766 24007 LO6ZEROS
048121,000366: 06,3767 24023 STOVL 504LPL +4
048122,000367: 06,3770 00017 504LPL
048123,000368: 06,3771 77616 RVQ
048124,000369:
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Page 1142
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048126,000371: # CONSTANTS AND ERASABLE ASSIGNMENTS
048127,000372:
048128,000373: 06,3772 12,2004 1B1 = DP1/2 # 1 SCALED B-1
048129,000374: 06,3772 0000050 RPREXIT = S1 # R-TO-RP AND RP-TO-R SUBR EXIT
048130,000375: 06,3772 0000051 EARTHMXX = S2 # EARTHMX, MOONMX SUBR. EXITS
048131,000376: 06,3772 504RPR = 0D # 6 REGS R OR RP VECTOR
048132,000377: 06,3772 SINNODI = 8D # 2 SIN(NODI)
048133,000378: 06,3772 DVECTR = 8D # 6 D VECTOR MOON
048134,000379: 06,3772 CVECTR = 8D # 6 C VECTR MOON
048135,000380: 06,3772 504AZ = 18D # 2 AZ
048136,000381: 06,3772 TIMSUBM = 14D # 3 TIME SUB M (MOON) T+T0 IN GETAZ
048137,000382: 06,3772 504LPL = 14D # 6 L OR LP VECTOR
048138,000383: 06,3772 AVECTR = 20D # 6 A VECTOR (MOON)
048139,000384: 06,3772 BVECTR = 26D # 6 B VECTOR (MOON)
048140,000385: 06,3772 MMATRIX = 20D # 18 M MATRIX
048141,000386: 06,3772 COB = 32D # 2 COS(B) B-1
048142,000387: 06,3772 SOB = 34D # 2 SIN(B) B-1
048143,000388: 06,3772 504F = 6D # 2 F(MOON)
048144,000389:
End of include-file PLANETARY_INERTIAL_ORIENTATION.agc. Parent file is MAIN.agc