Source Code
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These source-code files were from the printout at the MIT Museum, with many thanks
to Deborah Douglas, the Museum's Curator of Science and Technology, for releasing
it to us. The printout was digitally photographed by Paul Fjeld. A team of
volunteers transcribed the source code manually from these images or, where
appropriate, modified already-transcribed but similar source Luminary 131 (Apollo 13)
source code to agree with the images from the printout. Note that the page images
presented online are of reduced quality, and that higher-quality images
are available. Report any conversion errors or legibility
problems in page images to info@sandroid.org.
Notations on the program listing read, in part:GAP: ASSEMBLE REVISION 001 OF AGC PROGRAM LMY99 BY NASA 2021112-061 20'35 OCT. 28,1968Note that the date is the date of the printout, not the date of the program revision. |
048607,000002: ## Copyright: Public domain.
048608,000003: ## Filename: PLANETARY_INERTIAL_ORIENTATION.agc
048609,000004: ## Purpose: Part of the source code for Luminary 1A build 099.
048610,000005: ## It is part of the source code for the Lunar Module's (LM)
048611,000006: ## Apollo Guidance Computer (AGC), for Apollo 11.
048612,000007: ##
048613,000008: ## Assembler: yaYUL
048614,000009: ## Contact: Jim Lawton <jim.lawton@gmail.com>
048615,000010: ## Website: www.ibiblio.org/apollo.
048616,000011: ## Pages: 1140-1148
048617,000012: ## Mod history: 2009-05-28 JVL Updated from page images.
048618,000013: ## 2016-12-17 RSB Proofed text comments with octopus/ProoferComments
048619,000014: ## and corrected the errors found.
048620,000015: ## 2017-03-16 RSB Comment-text fixes identified in 5-way
048621,000016: ## side-by-side diff of Luminary 69/99/116/131/210.
048622,000017:
048623,000018: ## This source code has been transcribed or otherwise adapted from digitized
048624,000019: ## images of a hardcopy from the MIT Museum. The digitization was performed
048625,000020: ## by Paul Fjeld, and arranged for by Deborah Douglas of the Museum. Many
048626,000021: ## thanks to both. The images (with suitable reduction in storage size and
048627,000022: ## consequent reduction in image quality as well) are available online at
048628,000023: ## www.ibiblio.org/apollo. If for some reason you find that the images are
048629,000024: ## illegible, contact me at info@sandroid.org about getting access to the
048630,000025: ## (much) higher-quality images which Paul actually created.
048631,000026: ##
048632,000027: ## Notations on the hardcopy document read, in part:
048633,000028: ##
048634,000029: ## Assemble revision 001 of AGC program LMY99 by NASA 2021112-061
048635,000030: ## 16:27 JULY 14, 1969
048636,000031:
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Page 1140 |
048638,000033: # ..... RP-TO-R SUBROUTINE .....
048639,000034: # SUBROUTINE TO CONVERT RP (VECTOR IN PLANETARY COORDINATE SYSTEM, EITHER
048640,000035: # EARTH-FIXED OR MOON-FIXED) TO R (SAME VECTOR IN THE BASIC REF. SYSTEM)
048641,000036:
048642,000037: # R = MT(T) * (RP + LP X RP) MT = M MATRIX TRANSPOSE
048643,000038:
048644,000039: # CALLING SEQUENCE
048645,000040: # L CALL
048646,000041: # L+1 RP-TO-R
048647,000042:
048648,000043: # SUBROUTINES USED
048649,000044: # EARTHMX, MOONMX, EARTHL
048650,000045:
048651,000046: # ITEMS AVAILABLE FROM LAUNCH DATA
048652,000047: # 504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
048653,000048: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
048654,000049:
048655,000050: # ITEMS NECESSARY FOR SUBR. USED (SEE DESCRIPTION OF SUBR.)
048656,000051:
048657,000052: # INPUT
048658,000053: # MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
048659,000054: # 0-5D = RP VECTOR
048660,000055: # 6-7D = TIME
048661,000056:
048662,000057: # OUTPUT
048663,000058: # MPAC = R VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
048664,000059:
048665,000060: 26,2000 SETLOC PLANTIN1
048666,000061: 26,2000 BANK
048667,000062:
048668,000063: 26,3716 COUNT* $$/LUROT
048669,000064:
048670,000065: 26,3716 46020 RP-TO-R STQ BHIZ
048671,000066: 26,3717 00050 RPREXIT
048672,000067: 26,3720 55733 RPTORA
048673,000068: 26,3721 77624 CALL # COMPUTE M MATRIX FOR MOON
048674,000069: 26,3722 51720 MOONMX # LP=LM FOR MOON RADIANS B0
048675,000070: 26,3723 77775 VLOAD
048676,000071: 26,3724 02013 504LM
048677,000072: 26,3725 53235 RPTORB VXV VAD
048678,000073: 26,3726 00001 504RPR
048679,000074: 26,3727 00001 504RPR
048680,000075: 26,3730 52105 VXM GOTO
048681,000076: 26,3731 00025 MMATRIX # MPAC=R=MT(T)*(RP+LPXRP)
048682,000077: 26,3732 51706 RPRPXXXX # RESET PUSHLOC TO 0 BEFORE EXITING
048683,000078: 26,3733 77624 RPTORA CALL # EARTH COMPUTATIONS
048684,000079: 26,3734 55743 EARTHMX # M MATRIX B-1
048685,000080: 26,3735 77624 CALL
048686,000081: 26,3736 15753 EARTHL # L VECTOR RADIANS B0
048687,000082: 26,3737 76521 MXV VSL1 # LP=M(T)*L RAD B-0
048688,000083: 26,3740 00025 MMATRIX
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Page 1141 |
048690,000085: 26,3741 77650 GOTO
048691,000086: 26,3742 55725 RPTORB
048692,000087: 24,2000 SETLOC PLANTIN
048693,000088: 24,2000 BANK
048694,000089: 24,3670 COUNT* $$/LUROT
048695,000090:
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Page 1142 |
048697,000092: # ..... R-TO-RP SUBROUTINE .....
048698,000093: # SUBROUTINE TO CONVERT R (VECTOR IN REFERENCE COORD. SYSTEM) TO RP
048699,000094: # (VECTOR IN PLANETARY COORD SYSTEM) EITHER EARTH-FIXED OR MOON-FIXED
048700,000095:
048701,000096: # RP = M(T) * (R - L X R)
048702,000097:
048703,000098: # CALLING SEQUENCE
048704,000099: # L CALL
048705,000100: # L+1 R-TO-RP
048706,000101:
048707,000102: # SUBROUTINES USED
048708,000103: # EARTHMX, MOONMX, EARTHL
048709,000104:
048710,000105: # INPUT
048711,000106: # MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
048712,000107: # 0-5D = R VECTOR
048713,000108: # 6-7D = TIME
048714,000109:
048715,000110: # ITEMS AVAILABLE FROM LAUNCH DATA
048716,000111: # 504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
048717,000112: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
048718,000113:
048719,000114: # ITEMS NECESSARY FOR SUBROUTINES USED (SEE DESCRIPTION OF SUBR.)
048720,000115:
048721,000116: # OUTPUT
048722,000117: # MPAC = RP VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
048723,000118:
048724,000119: 24,3670 46020 R-TO-RP STQ BHIZ
048725,000120: 24,3671 00050 RPREXIT
048726,000121: 24,3672 51712 RTORPA
048727,000122: 24,3673 77624 CALL
048728,000123: 24,3674 51720 MOONMX
048729,000124: 24,3675 61375 VLOAD VXM
048730,000125: 24,3676 02013 504LM # LP=LM
048731,000126: 24,3677 00025 MMATRIX
048732,000127: 24,3700 77772 VSL1 # L = MT(T)*LP RADIANS B0
048733,000128: 24,3701 51235 RTORPB VXV BVSU
048734,000129: 24,3702 00001 504RPR
048735,000130: 24,3703 00001 504RPR
048736,000131: 24,3704 77721 MXV # M(T)*(R-LXR) B-2
048737,000132: 24,3705 00025 MMATRIX
048738,000133: 24,3706 40372 RPRPXXXX VSL1 SETPD
048739,000134: 24,3707 00001 0D
048740,000135: 24,3710 77650 GOTO
048741,000136: 24,3711 00050 RPREXIT
048742,000137: 24,3712 77624 RTORPA CALL # EARTH COMPUTATIONS
048743,000138: 24,3713 55743 EARTHMX
048744,000139: 24,3714 77624 CALL
048745,000140: 24,3715 15753 EARTHL
048746,000141: 24,3716 77650 GOTO # MPAC=L=(-AX,-AY,0) RAD B-0
048747,000142: 24,3717 51701 RTORPB
048748,000143:
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Page 1143 |
048750,000145: # ..... MOONMX SUBROUTINE .....
048751,000146: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE MOON
048752,000147:
048753,000148: # CALLING SEQUENCE
048754,000149: # L CALL
048755,000150: # L+1 MOONMX
048756,000151:
048757,000152: # SUBROUTINES USED
048758,000153: # NEWANGLE
048759,000154:
048760,000155: # INPUT
048761,000156: # 6-7D = TIME
048762,000157:
048763,000158: # ITEMS AVAILABLE FROM LAUNCH DATA
048764,000159: # BSUBO, BDOT
048765,000160: # TIMSUBO, NODIO, NODDOT, FSUBO, FDOT
048766,000161: # COSI = COS(I) B-1
048767,000162: # SINI = SIN(I) B-1
048768,000163: # I IS THE ANGLE BETWEEN THE MEAN LUNAR EQUATORIAL PLANE AND THE
048769,000164: # PLANE OF THE ECLIPTIC (1 DEGREE 32.1 MINUTES)
048770,000165:
048771,000166: # OUTPUT
048772,000167: # MMATRIX = 3X3 M MATRIX B-1 (STORED IN VAC AREA)
048773,000168:
048774,000169: 24,3720 40220 MOONMX STQ SETPD
048775,000170: 24,3721 00051 EARTHMXX
048776,000171: 24,3722 00011 8D
048777,000172: 24,3723 77770 AXT,1 # B REQUIRES SL 0, SL 5 IN NEWANGLE
048778,000173: 24,3724 00005 5
048779,000174: 24,3725 65345 DLOAD PDDL # PD 10D 8-9D=BSUBO
048780,000175: 24,3726 14017 BSUBO # 10-11D=BDOT
048781,000176: 24,3727 14011 BDOT
048782,000177: 24,3730 45006 PUSH CALL # PD 12D
048783,000178: 24,3731 53743 NEWANGLE # EXIT WITH PD 8D AND MPAC= B REVS B0
048784,000179: 24,3732 71406 PUSH COS # PD 10D
048785,000180: 24,3733 14041 STODL COB # PD 8D COS(B) B-1
048786,000181: 24,3734 77756 SIN # SIN(B) B-1
048787,000182: 24,3735 14043 STODL SOB # SETUP INPUT FOR NEWANGLE
048788,000183: 24,3736 14015 FSUBO # 8-9D=FSUBO
048789,000184: 24,3737 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=FDOT
048790,000185: 24,3740 14007 FDOT
048791,000186: 24,3741 45170 AXT,1 CALL # F REQUIRES SL 1, SL 6 IN NEWANGLE
048792,000187: 24,3742 00004 4
048793,000188: 24,3743 53743 NEWANGLE # EXIT WITH PD 8D AND MPAC= F REVS B0
048794,000189: 24,3744 14027 STODL AVECTR +2 # SAVE F TEMP
048795,000190: 24,3745 14013 NODIO # 8-9D=NODIO
048796,000191: 24,3746 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=NODDOT
048797,000192: 24,3747 14005 NODDOT # MPAC=T
048798,000193: 24,3750 45170 AXT,1 CALL # NODE REQUIRES SL 0, SL 5 IN NEWANGLE
048799,000194: 24,3751 00005 5
048800,000195: 24,3752 53743 NEWANGLE # EXIT WITH PD 8D AND MPAC= NODI REVS B0
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Page 1144 |
048802,000197: 24,3753 71406 PUSH COS # PD 10D 8-9D= NODI REVS B0
048803,000198: 24,3754 77606 PUSH # PD 12D 10-11D= COS(NODI) B-1
048804,000199: 24,3755 00025 STORE AVECTR
048805,000200: 24,3756 76405 DMP SL1R
048806,000201: 24,3757 00041 COB # COS(NODI) B-1
048807,000202: 24,3760 14035 STODL BVECTR +2 # PD 10D 20-25D=AVECTR= COB*SIN(NODI)
048808,000203: 24,3761 76405 DMP SL1R # SOB*SIN(NODI)
048809,000204: 24,3762 00043 SOB
048810,000205: 24,3763 14037 STODL BVECTR +4 # PD 8D
048811,000206: 24,3764 41556 SIN PUSH # PD 10D -SIN(NODI) B-1
048812,000207: 24,3765 77676 DCOMP # 26-31D=BVECTR= COB*COS(NODI)
048813,000208: 24,3766 14033 STODL BVECTR # PD 8D SOB*COS(NODI)
048814,000209: 24,3767 00027 AVECTR +2 # MOVE F FROM TEMP LOC. TO 504F
048815,000210: 24,3770 14007 STODL 504F
048816,000211: 24,3771 76405 DMP SL1R
048817,000212: 24,3772 00041 COB
048818,000213: 24,3773 77650 GOTO
048819,000214: 24,3774 53671 MOONMXA
048820,000215:
048821,000216: 25,3671 BANK 25
048822,000217: 25,2000 SETLOC PLANTIN3
048823,000218: 25,2000 BANK
048824,000219: 25,3671 COUNT* $$/LUROT
048825,000220:
048826,000221: 25,3671 14027 MOONMXA STODL AVECTR +2
048827,000222: 25,3672 00011 SINNODI # 8-9D=SIN(NODI) B-1
048828,000223: 25,3673 76405 DMP SL1R
048829,000224: 25,3674 00043 SOB
048830,000225: 25,3675 14031 STODL AVECTR +4 # 0
048831,000226: 25,3676 06522 HI6ZEROS # 8-13D= CVECTR= -SOB B-1
048832,000227: 25,3677 57525 PDDL DCOMP # PD 10D COB
048833,000228: 25,3700 00043 SOB
048834,000229: 25,3701 63325 PDDL PDVL # PD 12D THEN PD 14D
048835,000230: 25,3702 00041 COB
048836,000231: 25,3703 00033 BVECTR
048837,000232: 25,3704 63361 VXSC PDVL # PD 20D BVECTR*SINI B-2
048838,000233: 25,3705 14003 SINI
048839,000234: 25,3706 00011 CVECTR
048840,000235: 25,3707 53361 VXSC VAD # PD 14D CVECTR*COSI B-2
048841,000236: 25,3710 14001 COSI
048842,000237: 25,3711 77772 VSL1
048843,000238: 25,3712 24041 STOVL MMATRIX +12D # PD 8D M2=BVECTR*SINI+CVECTR*COSI B-1
048844,000239: 25,3713 63361 VXSC PDVL # PD 14D
048845,000240: 25,3714 14003 SINI # CVECTR*SINI B-2
048846,000241: 25,3715 00033 BVECTR
048847,000242: 25,3716 52361 VXSC VSU # PD 8D BVECTR*COSI B-2
048848,000243: 25,3717 14001 COSI
048849,000244: 25,3720 65372 VSL1 PDDL # PD 14D
048850,000245: 25,3721 00007 504F # 8-13D=DVECTR=BVECTR*COSI-CVECTR*SINI B-1
048851,000246: 25,3722 74346 COS VXSC
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Page 1145 |
048853,000248: 25,3723 00011 DVECTR
048854,000249: 25,3724 73525 PDDL SIN # PD 20D 14-19D= DVECTR*COSF B-2
048855,000250: 25,3725 00007 504F
048856,000251: 25,3726 52361 VXSC VSU # PD 14D AVECTR*SINF B-2
048857,000252: 25,3727 00025 AVECTR
048858,000253: 25,3730 77772 VSL1
048859,000254: 25,3731 14033 STODL MMATRIX +6 # M1= AVECTR*SINF-DVECTR*COSF B-1
048860,000255: 25,3732 00007 504F
048861,000256: 25,3733 74356 SIN VXSC # PD 8D
048862,000257: 25,3734 71525 PDDL COS # PD 14D 8-13D=DVECTR*SINF B-2
048863,000258: 25,3735 00007 504F
048864,000259: 25,3736 53361 VXSC VAD # PD 8D AVECTR*COSF B-2
048865,000260: 25,3737 00025 AVECTR
048866,000261: 25,3740 57572 VSL1 VCOMP
048867,000262: 25,3741 34025 STCALL MMATRIX # M0= -(AVECTR*COSF+DVECTR*SINF) B-1
048868,000263: 25,3742 00051 EARTHMXX
048869,000264:
048870,000265: # COMPUTE X=X0+(XDOT)(T+T0)
048871,000266: # 8-9D= XO (REVS B-0), PUSHLOC SET AT 12D
048872,000267: # 10-11D=XDOT (REVS/CSEC) SCALED B+23 FOR WEARTH,B+28 FOR NODDOT AND BDOT
048873,000268: # AND B+27 FOR FDOT
048874,000269: # X1=DIFFERENCE IN 23 AND SCALING OF XDOT, =0 FOR WEARTH, 5 FOR NODDOT AND
048875,000270: # BDOT AND 4 FOR FDOT
048876,000271: # 6-7D=T (CSEC B-28), TIMSUBO= (CSEC B-42 TRIPLE PREC.)
048877,000272:
048878,000273: 25,3743 54345 NEWANGLE DLOAD SR # ENTER PD 12D
048879,000274: 25,3744 00007 6D
048880,000275: 25,3745 20617 14D
048881,000276: 25,3746 72371 TAD TLOAD # CHANGE MODE TO TP
048882,000277: 25,3747 01707 TIMSUBO
048883,000278: 25,3750 00155 MPAC
048884,000279: 25,3751 14017 STODL TIMSUBM # T+T0 CSEC B-42
048885,000280: 25,3752 00020 TIMSUBM +1
048886,000281: 25,3753 77605 DMP # PD 10D MULT BY XDOT IN 10-11D
048887,000282: 25,3754 43257 SL* DAD # PD 8D ADD XO IN 8-9D AFTER SHIFTING
048888,000283: 25,3755 20206 5,1 # SUCH THAT SCALING IS B-0
048889,000284: 25,3756 67206 PUSH SLOAD # PD 10D SAVE PARTIAL (X0+XDOT*T) IN 8-9D
048890,000285: 25,3757 00017 TIMSUBM
048891,000286: 25,3760 41261 SL DMP
048892,000287: 25,3761 20212 9D
048893,000288: 25,3762 00013 10D # XDOT
048894,000289: 25,3763 43257 SL* DAD # PD 8D SHIFT SUCH THAT THIS PART OF X
048895,000290: 25,3764 20213 10D,1 # IS SCALED REVS/CSEC B-0
048896,000291: 25,3765 77600 BOV # TURN OFF OVERFLOW IF SET BY SHIFT
048897,000292: 25,3766 53767 +1 # INSTRUCTION BEFORE EXITING
048898,000293: 25,3767 77616 RVQ # MPAC=X= X0+(XDOT)(T+T0) REVS B0
048899,000294:
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Page 1146 |
048901,000296: # ..... EARTHMX SUBROUTINE .....
048902,000297: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE EARTH
048903,000298:
048904,000299: # CALLING SEQUENCE
048905,000300: # L CALL
048906,000301: # L+1 EARTHMX
048907,000302:
048908,000303: # SUBROUTINES USED
048909,000304: # NEWANGLE
048910,000305:
048911,000306: # INPUT
048912,000307: # INPUT AVAILABLE FROM LAUNCH DATA AZO REVS B-0
048913,000308: # TEPHEM CSEC B-42
048914,000309: # 6-7D= TIME CSEC B-28
048915,000310:
048916,000311: # OUTPUT
048917,000312: # MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
048918,000313:
048919,000314: 26,3743 BANK 26
048920,000315: 26,2000 SETLOC PLANTIN1
048921,000316: 26,2000 BANK
048922,000317: 26,3743 COUNT* $$/LUROT
048923,000318:
048924,000319: 26,3743 40220 EARTHMX STQ SETPD # SET 8-9D=AZO
048925,000320: 26,3744 00051 EARTHMXX
048926,000321: 26,3745 00011 8D # 10-11D=WEARTH
048927,000322: 26,3746 77770 AXT,1 # FOR SL 5, AND SL 10 IN NEWANGLE
048928,000323: 26,3747 00000 0
048929,000324: 26,3750 65345 DLOAD PDDL # LEAVING PD SET AT 12D FOR NEWANGLE
048930,000325: 26,3751 01712 AZO
048931,000326: 26,3752 14021 WEARTH
048932,000327: 26,3753 45006 PUSH CALL
048933,000328: 26,3754 53743 NEWANGLE
048934,000329: 26,3755 41401 SETPD PUSH # 18-19D=504AZ
048935,000330: 26,3756 00023 18D # COS(AZ) SIN(AZ) 0
048936,000331: 26,3757 65346 COS PDDL # 20-37D= MMATRIX= -SIN(AZ) COS(AZ) 0 B-1
048937,000332: 26,3760 00023 504AZ # 0 0 1
048938,000333: 26,3761 65356 SIN PDDL
048939,000334: 26,3762 06522 HI6ZEROS
048940,000335: 26,3763 73525 PDDL SIN
048941,000336: 26,3764 00023 504AZ
048942,000337: 26,3765 65276 DCOMP PDDL
048943,000338: 26,3766 00023 504AZ
048944,000339: 26,3767 63346 COS PDVL
048945,000340: 26,3770 06522 HI6ZEROS
048946,000341: 26,3771 41525 PDDL PUSH
048947,000342: 26,3772 06520 HIDPHALF
048948,000343: 26,3773 77650 GOTO
048949,000344: 26,3774 00051 EARTHMXX
048950,000345:
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Page 1147 |
048952,000347: # ..... EARTHL SUBROUTINE .....
048953,000348: # SUBROUTINE TO COMPUTE L VECTOR FOR EARTH
048954,000349:
048955,000350: # CALLING SEQUENCE
048956,000351: # L CALL
048957,000352: # L+1 EARTHL
048958,000353:
048959,000354: # INPUT
048960,000355: # AXO,AYO SET AT LAUNCH TIME WITH AYO IMMEDIATELY FOLLOWING AXO IN CORE
048961,000356:
048962,000357: # OUTPUT
048963,000358: # -AX
048964,000359: # MPAC= -AY RADIANS B-0
048965,000360: # 0
048966,000361:
048967,000362: 06,3753 BANK 06
048968,000363: 06,2000 SETLOC EARTHLOC
048969,000364: 06,2000 BANK
048970,000365: 06,3753 COUNT* $$/LUROT
048971,000366:
048972,000367: 06,3753 57545 EARTHL DLOAD DCOMP
048973,000368: 06,3754 01716 AXO
048974,000369: 06,3755 14017 STODL 504LPL
048975,000370: 06,3756 01714 -AYO
048976,000371: 06,3757 14021 STODL 504LPL +2
048977,000372: 06,3760 24007 LO6ZEROS
048978,000373: 06,3761 24023 STOVL 504LPL +4
048979,000374: 06,3762 00017 504LPL
048980,000375: 06,3763 77616 RVQ
048981,000376:
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Page 1148 |
048983,000378: # CONSTANTS AND ERASABLE ASSIGNMENTS
048984,000379:
048985,000380: 06,3764 12,2004 1B1 = DP1/2 # 1 SCALED B-1
048986,000381: 06,3764 0000050 RPREXIT = S1 # R-TO-RP AND RP-TO-R SUBR EXIT
048987,000382: 06,3764 0000051 EARTHMXX = S2 # EARTHMX, MOONMX SUBR. EXITS
048988,000383: 06,3764 504RPR = 0D # 6 REGS R OR RP VECTOR
048989,000384: 06,3764 SINNODI = 8D # 2 SIN(NODI)
048990,000385: 06,3764 DVECTR = 8D # 6 D VECTOR MOON
048991,000386: 06,3764 CVECTR = 8D # 6 C VECTR MOON
048992,000387: 06,3764 504AZ = 18D # 2 AZ
048993,000388: 06,3764 TIMSUBM = 14D # 3 TIME SUB M (MOON) T+T0 IN GETAZ
048994,000389: 06,3764 504LPL = 14D # 6 L OR LP VECTOR
048995,000390: 06,3764 AVECTR = 20D # 6 A VECTOR (MOON)
048996,000391: 06,3764 BVECTR = 26D # 6 B VECTOR (MOON)
048997,000392: 06,3764 MMATRIX = 20D # 18 M MATRIX
048998,000393: 06,3764 COB = 32D # 2 COS(B) B-1
048999,000394: 06,3764 SOB = 34D # 2 SIN(B) B-1
049000,000395: 06,3764 504F = 6D # 2 F(MOON)
049001,000396:
End of include-file PLANETARY_INERTIAL_ORIENTATION.agc. Parent file is MAIN.agc