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. |
048642,000002: ## Copyright: Public domain.
048643,000003: ## Filename: PLANETARY_INERTIAL_ORIENTATION.agc
048644,000004: ## Purpose: Part of the source code for Luminary 1A build 099.
048645,000005: ## It is part of the source code for the Lunar Module's (LM)
048646,000006: ## Apollo Guidance Computer (AGC), for Apollo 11.
048647,000007: ##
048648,000008: ## Assembler: yaYUL
048649,000009: ## Contact: Jim Lawton <jim.lawton@gmail.com>
048650,000010: ## Website: www.ibiblio.org/apollo.
048651,000011: ## Pages: 1140-1148
048652,000012: ## Mod history: 2009-05-28 JVL Updated from page images.
048653,000013: ## 2016-12-17 RSB Proofed text comments with octopus/ProoferComments
048654,000014: ## and corrected the errors found.
048655,000015: ## 2017-03-16 RSB Comment-text fixes identified in 5-way
048656,000016: ## side-by-side diff of Luminary 69/99/116/131/210.
048657,000017:
048658,000018: ## This source code has been transcribed or otherwise adapted from digitized
048659,000019: ## images of a hardcopy from the MIT Museum. The digitization was performed
048660,000020: ## by Paul Fjeld, and arranged for by Deborah Douglas of the Museum. Many
048661,000021: ## thanks to both. The images (with suitable reduction in storage size and
048662,000022: ## consequent reduction in image quality as well) are available online at
048663,000023: ## www.ibiblio.org/apollo. If for some reason you find that the images are
048664,000024: ## illegible, contact me at info@sandroid.org about getting access to the
048665,000025: ## (much) higher-quality images which Paul actually created.
048666,000026: ##
048667,000027: ## Notations on the hardcopy document read, in part:
048668,000028: ##
048669,000029: ## Assemble revision 001 of AGC program LMY99 by NASA 2021112-061
048670,000030: ## 16:27 JULY 14, 1969
048671,000031:
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Page 1140 |
048673,000033: # ..... RP-TO-R SUBROUTINE .....
048674,000034: # SUBROUTINE TO CONVERT RP (VECTOR IN PLANETARY COORDINATE SYSTEM, EITHER
048675,000035: # EARTH-FIXED OR MOON-FIXED) TO R (SAME VECTOR IN THE BASIC REF. SYSTEM)
048676,000036:
048677,000037: # R = MT(T) * (RP + LP X RP) MT = M MATRIX TRANSPOSE
048678,000038:
048679,000039: # CALLING SEQUENCE
048680,000040: # L CALL
048681,000041: # L+1 RP-TO-R
048682,000042:
048683,000043: # SUBROUTINES USED
048684,000044: # EARTHMX, MOONMX, EARTHL
048685,000045:
048686,000046: # ITEMS AVAILABLE FROM LAUNCH DATA
048687,000047: # 504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
048688,000048: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
048689,000049:
048690,000050: # ITEMS NECESSARY FOR SUBR. USED (SEE DESCRIPTION OF SUBR.)
048691,000051:
048692,000052: # INPUT
048693,000053: # MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
048694,000054: # 0-5D = RP VECTOR
048695,000055: # 6-7D = TIME
048696,000056:
048697,000057: # OUTPUT
048698,000058: # MPAC = R VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
048699,000059:
048700,000060: 26,2000 SETLOC PLANTIN1
048701,000061: 26,2000 BANK
048702,000062:
048703,000063: 26,3716 COUNT* $$/LUROT
048704,000064:
048705,000065: 26,3716 46020 RP-TO-R STQ BHIZ
048706,000066: 26,3717 00050 RPREXIT
048707,000067: 26,3720 55733 RPTORA
048708,000068: 26,3721 77624 CALL # COMPUTE M MATRIX FOR MOON
048709,000069: 26,3722 51720 MOONMX # LP=LM FOR MOON RADIANS B0
048710,000070: 26,3723 77775 VLOAD
048711,000071: 26,3724 02013 504LM
048712,000072: 26,3725 53235 RPTORB VXV VAD
048713,000073: 26,3726 00001 504RPR
048714,000074: 26,3727 00001 504RPR
048715,000075: 26,3730 52105 VXM GOTO
048716,000076: 26,3731 00025 MMATRIX # MPAC=R=MT(T)*(RP+LPXRP)
048717,000077: 26,3732 51706 RPRPXXXX # RESET PUSHLOC TO 0 BEFORE EXITING
048718,000078: 26,3733 77624 RPTORA CALL # EARTH COMPUTATIONS
048719,000079: 26,3734 55743 EARTHMX # M MATRIX B-1
048720,000080: 26,3735 77624 CALL
048721,000081: 26,3736 15753 EARTHL # L VECTOR RADIANS B0
048722,000082: 26,3737 76521 MXV VSL1 # LP=M(T)*L RAD B-0
048723,000083: 26,3740 00025 MMATRIX
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Page 1141 |
048725,000085: 26,3741 77650 GOTO
048726,000086: 26,3742 55725 RPTORB
048727,000087: 24,2000 SETLOC PLANTIN
048728,000088: 24,2000 BANK
048729,000089: 24,3670 COUNT* $$/LUROT
048730,000090:
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Page 1142 |
048732,000092: # ..... R-TO-RP SUBROUTINE .....
048733,000093: # SUBROUTINE TO CONVERT R (VECTOR IN REFERENCE COORD. SYSTEM) TO RP
048734,000094: # (VECTOR IN PLANETARY COORD SYSTEM) EITHER EARTH-FIXED OR MOON-FIXED
048735,000095:
048736,000096: # RP = M(T) * (R - L X R)
048737,000097:
048738,000098: # CALLING SEQUENCE
048739,000099: # L CALL
048740,000100: # L+1 R-TO-RP
048741,000101:
048742,000102: # SUBROUTINES USED
048743,000103: # EARTHMX, MOONMX, EARTHL
048744,000104:
048745,000105: # INPUT
048746,000106: # MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
048747,000107: # 0-5D = R VECTOR
048748,000108: # 6-7D = TIME
048749,000109:
048750,000110: # ITEMS AVAILABLE FROM LAUNCH DATA
048751,000111: # 504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
048752,000112: # IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
048753,000113:
048754,000114: # ITEMS NECESSARY FOR SUBROUTINES USED (SEE DESCRIPTION OF SUBR.)
048755,000115:
048756,000116: # OUTPUT
048757,000117: # MPAC = RP VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
048758,000118:
048759,000119: 24,3670 46020 R-TO-RP STQ BHIZ
048760,000120: 24,3671 00050 RPREXIT
048761,000121: 24,3672 51712 RTORPA
048762,000122: 24,3673 77624 CALL
048763,000123: 24,3674 51720 MOONMX
048764,000124: 24,3675 61375 VLOAD VXM
048765,000125: 24,3676 02013 504LM # LP=LM
048766,000126: 24,3677 00025 MMATRIX
048767,000127: 24,3700 77772 VSL1 # L = MT(T)*LP RADIANS B0
048768,000128: 24,3701 51235 RTORPB VXV BVSU
048769,000129: 24,3702 00001 504RPR
048770,000130: 24,3703 00001 504RPR
048771,000131: 24,3704 77721 MXV # M(T)*(R-LXR) B-2
048772,000132: 24,3705 00025 MMATRIX
048773,000133: 24,3706 40372 RPRPXXXX VSL1 SETPD
048774,000134: 24,3707 00001 0D
048775,000135: 24,3710 77650 GOTO
048776,000136: 24,3711 00050 RPREXIT
048777,000137: 24,3712 77624 RTORPA CALL # EARTH COMPUTATIONS
048778,000138: 24,3713 55743 EARTHMX
048779,000139: 24,3714 77624 CALL
048780,000140: 24,3715 15753 EARTHL
048781,000141: 24,3716 77650 GOTO # MPAC=L=(-AX,-AY,0) RAD B-0
048782,000142: 24,3717 51701 RTORPB
048783,000143:
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Page 1143 |
048785,000145: # ..... MOONMX SUBROUTINE .....
048786,000146: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE MOON
048787,000147:
048788,000148: # CALLING SEQUENCE
048789,000149: # L CALL
048790,000150: # L+1 MOONMX
048791,000151:
048792,000152: # SUBROUTINES USED
048793,000153: # NEWANGLE
048794,000154:
048795,000155: # INPUT
048796,000156: # 6-7D = TIME
048797,000157:
048798,000158: # ITEMS AVAILABLE FROM LAUNCH DATA
048799,000159: # BSUBO, BDOT
048800,000160: # TIMSUBO, NODIO, NODDOT, FSUBO, FDOT
048801,000161: # COSI = COS(I) B-1
048802,000162: # SINI = SIN(I) B-1
048803,000163: # I IS THE ANGLE BETWEEN THE MEAN LUNAR EQUATORIAL PLANE AND THE
048804,000164: # PLANE OF THE ECLIPTIC (1 DEGREE 32.1 MINUTES)
048805,000165:
048806,000166: # OUTPUT
048807,000167: # MMATRIX = 3X3 M MATRIX B-1 (STORED IN VAC AREA)
048808,000168:
048809,000169: 24,3720 40220 MOONMX STQ SETPD
048810,000170: 24,3721 00051 EARTHMXX
048811,000171: 24,3722 00011 8D
048812,000172: 24,3723 77770 AXT,1 # B REQUIRES SL 0, SL 5 IN NEWANGLE
048813,000173: 24,3724 00005 5
048814,000174: 24,3725 65345 DLOAD PDDL # PD 10D 8-9D=BSUBO
048815,000175: 24,3726 14017 BSUBO # 10-11D=BDOT
048816,000176: 24,3727 14011 BDOT
048817,000177: 24,3730 45006 PUSH CALL # PD 12D
048818,000178: 24,3731 53743 NEWANGLE # EXIT WITH PD 8D AND MPAC= B REVS B0
048819,000179: 24,3732 71406 PUSH COS # PD 10D
048820,000180: 24,3733 14041 STODL COB # PD 8D COS(B) B-1
048821,000181: 24,3734 77756 SIN # SIN(B) B-1
048822,000182: 24,3735 14043 STODL SOB # SETUP INPUT FOR NEWANGLE
048823,000183: 24,3736 14015 FSUBO # 8-9D=FSUBO
048824,000184: 24,3737 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=FDOT
048825,000185: 24,3740 14007 FDOT
048826,000186: 24,3741 45170 AXT,1 CALL # F REQUIRES SL 1, SL 6 IN NEWANGLE
048827,000187: 24,3742 00004 4
048828,000188: 24,3743 53743 NEWANGLE # EXIT WITH PD 8D AND MPAC= F REVS B0
048829,000189: 24,3744 14027 STODL AVECTR +2 # SAVE F TEMP
048830,000190: 24,3745 14013 NODIO # 8-9D=NODIO
048831,000191: 24,3746 41525 PDDL PUSH # PD 10D THEN 12D 10-11D=NODDOT
048832,000192: 24,3747 14005 NODDOT # MPAC=T
048833,000193: 24,3750 45170 AXT,1 CALL # NODE REQUIRES SL 0, SL 5 IN NEWANGLE
048834,000194: 24,3751 00005 5
048835,000195: 24,3752 53743 NEWANGLE # EXIT WITH PD 8D AND MPAC= NODI REVS B0
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Page 1144 |
048837,000197: 24,3753 71406 PUSH COS # PD 10D 8-9D= NODI REVS B0
048838,000198: 24,3754 77606 PUSH # PD 12D 10-11D= COS(NODI) B-1
048839,000199: 24,3755 00025 STORE AVECTR
048840,000200: 24,3756 76405 DMP SL1R
048841,000201: 24,3757 00041 COB # COS(NODI) B-1
048842,000202: 24,3760 14035 STODL BVECTR +2 # PD 10D 20-25D=AVECTR= COB*SIN(NODI)
048843,000203: 24,3761 76405 DMP SL1R # SOB*SIN(NODI)
048844,000204: 24,3762 00043 SOB
048845,000205: 24,3763 14037 STODL BVECTR +4 # PD 8D
048846,000206: 24,3764 41556 SIN PUSH # PD 10D -SIN(NODI) B-1
048847,000207: 24,3765 77676 DCOMP # 26-31D=BVECTR= COB*COS(NODI)
048848,000208: 24,3766 14033 STODL BVECTR # PD 8D SOB*COS(NODI)
048849,000209: 24,3767 00027 AVECTR +2 # MOVE F FROM TEMP LOC. TO 504F
048850,000210: 24,3770 14007 STODL 504F
048851,000211: 24,3771 76405 DMP SL1R
048852,000212: 24,3772 00041 COB
048853,000213: 24,3773 77650 GOTO
048854,000214: 24,3774 53671 MOONMXA
048855,000215:
048856,000216: 25,3671 BANK 25
048857,000217: 25,2000 SETLOC PLANTIN3
048858,000218: 25,2000 BANK
048859,000219: 25,3671 COUNT* $$/LUROT
048860,000220:
048861,000221: 25,3671 14027 MOONMXA STODL AVECTR +2
048862,000222: 25,3672 00011 SINNODI # 8-9D=SIN(NODI) B-1
048863,000223: 25,3673 76405 DMP SL1R
048864,000224: 25,3674 00043 SOB
048865,000225: 25,3675 14031 STODL AVECTR +4 # 0
048866,000226: 25,3676 06522 HI6ZEROS # 8-13D= CVECTR= -SOB B-1
048867,000227: 25,3677 57525 PDDL DCOMP # PD 10D COB
048868,000228: 25,3700 00043 SOB
048869,000229: 25,3701 63325 PDDL PDVL # PD 12D THEN PD 14D
048870,000230: 25,3702 00041 COB
048871,000231: 25,3703 00033 BVECTR
048872,000232: 25,3704 63361 VXSC PDVL # PD 20D BVECTR*SINI B-2
048873,000233: 25,3705 14003 SINI
048874,000234: 25,3706 00011 CVECTR
048875,000235: 25,3707 53361 VXSC VAD # PD 14D CVECTR*COSI B-2
048876,000236: 25,3710 14001 COSI
048877,000237: 25,3711 77772 VSL1
048878,000238: 25,3712 24041 STOVL MMATRIX +12D # PD 8D M2=BVECTR*SINI+CVECTR*COSI B-1
048879,000239: 25,3713 63361 VXSC PDVL # PD 14D
048880,000240: 25,3714 14003 SINI # CVECTR*SINI B-2
048881,000241: 25,3715 00033 BVECTR
048882,000242: 25,3716 52361 VXSC VSU # PD 8D BVECTR*COSI B-2
048883,000243: 25,3717 14001 COSI
048884,000244: 25,3720 65372 VSL1 PDDL # PD 14D
048885,000245: 25,3721 00007 504F # 8-13D=DVECTR=BVECTR*COSI-CVECTR*SINI B-1
048886,000246: 25,3722 74346 COS VXSC
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Page 1145 |
048888,000248: 25,3723 00011 DVECTR
048889,000249: 25,3724 73525 PDDL SIN # PD 20D 14-19D= DVECTR*COSF B-2
048890,000250: 25,3725 00007 504F
048891,000251: 25,3726 52361 VXSC VSU # PD 14D AVECTR*SINF B-2
048892,000252: 25,3727 00025 AVECTR
048893,000253: 25,3730 77772 VSL1
048894,000254: 25,3731 14033 STODL MMATRIX +6 # M1= AVECTR*SINF-DVECTR*COSF B-1
048895,000255: 25,3732 00007 504F
048896,000256: 25,3733 74356 SIN VXSC # PD 8D
048897,000257: 25,3734 71525 PDDL COS # PD 14D 8-13D=DVECTR*SINF B-2
048898,000258: 25,3735 00007 504F
048899,000259: 25,3736 53361 VXSC VAD # PD 8D AVECTR*COSF B-2
048900,000260: 25,3737 00025 AVECTR
048901,000261: 25,3740 57572 VSL1 VCOMP
048902,000262: 25,3741 34025 STCALL MMATRIX # M0= -(AVECTR*COSF+DVECTR*SINF) B-1
048903,000263: 25,3742 00051 EARTHMXX
048904,000264:
048905,000265: # COMPUTE X=X0+(XDOT)(T+T0)
048906,000266: # 8-9D= XO (REVS B-0), PUSHLOC SET AT 12D
048907,000267: # 10-11D=XDOT (REVS/CSEC) SCALED B+23 FOR WEARTH,B+28 FOR NODDOT AND BDOT
048908,000268: # AND B+27 FOR FDOT
048909,000269: # X1=DIFFERENCE IN 23 AND SCALING OF XDOT, =0 FOR WEARTH, 5 FOR NODDOT AND
048910,000270: # BDOT AND 4 FOR FDOT
048911,000271: # 6-7D=T (CSEC B-28), TIMSUBO= (CSEC B-42 TRIPLE PREC.)
048912,000272:
048913,000273: 25,3743 54345 NEWANGLE DLOAD SR # ENTER PD 12D
048914,000274: 25,3744 00007 6D
048915,000275: 25,3745 20617 14D
048916,000276: 25,3746 72371 TAD TLOAD # CHANGE MODE TO TP
048917,000277: 25,3747 01707 TIMSUBO
048918,000278: 25,3750 00155 MPAC
048919,000279: 25,3751 14017 STODL TIMSUBM # T+T0 CSEC B-42
048920,000280: 25,3752 00020 TIMSUBM +1
048921,000281: 25,3753 77605 DMP # PD 10D MULT BY XDOT IN 10-11D
048922,000282: 25,3754 43257 SL* DAD # PD 8D ADD XO IN 8-9D AFTER SHIFTING
048923,000283: 25,3755 20206 5,1 # SUCH THAT SCALING IS B-0
048924,000284: 25,3756 67206 PUSH SLOAD # PD 10D SAVE PARTIAL (X0+XDOT*T) IN 8-9D
048925,000285: 25,3757 00017 TIMSUBM
048926,000286: 25,3760 41261 SL DMP
048927,000287: 25,3761 20212 9D
048928,000288: 25,3762 00013 10D # XDOT
048929,000289: 25,3763 43257 SL* DAD # PD 8D SHIFT SUCH THAT THIS PART OF X
048930,000290: 25,3764 20213 10D,1 # IS SCALED REVS/CSEC B-0
048931,000291: 25,3765 77600 BOV # TURN OFF OVERFLOW IF SET BY SHIFT
048932,000292: 25,3766 53767 +1 # INSTRUCTION BEFORE EXITING
048933,000293: 25,3767 77616 RVQ # MPAC=X= X0+(XDOT)(T+T0) REVS B0
048934,000294:
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Page 1146 |
048936,000296: # ..... EARTHMX SUBROUTINE .....
048937,000297: # SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE EARTH
048938,000298:
048939,000299: # CALLING SEQUENCE
048940,000300: # L CALL
048941,000301: # L+1 EARTHMX
048942,000302:
048943,000303: # SUBROUTINES USED
048944,000304: # NEWANGLE
048945,000305:
048946,000306: # INPUT
048947,000307: # INPUT AVAILABLE FROM LAUNCH DATA AZO REVS B-0
048948,000308: # TEPHEM CSEC B-42
048949,000309: # 6-7D= TIME CSEC B-28
048950,000310:
048951,000311: # OUTPUT
048952,000312: # MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
048953,000313:
048954,000314: 26,3743 BANK 26
048955,000315: 26,2000 SETLOC PLANTIN1
048956,000316: 26,2000 BANK
048957,000317: 26,3743 COUNT* $$/LUROT
048958,000318:
048959,000319: 26,3743 40220 EARTHMX STQ SETPD # SET 8-9D=AZO
048960,000320: 26,3744 00051 EARTHMXX
048961,000321: 26,3745 00011 8D # 10-11D=WEARTH
048962,000322: 26,3746 77770 AXT,1 # FOR SL 5, AND SL 10 IN NEWANGLE
048963,000323: 26,3747 00000 0
048964,000324: 26,3750 65345 DLOAD PDDL # LEAVING PD SET AT 12D FOR NEWANGLE
048965,000325: 26,3751 01712 AZO
048966,000326: 26,3752 14021 WEARTH
048967,000327: 26,3753 45006 PUSH CALL
048968,000328: 26,3754 53743 NEWANGLE
048969,000329: 26,3755 41401 SETPD PUSH # 18-19D=504AZ
048970,000330: 26,3756 00023 18D # COS(AZ) SIN(AZ) 0
048971,000331: 26,3757 65346 COS PDDL # 20-37D= MMATRIX= -SIN(AZ) COS(AZ) 0 B-1
048972,000332: 26,3760 00023 504AZ # 0 0 1
048973,000333: 26,3761 65356 SIN PDDL
048974,000334: 26,3762 06522 HI6ZEROS
048975,000335: 26,3763 73525 PDDL SIN
048976,000336: 26,3764 00023 504AZ
048977,000337: 26,3765 65276 DCOMP PDDL
048978,000338: 26,3766 00023 504AZ
048979,000339: 26,3767 63346 COS PDVL
048980,000340: 26,3770 06522 HI6ZEROS
048981,000341: 26,3771 41525 PDDL PUSH
048982,000342: 26,3772 06520 HIDPHALF
048983,000343: 26,3773 77650 GOTO
048984,000344: 26,3774 00051 EARTHMXX
048985,000345:
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Page 1147 |
048987,000347: # ..... EARTHL SUBROUTINE .....
048988,000348: # SUBROUTINE TO COMPUTE L VECTOR FOR EARTH
048989,000349:
048990,000350: # CALLING SEQUENCE
048991,000351: # L CALL
048992,000352: # L+1 EARTHL
048993,000353:
048994,000354: # INPUT
048995,000355: # AXO,AYO SET AT LAUNCH TIME WITH AYO IMMEDIATELY FOLLOWING AXO IN CORE
048996,000356:
048997,000357: # OUTPUT
048998,000358: # -AX
048999,000359: # MPAC= -AY RADIANS B-0
049000,000360: # 0
049001,000361:
049002,000362: 06,3753 BANK 06
049003,000363: 06,2000 SETLOC EARTHLOC
049004,000364: 06,2000 BANK
049005,000365: 06,3753 COUNT* $$/LUROT
049006,000366:
049007,000367: 06,3753 57545 EARTHL DLOAD DCOMP
049008,000368: 06,3754 01716 AXO
049009,000369: 06,3755 14017 STODL 504LPL
049010,000370: 06,3756 01714 -AYO
049011,000371: 06,3757 14021 STODL 504LPL +2
049012,000372: 06,3760 24007 LO6ZEROS
049013,000373: 06,3761 24023 STOVL 504LPL +4
049014,000374: 06,3762 00017 504LPL
049015,000375: 06,3763 77616 RVQ
049016,000376:
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Page 1148 |
049018,000378: # CONSTANTS AND ERASABLE ASSIGNMENTS
049019,000379:
049020,000380: 06,3764 12,2004 1B1 = DP1/2 # 1 SCALED B-1
049021,000381: 06,3764 0000050 RPREXIT = S1 # R-TO-RP AND RP-TO-R SUBR EXIT
049022,000382: 06,3764 0000051 EARTHMXX = S2 # EARTHMX, MOONMX SUBR. EXITS
049023,000383: 06,3764 504RPR = 0D # 6 REGS R OR RP VECTOR
049024,000384: 06,3764 SINNODI = 8D # 2 SIN(NODI)
049025,000385: 06,3764 DVECTR = 8D # 6 D VECTOR MOON
049026,000386: 06,3764 CVECTR = 8D # 6 C VECTR MOON
049027,000387: 06,3764 504AZ = 18D # 2 AZ
049028,000388: 06,3764 TIMSUBM = 14D # 3 TIME SUB M (MOON) T+T0 IN GETAZ
049029,000389: 06,3764 504LPL = 14D # 6 L OR LP VECTOR
049030,000390: 06,3764 AVECTR = 20D # 6 A VECTOR (MOON)
049031,000391: 06,3764 BVECTR = 26D # 6 B VECTOR (MOON)
049032,000392: 06,3764 MMATRIX = 20D # 18 M MATRIX
049033,000393: 06,3764 COB = 32D # 2 COS(B) B-1
049034,000394: 06,3764 SOB = 34D # 2 SIN(B) B-1
049035,000395: 06,3764 504F = 6D # 2 F(MOON)
049036,000396:
End of include-file PLANETARY_INERTIAL_ORIENTATION.agc. Parent file is MAIN.agc