GAP: ASSEMBLE REVISION 055 OF AGC PROGRAM COMANCHE BY NASA 2021113-051 10:28 APR. 1,1969Note 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 Colossus 249 (Apollo 9)
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 055 OF AGC PROGRAM COMANCHE BY NASA 2021113-051 10:28 APR. 1,1969Note that the date is the date of the printout, not the date of the program revision. |
012435,000002: ## Copyright: Public domain.
012436,000003: ## Filename: CSM_GEOMETRY.agc
012437,000004: ## Purpose: Part of the source code for Colossus 2A, AKA Comanche 055.
012438,000005: ## It is part of the source code for the Command Module's (CM)
012439,000006: ## Apollo Guidance Computer (AGC), for Apollo 11.
012440,000007: ## Assembler: yaYUL
012441,000008: ## Contact: Ron Burkey <info@sandroid.org>.
012442,000009: ## Website: www.ibiblio.org/apollo.
012443,000010: ## Pages: 285-296
012444,000011: ## Mod history: 2009-05-08 RSB Adapted from the Colossus249/ file of the
012445,000012: ## same name, using Comanche055 page images.
012446,000013: ## 2016-12-10 RSB Proofed comments with octopus/ProoferComments
012447,000014: ## and fixed the errors found.
012448,000015: ## 2017-01-07 RSB Fixed comment errors detected in cross-diff vs
012449,000016: ## Colossus 249.
012450,000017: ## 2017-01-28 RSB WTIH -> WITH.
012451,000018: ##
012452,000019: ## This source code has been transcribed or otherwise adapted from digitized
012453,000020: ## images of a hardcopy from the MIT Museum. The digitization was performed
012454,000021: ## by Paul Fjeld, and arranged for by Deborah Douglas of the Museum. Many
012455,000022: ## thanks to both. The images (with suitable reduction in storage size and
012456,000023: ## consequent reduction in image quality as well) are available online at
012457,000024: ## www.ibiblio.org/apollo. If for some reason you find that the images are
012458,000025: ## illegible, contact me at info@sandroid.org about getting access to the
012459,000026: ## (much) higher-quality images which Paul actually created.
012460,000027: ##
012461,000028: ## Notations on the hardcopy document read, in part:
012462,000029: ##
012463,000030: ## Assemble revision 055 of AGC program Comanche by NASA
012464,000031: ## 2021113-051. 10:28 APR. 1, 1969
012465,000032: ##
012466,000033: ## This AGC program shall also be referred to as
012467,000034: ## Colossus 2A
012468,000035:
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Page 285 |
012470,000037: 22,2000 BANK 22
012471,000038: 23,2000 SETLOC COMGEOM1
012472,000039: 23,2000 BANK
012473,000040:
012474,000041: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
012475,000042: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
012476,000043:
012477,000044: # THE INPUTS ARE 1) THE SEXTANT SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
012478,000045: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
012479,000046: # JOB VAC AREA.
012480,000047:
012481,000048: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
012482,000049: # OUTPUT IS ALSO AVAILABLE AT MPAC.
012483,000050:
012484,000051: 23,2000 COUNT 23/GEOM
012485,000052:
012486,000053: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
012487,000054: 23,2001 00006 5,1 # TRUNNION = TA
012488,000055: 23,2002 45513 CDULOGIC
012489,000056: 23,2003 41434 RTB PUSH
012490,000057: 23,2004 46027 SXTLOGIC
012491,000058: 23,2005 72556 SIN SL1
012492,000059: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
012493,000060: 23,2007 00004 3,1 # SHAFT = SA
012494,000061: 23,2010 41434 RTB PUSH # PD4 = SA
012495,000062: 23,2011 45513 CDULOGIC
012496,000063:
012497,000064: 23,2012 41346 COS DMP
012498,000065: 23,2013 00003 2
012499,000066: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
012500,000067:
012501,000068: 23,2015 41356 SIN DMP
012502,000069: 23,2016 77626 STADR
012503,000070: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
012504,000071:
012505,000072: 23,2020 77746 COS
012506,000073: 23,2021 24045 STOVL STARM +4
012507,000074: 23,2022 00041 STARM # STARM = 32D
012508,000075: 23,2023 76521 MXV VSL1
012509,000076: 23,2024 06302 NB1NB2
012510,000077: 23,2025 00041 STORE 32D
012511,000078: 23,2026 77616 RVQ
012512,000079:
012513,000080: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
012514,000081: 23,2030 26154 ADS MPAC
012515,000082: 23,2031 35003 CAF QUARTER
012516,000083: 23,2032 07256 TC SHORTMP
012517,000084: 23,2033 06030 TC DANZIG
012518,000085:
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Page 286 |
012520,000087: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
012521,000088: # OF-SIGHT LIES ALONG THE STAR VECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
012522,000089: # ERENCED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
012523,000090: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
012524,000091:
012525,000092: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO PRESENT STABLE MEMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
012526,000093: # INPUT AS *SMNB*, I.E. SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
012527,000094: # TO CDUTRIG WILL PROVIDE THIS INPUT.
012528,000095:
012529,000096: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012530,000097: # EQUAL TO ZERO).
012531,000098:
012532,000099: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D
012533,000100: 23,2035 00034 28D
012534,000101: 23,2036 02766 STAR
012535,000102: 23,2037 77624 CALL
012536,000103: 23,2040 47644 *SMNB*
012537,000104: 23,2041 76521 MXV VSL1
012538,000105: 23,2042 06260 NB2NB1
012539,000106: 23,2043 26766 STOVL STAR
012540,000107: 23,2044 15333 HIUNITX
012541,000108: 23,2045 26555 STOVL XNB1
012542,000109: 23,2046 15331 HIUNITY
012543,000110: 23,2047 26563 STOVL YNB1
012544,000111: 23,2050 15327 HIUNITZ
012545,000112: 23,2051 36571 STCALL ZNB1
012546,000113: 23,2052 46076 SXTANG1
012547,000114:
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012549,000116: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
012550,000117: # SIGHT LIES ALONG THE STAR VECTOR.
012551,000118:
012552,000119: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
012553,000120: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB,AND
012554,000121: # ZNB.
012555,000122:
012556,000123: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012557,000124: # EQUAL TO ZERO).
012558,000125:
012559,000126: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
012560,000127: 23,2054 00034 28D
012561,000128: 23,2055 45662 TRANSP1 # EREF WRT NB2
012562,000129: 23,2056 64375 VLOAD MXV
012563,000130: 23,2057 02714 XNB
012564,000131: 23,2060 06260 NB2NB1
012565,000132: 23,2061 77772 VSL1
012566,000133: 23,2062 26555 STOVL XNB1
012567,000134: 23,2063 02722 YNB
012568,000135: 23,2064 76521 MXV VSL1
012569,000136: 23,2065 06260 NB2NB1
012570,000137: 23,2066 26563 STOVL YNB1
012571,000138: 23,2067 02730 ZNB
012572,000139: 23,2070 76521 MXV VSL1
012573,000140: 23,2071 06260 NB2NB1
012574,000141: 23,2072 02571 STORE ZNB1
012575,000142:
012576,000143: 23,2073 47034 RTB RTB
012577,000144: 23,2074 45662 TRANSP1
012578,000145: 23,2075 45676 TRANSP2
012579,000146:
012580,000147: 23,2076 47375 SXTANG1 VLOAD VXV
012581,000148: 23,2077 02571 ZNB1
012582,000149: 23,2100 02766 STAR
012583,000150: 23,2101 77600 BOV
012584,000151: 23,2102 46103 +1
012585,000152: 23,2103 40056 UNIT BOV
012586,000153: 23,2104 46145 ZNB=S1
012587,000154: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
012588,000155:
012589,000156: 23,2106 57441 DOT DCOMP
012590,000157: 23,2107 02555 XNB1
012591,000158: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
012592,000159: 23,2111 00027 PDA
012593,000160:
012594,000161: 23,2112 77641 DOT
012595,000162: 23,2113 02563 YNB1
012596,000163: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
012597,000164: 23,2115 47256 ARCTRIG
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012599,000166: 23,2116 77634 RTB
012600,000167: 23,2117 45546 1STO2S
012601,000168: 23,2120 26774 STOVL SAC
012602,000169: 23,2121 02766 STAR
012603,000170: 23,2122 77600 BOV
012604,000171: 23,2123 46124 +1
012605,000172: 23,2124 72441 DOT SL1
012606,000173: 23,2125 02571 ZNB1
012607,000174: 23,2126 77726 ACOS
012608,000175: 23,2127 62440 BMN SL2
012609,000176: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
012610,000177: 23,2131 45200 BOV DSU
012611,000178: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
012612,000179: 23,2133 06331 20DEG-
012613,000180: 23,2134 77634 RTB
012614,000181: 23,2135 45546 1STO2S
012615,000182: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
012616,000183: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEG
012617,000184: 23,2140 01630 CULTFLAG
012618,000185: 23,2141 00034 28D
012619,000186: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
012620,000187: 23,2143 01430 CULTFLAG
012621,000188: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI
012622,000189: 23,2145 77745 ZNB=S1 DLOAD
012623,000190: 23,2146 06325 270DEG
012624,000191: 23,2147 16774 STODL SAC
012625,000192: 23,2150 06327 20DEGS-
012626,000193: 23,2151 02776 STORE PAC
012627,000194: 23,2152 77614 CLRGO
012628,000195: 23,2153 01630 CULTFLAG
012629,000196: 23,2154 00034 28D
012630,000197:
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012632,000199: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
012633,000200: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO
012634,000201: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
012635,000202: # R-OTHER, V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
012636,000203: # OTHER VEHICLES COMPUTER.
012637,000204:
012638,000205: # INPUT
012639,000206: # STATE VECTOR IN TEMPORARY STORAGE AREA
012640,000207: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
012641,000208: # SET X2 TO +2
012642,000209: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
012643,000210: # SET X2 TO 0
012644,000211:
012645,000212: # OUTPUT
012646,000213: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
012647,000214: # OR
012648,000215: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
012649,000216:
012650,000217: 23,2155 BANK 23
012651,000218: 10,2000 SETLOC COMGEOM2
012652,000219: 10,2000 BANK
012653,000220: 10,2237 COUNT 10/GEOM
012654,000221: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
012655,000222: 10,2240 04756 AVEMIDSW
012656,000223: 10,2241 20242 +1
012657,000224: 10,2242 53775 VLOAD VSL*
012658,000225: 10,2243 01521 TDELTAV
012659,000226: 10,2244 57605 0 -7,2
012660,000227: 10,2245 53655 VAD VSL*
012661,000228: 10,2246 01535 RCV
012662,000229: 10,2247 57576 0,2
012663,000230: 10,2250 25171 STOVL RN
012664,000231: 10,2251 01527 TNUV
012665,000232: 10,2252 53257 VSL* VAD
012666,000233: 10,2253 57602 0 -4,2
012667,000234: 10,2254 01543 VCV
012668,000235: 10,2255 77657 VSL*
012669,000236: 10,2256 57576 0,2
012670,000237: 10,2257 15177 STODL VN
012671,000238: 10,2260 01517 TET
012672,000239: 10,2261 01205 STORE PIPTIME
012673,000240: 10,2262 77616 RVQ
012674,000241:
012675,000242: 10,2263 53775 SVDWN2 VLOAD VSL*
012676,000243: 10,2264 01521 TDELTAV
012677,000244: 10,2265 57605 0 -7,2
012678,000245: 10,2266 53655 VAD VSL*
012679,000246: 10,2267 01535 RCV
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012681,000248: 10,2270 57576 0,2
012682,000249: 10,2271 25722 STOVL R-OTHER
012683,000250: 10,2272 01527 TNUV
012684,000251: 10,2273 53257 VSL* VAD
012685,000252: 10,2274 57602 0 -4,2
012686,000253: 10,2275 01543 VCV
012687,000254: 10,2276 77657 VSL*
012688,000255: 10,2277 57576 0,2
012689,000256: 10,2300 01730 STORE V-OTHER
012690,000257: 10,2301 77616 RVQ
012691,000258:
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012693,000260: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
012694,000261:
012695,000262: # ENTRY: CALL
012696,000263: # LOG
012697,000264:
012698,000265: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
012699,000266:
012700,000267: # EBANK IS ARBITRARY..
012701,000268:
012702,000269: 14,2000 BANK 14
012703,000270: 23,2000 SETLOC POWFLIT2
012704,000271: 23,2000 BANK
012705,000272: 23,2155 COUNT 23/GEOM
012706,000273:
012707,000274: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
012708,000275: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
012709,000276: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
012710,000277: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
012711,000278: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
012712,000279: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
012713,000280: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
012714,000281: 23,2165 01001 14636 2DEC .031335467
012715,000282: 23,2167 00325 07310 2DEC .0130145859
012716,000283: 23,2171 00541 16735 2DEC .0215738898
012717,000284:
012718,000285: 23,2173 35021 CAF ZERO
012719,000286: 23,2174 54156 TS MPAC +2
012720,000287: 23,2175 00006 EXTEND
012721,000288: 23,2176 32214 DCA CLOG2/32
012722,000289: 23,2177 52155 DXCH MPAC
012723,000290: 23,2200 52160 DXCH MPAC +3
012724,000291: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
012725,000292: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
012726,000293:
012727,000294: 23,2203 52156 DXCH MPAC +1
012728,000295: 23,2204 52155 DXCH MPAC
012729,000296: 23,2205 52160 DXCH MPAC +3
012730,000297: 23,2206 20155 DAS MPAC
012731,000298: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
012732,000299:
012733,000300: 23,2210 77616 RVQ
012734,000301:
012735,000302: 23,2211 37777 37777 NEARLY1 2DEC .999999999
012736,000303:
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012738,000305: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494
012739,000306:
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012741,000308: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
012742,000309: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
012743,000310: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
012744,000311:
012745,000312: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
012746,000313: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
012747,000314: # AND NORMAL COMPONENTS RTEAST AND RTNORM. INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
012748,000315: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
012749,000316: # TARGET VECTOR RT. ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
012750,000317: # THE EQUATIONS ARE
012751,000318: # - - - -
012752,000319: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT)
012753,000320:
012754,000321: # WHERE WT = WIE DTEAROT
012755,000322:
012756,000323: # RTINIT = INITIAL TARGET VECTOR
012757,000324: # - - -
012758,000325: # RTEAST = UNITW * RTINIT
012759,000326: # - - -
012760,000327: # RTNORM = RTEAST * UNITW
012761,000328:
012762,000329: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
012763,000330: #
012764,000331: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
012765,000332: # STCALL DTEAROT STCALL DTEAROT
012766,000333: # EARROT1 EARROT2
012767,000334: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
012768,000335: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
012769,000336:
012770,000337: # SUBROUTINES USED: NONE
012771,000338:
012772,000339: # NORMAL EXIT MODES: RVQ
012773,000340:
012774,000341: # ALARMS: NONE
012775,000342:
012776,000343: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
012777,000344: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
012778,000345: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
012779,000346: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
012780,000347:
012781,000348: # ERASABLE INITIALIZATION REQUIRED:
012782,000349: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
012783,000350: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
012784,000351: # DTEAROT (-28) CS TIME OF FLIGHT LEFT BY CALLER
012785,000352:
012786,000353: # DEBRIS: QPRET, PDL+0 ... PDL+5
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012788,000355: 23,2215 E7,1451 EBANK= RTINIT
012789,000356:
012790,000357: 23,2215 47375 EARROT1 VLOAD VXV
012791,000358: 23,2216 01714 UNITW # FULL UNIT VECTOR
012792,000359: 23,2217 03452 RTINIT # .5 UNIT
012793,000360: 23,2220 03460 STORE RTEAST # .5 UNIT
012794,000361:
012795,000362: 23,2221 77635 VXV
012796,000363: 23,2222 01714 UNITW # FULL UNIT
012797,000364: 23,2223 17466 STODL RTNORM # .5 UNIT
012798,000365: 23,2224 03606 DTEAROT # (-28) CS
012799,000366:
012800,000367: 23,2225 56204 EARROT2 BOVB DDV
012801,000368: 23,2226 57352 TCDANZIG # RESET OVFIND, IF ON
012802,000369: 23,2227 06256 1/WIE
012803,000370: 23,2230 41400 BOV PUSH
012804,000371: 23,2231 46245 OVERADAY
012805,000372: 23,2232 45346 COS DSU
012806,000373: 23,2233 15333 HIDPHALF
012807,000374: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST
012808,000375: 23,2235 03466 RTNORM # .5 UNIT
012809,000376: 23,2236 74356 SIN VXSC
012810,000377: 23,2237 03460 RTEAST # .5 UNIT
012811,000378: 23,2240 76455 VAD VSL1
012812,000379: 23,2241 53455 VAD UNIT # INSURE THAT RT IS 'UNIT'.
012813,000380: 23,2242 03452 RTINIT # .5 UNIT
012814,000381: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR
012815,000382:
012816,000383: 23,2244 77616 RVQ
012817,000384:
012818,000385: 23,2245 75345 OVERADAY DLOAD SIGN
012819,000386: 23,2246 06256 1/WIE
012820,000387: 23,2247 03606 DTEAROT
012821,000388: 23,2250 77621 BDSU
012822,000389: 23,2251 03606 DTEAROT
012823,000390: 23,2252 03606 STORE DTEAROT
012824,000391:
012825,000392: 23,2253 77650 GOTO
012826,000393: 23,2254 46225 EARROT2
012827,000394:
012828,000395: # WIE 2DEC .1901487997
012829,000396: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28
012830,000397: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1
012831,000398: 23,2261 00000 00000 2DEC 0 B-28
012832,000399: 23,2263 67313 65307 2DEC -.5376381241 B-1
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Page 295 |
012834,000401: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28
012835,000402: 23,2267 20000 00000 HALFNFLT 2DEC .5
012836,000403: 23,2271 00000 00000 2DEC 0 B-28
012837,000404: 23,2273 10464 12470 2DEC +.5376381241 B-1
012838,000405: 23,2275 00000 00000 2DEC 0 B-28
012839,000406: 23,2277 15373 11346 2DEC +.8431756920 B-1
012840,000407: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1
012841,000408: 23,2303 00000 00000 2DEC 0 B-28
012842,000409: 23,2305 10464 12470 2DEC +.5376381241 B-1
012843,000410: 23,2307 00000 00000 2DEC 0 B-28
012844,000411: 23,2311 20000 00000 2DEC .5
012845,000412: 23,2313 00000 00000 2DEC 0 B-28
012846,000413: 23,2315 67313 65307 2DEC -.5376381241 B-1
012847,000414: 23,2317 00000 00000 2DEC 0 B-28
012848,000415: 23,2321 15373 11346 2DEC +.8431756920 B-1
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Page 296 |
012850,000417: 23,2323 07020 10DEGS- DEC 3600 B-14
012851,000418: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 2S COMP.
012852,000419: 23,2325 00000 OCT 00000
012853,000420: 23,2326 61740 20DEGS- DEC -07199 B-14
012854,000421: 23,2327 77777 DEC -00000 B-14
012855,000422: 23,2330 07020 20DEG- DEC 03600 B-14
012856,000423: 23,2331 00000 DEC 00000 B-14
012857,000424:
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc