GAP: ASSEMBLE REVISION 001 OF AGC PROGRAM LMY99 BY NASA 2021112-061 16:27 JULY 14,1969Note that the date is the date of the printout, not the date of the program revision.
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 16:27 JULY 14,1969Note that the date is the date of the printout, not the date of the program revision. |
048644,000002: ## Copyright: Public domain.
048645,000003: ## Filename: PLANETARY_INERTIAL_ORIENTATION.agc
048646,000004: ## Purpose: Part of the source code for Luminary 1A build 099.
048647,000005: ## It is part of the source code for the Lunar Module's (LM)
048648,000006: ## Apollo Guidance Computer (AGC), for Apollo 11.
048649,000007: ##
048650,000008: ## Assembler: yaYUL
048651,000009: ## Contact: Jim Lawton <jim.lawton@gmail.com>
048652,000010: ## Website: www.ibiblio.org/apollo.
048653,000011: ## Pages: 1140-1148
048654,000012: ## Mod history: 2009-05-28 JVL Updated from page images.
048655,000013: ## 2016-12-17 RSB Proofed text comments with octopus/ProoferComments
048656,000014: ## and corrected the errors found.
048657,000015: ## 2017-03-16 RSB Comment-text fixes identified in 5-way
048658,000016: ## side-by-side diff of Luminary 69/99/116/131/210.
048659,000017:
048660,000018: ## This source code has been transcribed or otherwise adapted from digitized
048661,000019: ## images of a hardcopy from the MIT Museum. The digitization was performed
048662,000020: ## by Paul Fjeld, and arranged for by Deborah Douglas of the Museum. Many
048663,000021: ## thanks to both. The images (with suitable reduction in storage size and
048664,000022: ## consequent reduction in image quality as well) are available online at
048665,000023: ## www.ibiblio.org/apollo. If for some reason you find that the images are
048666,000024: ## illegible, contact me at info@sandroid.org about getting access to the
048667,000025: ## (much) higher-quality images which Paul actually created.
048668,000026: ##
048669,000027: ## Notations on the hardcopy document read, in part:
048670,000028: ##
048671,000029: ## Assemble revision 001 of AGC program LMY99 by NASA 2021112-061
048672,000030: ## 16:27 JULY 14, 1969
048673,000031:
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Page 1140 |
048675,000033: # ..... RP-TO-R SUBROUTINE .....
048676,000034: # SUBROUTINE TO CONVERT RP (VECTOR IN PLANETARY COORDINATE SYSTEM, EITHER
048677,000035: # EARTH-FIXED OR MOON-FIXED) TO R (SAME VECTOR IN THE BASIC REF. SYSTEM)
048678,000036:
048679,000037: # R = MT(T) * (RP + LP X RP) MT = M MATRIX TRANSPOSE
048680,000038:
048681,000039: # CALLING SEQUENCE
048682,000040: # L CALL
048683,000041: # L+1 RP-TO-R
048684,000042:
048685,000043: # SUBROUTINES USED
048686,000044: # EARTHMX, MOONMX, EARTHL
048687,000045:
048688,000046: # ITEMS AVAILABLE FROM LAUNCH DATA
048689,000047: # 504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
048690,000048: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
048691,000049:
048692,000050: # ITEMS NECESSARY FOR SUBR. USED (SEE DESCRIPTION OF SUBR.)
048693,000051:
048694,000052: # INPUT
048695,000053: # MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
048696,000054: # 0-5D = RP VECTOR
048697,000055: # 6-7D = TIME
048698,000056:
048699,000057: # OUTPUT
048700,000058: # MPAC = R VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
048701,000059:
048702,000060: 26,2000 SETLOC PLANTIN1
048703,000061: 26,2000 BANK
048704,000062:
048705,000063: 26,3716 COUNT* $$/LUROT
048706,000064:
048707,000065: 26,3716 46020 RP-TO-R STQ BHIZ
048708,000066: 26,3717 00050 RPREXIT
048709,000067: 26,3720 55733 RPTORA
048710,000068: 26,3721 77624 CALL # COMPUTE M MATRIX FOR MOON
048711,000069: 26,3722 51720 MOONMX # LP=LM FOR MOON RADIANS B0
048712,000070: 26,3723 77775 VLOAD
048713,000071: 26,3724 02013 504LM
048714,000072: 26,3725 53235 RPTORB VXV VAD
048715,000073: 26,3726 00001 504RPR
048716,000074: 26,3727 00001 504RPR
048717,000075: 26,3730 52105 VXM GOTO
048718,000076: 26,3731 00025 MMATRIX # MPAC=R=MT(T)*(RP+LPXRP)
048719,000077: 26,3732 51706 RPRPXXXX # RESET PUSHLOC TO 0 BEFORE EXITING
048720,000078: 26,3733 77624 RPTORA CALL # EARTH COMPUTATIONS
048721,000079: 26,3734 55743 EARTHMX # M MATRIX B-1
048722,000080: 26,3735 77624 CALL
048723,000081: 26,3736 15753 EARTHL # L VECTOR RADIANS B0
048724,000082: 26,3737 76521 MXV VSL1 # LP=M(T)*L RAD B-0
048725,000083: 26,3740 00025 MMATRIX
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Page 1141 |
048727,000085: 26,3741 77650 GOTO
048728,000086: 26,3742 55725 RPTORB
048729,000087: 24,2000 SETLOC PLANTIN
048730,000088: 24,2000 BANK
048731,000089: 24,3670 COUNT* $$/LUROT
048732,000090:
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Page 1142 |
048734,000092: # ..... R-TO-RP SUBROUTINE .....
048735,000093: # SUBROUTINE TO CONVERT R (VECTOR IN REFERENCE COORD. SYSTEM) TO RP
048736,000094: # (VECTOR IN PLANETARY COORD SYSTEM) EITHER EARTH-FIXED OR MOON-FIXED
048737,000095:
048738,000096: # RP = M(T) * (R - L X R)
048739,000097:
048740,000098: # CALLING SEQUENCE
048741,000099: # L CALL
048742,000100: # L+1 R-TO-RP
048743,000101:
048744,000102: # SUBROUTINES USED
048745,000103: # EARTHMX, MOONMX, EARTHL
048746,000104:
048747,000105: # INPUT
048748,000106: # MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
048749,000107: # 0-5D = R VECTOR
048750,000108: # 6-7D = TIME
048751,000109:
048752,000110: # ITEMS AVAILABLE FROM LAUNCH DATA
048753,000111: # 504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
048754,000112: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
048755,000113:
048756,000114: # ITEMS NECESSARY FOR SUBROUTINES USED (SEE DESCRIPTION OF SUBR.)
048757,000115:
048758,000116: # OUTPUT
048759,000117: # MPAC = RP VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
048760,000118:
048761,000119: 24,3670 46020 R-TO-RP STQ BHIZ
048762,000120: 24,3671 00050 RPREXIT
048763,000121: 24,3672 51712 RTORPA
048764,000122: 24,3673 77624 CALL
048765,000123: 24,3674 51720 MOONMX
048766,000124: 24,3675 61375 VLOAD VXM
048767,000125: 24,3676 02013 504LM # LP=LM
048768,000126: 24,3677 00025 MMATRIX
048769,000127: 24,3700 77772 VSL1 # L = MT(T)*LP RADIANS B0
048770,000128: 24,3701 51235 RTORPB VXV BVSU
048771,000129: 24,3702 00001 504RPR
048772,000130: 24,3703 00001 504RPR
048773,000131: 24,3704 77721 MXV # M(T)*(R-LXR) B-2
048774,000132: 24,3705 00025 MMATRIX
048775,000133: 24,3706 40372 RPRPXXXX VSL1 SETPD
048776,000134: 24,3707 00001 0D
048777,000135: 24,3710 77650 GOTO
048778,000136: 24,3711 00050 RPREXIT
048779,000137: 24,3712 77624 RTORPA CALL # EARTH COMPUTATIONS
048780,000138: 24,3713 55743 EARTHMX
048781,000139: 24,3714 77624 CALL
048782,000140: 24,3715 15753 EARTHL
048783,000141: 24,3716 77650 GOTO # MPAC=L=(-AX,-AY,0) RAD B-0
048784,000142: 24,3717 51701 RTORPB
048785,000143:
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Page 1143 |
048787,000145: # ..... MOONMX SUBROUTINE .....
048788,000146: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE MOON
048789,000147:
048790,000148: # CALLING SEQUENCE
048791,000149: # L CALL
048792,000150: # L+1 MOONMX
048793,000151:
048794,000152: # SUBROUTINES USED
048795,000153: # NEWANGLE
048796,000154:
048797,000155: # INPUT
048798,000156: # 6-7D = TIME
048799,000157:
048800,000158: # ITEMS AVAILABLE FROM LAUNCH DATA
048801,000159: # BSUBO, BDOT
048802,000160: # TIMSUBO, NODIO, NODDOT, FSUBO, FDOT
048803,000161: # COSI = COS(I) B-1
048804,000162: # SINI = SIN(I) B-1
048805,000163: # I IS THE ANGLE BETWEEN THE MEAN LUNAR EQUATORIAL PLANE AND THE
048806,000164: # PLANE OF THE ECLIPTIC (1 DEGREE 32.1 MINUTES)
048807,000165:
048808,000166: # OUTPUT
048809,000167: # MMATRIX = 3X3 M MATRIX B-1 (STORED IN VAC AREA)
048810,000168:
048811,000169: 24,3720 40220 MOONMX STQ SETPD
048812,000170: 24,3721 00051 EARTHMXX
048813,000171: 24,3722 00011 8D
048814,000172: 24,3723 77770 AXT,1 # B REQUIRES SL 0, SL 5 IN NEWANGLE
048815,000173: 24,3724 00005 5
048816,000174: 24,3725 65345 DLOAD PDDL # PD 10D 8-9D=BSUBO
048817,000175: 24,3726 14017 BSUBO # 10-11D=BDOT
048818,000176: 24,3727 14011 BDOT
048819,000177: 24,3730 45006 PUSH CALL # PD 12D
048820,000178: 24,3731 53743 NEWANGLE # EXIT WITH PD 8D AND MPAC= B REVS B0
048821,000179: 24,3732 71406 PUSH COS # PD 10D
048822,000180: 24,3733 14041 STODL COB # PD 8D COS(B) B-1
048823,000181: 24,3734 77756 SIN # SIN(B) B-1
048824,000182: 24,3735 14043 STODL SOB # SETUP INPUT FOR NEWANGLE
048825,000183: 24,3736 14015 FSUBO # 8-9D=FSUBO
048826,000184: 24,3737 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=FDOT
048827,000185: 24,3740 14007 FDOT
048828,000186: 24,3741 45170 AXT,1 CALL # F REQUIRES SL 1, SL 6 IN NEWANGLE
048829,000187: 24,3742 00004 4
048830,000188: 24,3743 53743 NEWANGLE # EXIT WITH PD 8D AND MPAC= F REVS B0
048831,000189: 24,3744 14027 STODL AVECTR +2 # SAVE F TEMP
048832,000190: 24,3745 14013 NODIO # 8-9D=NODIO
048833,000191: 24,3746 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=NODDOT
048834,000192: 24,3747 14005 NODDOT # MPAC=T
048835,000193: 24,3750 45170 AXT,1 CALL # NODE REQUIRES SL 0, SL 5 IN NEWANGLE
048836,000194: 24,3751 00005 5
048837,000195: 24,3752 53743 NEWANGLE # EXIT WITH PD 8D AND MPAC= NODI REVS B0
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Page 1144 |
048839,000197: 24,3753 71406 PUSH COS # PD 10D 8-9D= NODI REVS B0
048840,000198: 24,3754 77606 PUSH # PD 12D 10-11D= COS(NODI) B-1
048841,000199: 24,3755 00025 STORE AVECTR
048842,000200: 24,3756 76405 DMP SL1R
048843,000201: 24,3757 00041 COB # COS(NODI) B-1
048844,000202: 24,3760 14035 STODL BVECTR +2 # PD 10D 20-25D=AVECTR= COB*SIN(NODI)
048845,000203: 24,3761 76405 DMP SL1R # SOB*SIN(NODI)
048846,000204: 24,3762 00043 SOB
048847,000205: 24,3763 14037 STODL BVECTR +4 # PD 8D
048848,000206: 24,3764 41556 SIN PUSH # PD 10D -SIN(NODI) B-1
048849,000207: 24,3765 77676 DCOMP # 26-31D=BVECTR= COB*COS(NODI)
048850,000208: 24,3766 14033 STODL BVECTR # PD 8D SOB*COS(NODI)
048851,000209: 24,3767 00027 AVECTR +2 # MOVE F FROM TEMP LOC. TO 504F
048852,000210: 24,3770 14007 STODL 504F
048853,000211: 24,3771 76405 DMP SL1R
048854,000212: 24,3772 00041 COB
048855,000213: 24,3773 77650 GOTO
048856,000214: 24,3774 53671 MOONMXA
048857,000215:
048858,000216: 25,3671 BANK 25
048859,000217: 25,2000 SETLOC PLANTIN3
048860,000218: 25,2000 BANK
048861,000219: 25,3671 COUNT* $$/LUROT
048862,000220:
048863,000221: 25,3671 14027 MOONMXA STODL AVECTR +2
048864,000222: 25,3672 00011 SINNODI # 8-9D=SIN(NODI) B-1
048865,000223: 25,3673 76405 DMP SL1R
048866,000224: 25,3674 00043 SOB
048867,000225: 25,3675 14031 STODL AVECTR +4 # 0
048868,000226: 25,3676 06522 HI6ZEROS # 8-13D= CVECTR= -SOB B-1
048869,000227: 25,3677 57525 PDDL DCOMP # PD 10D COB
048870,000228: 25,3700 00043 SOB
048871,000229: 25,3701 63325 PDDL PDVL # PD 12D THEN PD 14D
048872,000230: 25,3702 00041 COB
048873,000231: 25,3703 00033 BVECTR
048874,000232: 25,3704 63361 VXSC PDVL # PD 20D BVECTR*SINI B-2
048875,000233: 25,3705 14003 SINI
048876,000234: 25,3706 00011 CVECTR
048877,000235: 25,3707 53361 VXSC VAD # PD 14D CVECTR*COSI B-2
048878,000236: 25,3710 14001 COSI
048879,000237: 25,3711 77772 VSL1
048880,000238: 25,3712 24041 STOVL MMATRIX +12D # PD 8D M2=BVECTR*SINI+CVECTR*COSI B-1
048881,000239: 25,3713 63361 VXSC PDVL # PD 14D
048882,000240: 25,3714 14003 SINI # CVECTR*SINI B-2
048883,000241: 25,3715 00033 BVECTR
048884,000242: 25,3716 52361 VXSC VSU # PD 8D BVECTR*COSI B-2
048885,000243: 25,3717 14001 COSI
048886,000244: 25,3720 65372 VSL1 PDDL # PD 14D
048887,000245: 25,3721 00007 504F # 8-13D=DVECTR=BVECTR*COSI-CVECTR*SINI B-1
048888,000246: 25,3722 74346 COS VXSC
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Page 1145 |
048890,000248: 25,3723 00011 DVECTR
048891,000249: 25,3724 73525 PDDL SIN # PD 20D 14-19D= DVECTR*COSF B-2
048892,000250: 25,3725 00007 504F
048893,000251: 25,3726 52361 VXSC VSU # PD 14D AVECTR*SINF B-2
048894,000252: 25,3727 00025 AVECTR
048895,000253: 25,3730 77772 VSL1
048896,000254: 25,3731 14033 STODL MMATRIX +6 # M1= AVECTR*SINF-DVECTR*COSF B-1
048897,000255: 25,3732 00007 504F
048898,000256: 25,3733 74356 SIN VXSC # PD 8D
048899,000257: 25,3734 71525 PDDL COS # PD 14D 8-13D=DVECTR*SINF B-2
048900,000258: 25,3735 00007 504F
048901,000259: 25,3736 53361 VXSC VAD # PD 8D AVECTR*COSF B-2
048902,000260: 25,3737 00025 AVECTR
048903,000261: 25,3740 57572 VSL1 VCOMP
048904,000262: 25,3741 34025 STCALL MMATRIX # M0= -(AVECTR*COSF+DVECTR*SINF) B-1
048905,000263: 25,3742 00051 EARTHMXX
048906,000264:
048907,000265: # COMPUTE X=X0+(XDOT)(T+T0)
048908,000266: # 8-9D= XO (REVS B-0), PUSHLOC SET AT 12D
048909,000267: # 10-11D=XDOT (REVS/CSEC) SCALED B+23 FOR WEARTH,B+28 FOR NODDOT AND BDOT
048910,000268: # AND B+27 FOR FDOT
048911,000269: # X1=DIFFERENCE IN 23 AND SCALING OF XDOT, =0 FOR WEARTH, 5 FOR NODDOT AND
048912,000270: # BDOT AND 4 FOR FDOT
048913,000271: # 6-7D=T (CSEC B-28), TIMSUBO= (CSEC B-42 TRIPLE PREC.)
048914,000272:
048915,000273: 25,3743 54345 NEWANGLE DLOAD SR # ENTER PD 12D
048916,000274: 25,3744 00007 6D
048917,000275: 25,3745 20617 14D
048918,000276: 25,3746 72371 TAD TLOAD # CHANGE MODE TO TP
048919,000277: 25,3747 01707 TIMSUBO
048920,000278: 25,3750 00155 MPAC
048921,000279: 25,3751 14017 STODL TIMSUBM # T+T0 CSEC B-42
048922,000280: 25,3752 00020 TIMSUBM +1
048923,000281: 25,3753 77605 DMP # PD 10D MULT BY XDOT IN 10-11D
048924,000282: 25,3754 43257 SL* DAD # PD 8D ADD XO IN 8-9D AFTER SHIFTING
048925,000283: 25,3755 20206 5,1 # SUCH THAT SCALING IS B-0
048926,000284: 25,3756 67206 PUSH SLOAD # PD 10D SAVE PARTIAL (X0+XDOT*T) IN 8-9D
048927,000285: 25,3757 00017 TIMSUBM
048928,000286: 25,3760 41261 SL DMP
048929,000287: 25,3761 20212 9D
048930,000288: 25,3762 00013 10D # XDOT
048931,000289: 25,3763 43257 SL* DAD # PD 8D SHIFT SUCH THAT THIS PART OF X
048932,000290: 25,3764 20213 10D,1 # IS SCALED REVS/CSEC B-0
048933,000291: 25,3765 77600 BOV # TURN OFF OVERFLOW IF SET BY SHIFT
048934,000292: 25,3766 53767 +1 # INSTRUCTION BEFORE EXITING
048935,000293: 25,3767 77616 RVQ # MPAC=X= X0+(XDOT)(T+T0) REVS B0
048936,000294:
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Page 1146 |
048938,000296: # ..... EARTHMX SUBROUTINE .....
048939,000297: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE EARTH
048940,000298:
048941,000299: # CALLING SEQUENCE
048942,000300: # L CALL
048943,000301: # L+1 EARTHMX
048944,000302:
048945,000303: # SUBROUTINES USED
048946,000304: # NEWANGLE
048947,000305:
048948,000306: # INPUT
048949,000307: # INPUT AVAILABLE FROM LAUNCH DATA AZO REVS B-0
048950,000308: # TEPHEM CSEC B-42
048951,000309: # 6-7D= TIME CSEC B-28
048952,000310:
048953,000311: # OUTPUT
048954,000312: # MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
048955,000313:
048956,000314: 26,3743 BANK 26
048957,000315: 26,2000 SETLOC PLANTIN1
048958,000316: 26,2000 BANK
048959,000317: 26,3743 COUNT* $$/LUROT
048960,000318:
048961,000319: 26,3743 40220 EARTHMX STQ SETPD # SET 8-9D=AZO
048962,000320: 26,3744 00051 EARTHMXX
048963,000321: 26,3745 00011 8D # 10-11D=WEARTH
048964,000322: 26,3746 77770 AXT,1 # FOR SL 5, AND SL 10 IN NEWANGLE
048965,000323: 26,3747 00000 0
048966,000324: 26,3750 65345 DLOAD PDDL # LEAVING PD SET AT 12D FOR NEWANGLE
048967,000325: 26,3751 01712 AZO
048968,000326: 26,3752 14021 WEARTH
048969,000327: 26,3753 45006 PUSH CALL
048970,000328: 26,3754 53743 NEWANGLE
048971,000329: 26,3755 41401 SETPD PUSH # 18-19D=504AZ
048972,000330: 26,3756 00023 18D # COS(AZ) SIN(AZ) 0
048973,000331: 26,3757 65346 COS PDDL # 20-37D= MMATRIX= -SIN(AZ) COS(AZ) 0 B-1
048974,000332: 26,3760 00023 504AZ # 0 0 1
048975,000333: 26,3761 65356 SIN PDDL
048976,000334: 26,3762 06522 HI6ZEROS
048977,000335: 26,3763 73525 PDDL SIN
048978,000336: 26,3764 00023 504AZ
048979,000337: 26,3765 65276 DCOMP PDDL
048980,000338: 26,3766 00023 504AZ
048981,000339: 26,3767 63346 COS PDVL
048982,000340: 26,3770 06522 HI6ZEROS
048983,000341: 26,3771 41525 PDDL PUSH
048984,000342: 26,3772 06520 HIDPHALF
048985,000343: 26,3773 77650 GOTO
048986,000344: 26,3774 00051 EARTHMXX
048987,000345:
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Page 1147 |
048989,000347: # ..... EARTHL SUBROUTINE .....
048990,000348: # SUBROUTINE TO COMPUTE L VECTOR FOR EARTH
048991,000349:
048992,000350: # CALLING SEQUENCE
048993,000351: # L CALL
048994,000352: # L+1 EARTHL
048995,000353:
048996,000354: # INPUT
048997,000355: # AXO,AYO SET AT LAUNCH TIME WITH AYO IMMEDIATELY FOLLOWING AXO IN CORE
048998,000356:
048999,000357: # OUTPUT
049000,000358: # -AX
049001,000359: # MPAC= -AY RADIANS B-0
049002,000360: # 0
049003,000361:
049004,000362: 06,3753 BANK 06
049005,000363: 06,2000 SETLOC EARTHLOC
049006,000364: 06,2000 BANK
049007,000365: 06,3753 COUNT* $$/LUROT
049008,000366:
049009,000367: 06,3753 57545 EARTHL DLOAD DCOMP
049010,000368: 06,3754 01716 AXO
049011,000369: 06,3755 14017 STODL 504LPL
049012,000370: 06,3756 01714 -AYO
049013,000371: 06,3757 14021 STODL 504LPL +2
049014,000372: 06,3760 24007 LO6ZEROS
049015,000373: 06,3761 24023 STOVL 504LPL +4
049016,000374: 06,3762 00017 504LPL
049017,000375: 06,3763 77616 RVQ
049018,000376:
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Page 1148 |
049020,000378: # CONSTANTS AND ERASABLE ASSIGNMENTS
049021,000379:
049022,000380: 06,3764 12,2004 1B1 = DP1/2 # 1 SCALED B-1
049023,000381: 06,3764 0000050 RPREXIT = S1 # R-TO-RP AND RP-TO-R SUBR EXIT
049024,000382: 06,3764 0000051 EARTHMXX = S2 # EARTHMX, MOONMX SUBR. EXITS
049025,000383: 06,3764 504RPR = 0D # 6 REGS R OR RP VECTOR
049026,000384: 06,3764 SINNODI = 8D # 2 SIN(NODI)
049027,000385: 06,3764 DVECTR = 8D # 6 D VECTOR MOON
049028,000386: 06,3764 CVECTR = 8D # 6 C VECTR MOON
049029,000387: 06,3764 504AZ = 18D # 2 AZ
049030,000388: 06,3764 TIMSUBM = 14D # 3 TIME SUB M (MOON) T+T0 IN GETAZ
049031,000389: 06,3764 504LPL = 14D # 6 L OR LP VECTOR
049032,000390: 06,3764 AVECTR = 20D # 6 A VECTOR (MOON)
049033,000391: 06,3764 BVECTR = 26D # 6 B VECTOR (MOON)
049034,000392: 06,3764 MMATRIX = 20D # 18 M MATRIX
049035,000393: 06,3764 COB = 32D # 2 COS(B) B-1
049036,000394: 06,3764 SOB = 34D # 2 SIN(B) B-1
049037,000395: 06,3764 504F = 6D # 2 F(MOON)
049038,000396:
End of include-file PLANETARY_INERTIAL_ORIENTATION.agc. Parent file is MAIN.agc