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. |
012428,000002: ## Copyright: Public domain.
012429,000003: ## Filename: CSM_GEOMETRY.agc
012430,000004: ## Purpose: Part of the source code for Colossus 2A, AKA Comanche 055.
012431,000005: ## It is part of the source code for the Command Module's (CM)
012432,000006: ## Apollo Guidance Computer (AGC), for Apollo 11.
012433,000007: ## Assembler: yaYUL
012434,000008: ## Contact: Ron Burkey <info@sandroid.org>.
012435,000009: ## Website: www.ibiblio.org/apollo.
012436,000010: ## Pages: 285-296
012437,000011: ## Mod history: 2009-05-08 RSB Adapted from the Colossus249/ file of the
012438,000012: ## same name, using Comanche055 page images.
012439,000013: ## 2016-12-10 RSB Proofed comments with octopus/ProoferComments
012440,000014: ## and fixed the errors found.
012441,000015: ## 2017-01-07 RSB Fixed comment errors detected in cross-diff vs
012442,000016: ## Colossus 249.
012443,000017: ## 2017-01-28 RSB WTIH -> WITH.
012444,000018: ##
012445,000019: ## This source code has been transcribed or otherwise adapted from digitized
012446,000020: ## images of a hardcopy from the MIT Museum. The digitization was performed
012447,000021: ## by Paul Fjeld, and arranged for by Deborah Douglas of the Museum. Many
012448,000022: ## thanks to both. The images (with suitable reduction in storage size and
012449,000023: ## consequent reduction in image quality as well) are available online at
012450,000024: ## www.ibiblio.org/apollo. If for some reason you find that the images are
012451,000025: ## illegible, contact me at info@sandroid.org about getting access to the
012452,000026: ## (much) higher-quality images which Paul actually created.
012453,000027: ##
012454,000028: ## Notations on the hardcopy document read, in part:
012455,000029: ##
012456,000030: ## Assemble revision 055 of AGC program Comanche by NASA
012457,000031: ## 2021113-051. 10:28 APR. 1, 1969
012458,000032: ##
012459,000033: ## This AGC program shall also be referred to as
012460,000034: ## Colossus 2A
012461,000035:
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Page 285 |
012463,000037: 22,2000 BANK 22
012464,000038: 23,2000 SETLOC COMGEOM1
012465,000039: 23,2000 BANK
012466,000040:
012467,000041: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
012468,000042: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
012469,000043:
012470,000044: # THE INPUTS ARE 1) THE SEXTANT SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
012471,000045: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
012472,000046: # JOB VAC AREA.
012473,000047:
012474,000048: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
012475,000049: # OUTPUT IS ALSO AVAILABLE AT MPAC.
012476,000050:
012477,000051: 23,2000 COUNT 23/GEOM
012478,000052:
012479,000053: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
012480,000054: 23,2001 00006 5,1 # TRUNNION = TA
012481,000055: 23,2002 45513 CDULOGIC
012482,000056: 23,2003 41434 RTB PUSH
012483,000057: 23,2004 46027 SXTLOGIC
012484,000058: 23,2005 72556 SIN SL1
012485,000059: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
012486,000060: 23,2007 00004 3,1 # SHAFT = SA
012487,000061: 23,2010 41434 RTB PUSH # PD4 = SA
012488,000062: 23,2011 45513 CDULOGIC
012489,000063:
012490,000064: 23,2012 41346 COS DMP
012491,000065: 23,2013 00003 2
012492,000066: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
012493,000067:
012494,000068: 23,2015 41356 SIN DMP
012495,000069: 23,2016 77626 STADR
012496,000070: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
012497,000071:
012498,000072: 23,2020 77746 COS
012499,000073: 23,2021 24045 STOVL STARM +4
012500,000074: 23,2022 00041 STARM # STARM = 32D
012501,000075: 23,2023 76521 MXV VSL1
012502,000076: 23,2024 06302 NB1NB2
012503,000077: 23,2025 00041 STORE 32D
012504,000078: 23,2026 77616 RVQ
012505,000079:
012506,000080: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
012507,000081: 23,2030 26154 ADS MPAC
012508,000082: 23,2031 35003 CAF QUARTER
012509,000083: 23,2032 07256 TC SHORTMP
012510,000084: 23,2033 06030 TC DANZIG
012511,000085:
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Page 286 |
012513,000087: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
012514,000088: # OF-SIGHT LIES ALONG THE STAR VECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
012515,000089: # ERENCED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
012516,000090: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
012517,000091:
012518,000092: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO PRESENT STABLE MEMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
012519,000093: # INPUT AS *SMNB*, I.E. SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
012520,000094: # TO CDUTRIG WILL PROVIDE THIS INPUT.
012521,000095:
012522,000096: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012523,000097: # EQUAL TO ZERO).
012524,000098:
012525,000099: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D
012526,000100: 23,2035 00034 28D
012527,000101: 23,2036 02766 STAR
012528,000102: 23,2037 77624 CALL
012529,000103: 23,2040 47644 *SMNB*
012530,000104: 23,2041 76521 MXV VSL1
012531,000105: 23,2042 06260 NB2NB1
012532,000106: 23,2043 26766 STOVL STAR
012533,000107: 23,2044 15333 HIUNITX
012534,000108: 23,2045 26555 STOVL XNB1
012535,000109: 23,2046 15331 HIUNITY
012536,000110: 23,2047 26563 STOVL YNB1
012537,000111: 23,2050 15327 HIUNITZ
012538,000112: 23,2051 36571 STCALL ZNB1
012539,000113: 23,2052 46076 SXTANG1
012540,000114:
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012542,000116: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
012543,000117: # SIGHT LIES ALONG THE STAR VECTOR.
012544,000118:
012545,000119: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
012546,000120: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB,AND
012547,000121: # ZNB.
012548,000122:
012549,000123: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012550,000124: # EQUAL TO ZERO).
012551,000125:
012552,000126: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
012553,000127: 23,2054 00034 28D
012554,000128: 23,2055 45662 TRANSP1 # EREF WRT NB2
012555,000129: 23,2056 64375 VLOAD MXV
012556,000130: 23,2057 02714 XNB
012557,000131: 23,2060 06260 NB2NB1
012558,000132: 23,2061 77772 VSL1
012559,000133: 23,2062 26555 STOVL XNB1
012560,000134: 23,2063 02722 YNB
012561,000135: 23,2064 76521 MXV VSL1
012562,000136: 23,2065 06260 NB2NB1
012563,000137: 23,2066 26563 STOVL YNB1
012564,000138: 23,2067 02730 ZNB
012565,000139: 23,2070 76521 MXV VSL1
012566,000140: 23,2071 06260 NB2NB1
012567,000141: 23,2072 02571 STORE ZNB1
012568,000142:
012569,000143: 23,2073 47034 RTB RTB
012570,000144: 23,2074 45662 TRANSP1
012571,000145: 23,2075 45676 TRANSP2
012572,000146:
012573,000147: 23,2076 47375 SXTANG1 VLOAD VXV
012574,000148: 23,2077 02571 ZNB1
012575,000149: 23,2100 02766 STAR
012576,000150: 23,2101 77600 BOV
012577,000151: 23,2102 46103 +1
012578,000152: 23,2103 40056 UNIT BOV
012579,000153: 23,2104 46145 ZNB=S1
012580,000154: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
012581,000155:
012582,000156: 23,2106 57441 DOT DCOMP
012583,000157: 23,2107 02555 XNB1
012584,000158: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
012585,000159: 23,2111 00027 PDA
012586,000160:
012587,000161: 23,2112 77641 DOT
012588,000162: 23,2113 02563 YNB1
012589,000163: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
012590,000164: 23,2115 47256 ARCTRIG
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012592,000166: 23,2116 77634 RTB
012593,000167: 23,2117 45546 1STO2S
012594,000168: 23,2120 26774 STOVL SAC
012595,000169: 23,2121 02766 STAR
012596,000170: 23,2122 77600 BOV
012597,000171: 23,2123 46124 +1
012598,000172: 23,2124 72441 DOT SL1
012599,000173: 23,2125 02571 ZNB1
012600,000174: 23,2126 77726 ACOS
012601,000175: 23,2127 62440 BMN SL2
012602,000176: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
012603,000177: 23,2131 45200 BOV DSU
012604,000178: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
012605,000179: 23,2133 06331 20DEG-
012606,000180: 23,2134 77634 RTB
012607,000181: 23,2135 45546 1STO2S
012608,000182: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
012609,000183: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEG
012610,000184: 23,2140 01630 CULTFLAG
012611,000185: 23,2141 00034 28D
012612,000186: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
012613,000187: 23,2143 01430 CULTFLAG
012614,000188: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI
012615,000189: 23,2145 77745 ZNB=S1 DLOAD
012616,000190: 23,2146 06325 270DEG
012617,000191: 23,2147 16774 STODL SAC
012618,000192: 23,2150 06327 20DEGS-
012619,000193: 23,2151 02776 STORE PAC
012620,000194: 23,2152 77614 CLRGO
012621,000195: 23,2153 01630 CULTFLAG
012622,000196: 23,2154 00034 28D
012623,000197:
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Page 289 |
012625,000199: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
012626,000200: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO
012627,000201: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
012628,000202: # R-OTHER, V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
012629,000203: # OTHER VEHICLES COMPUTER.
012630,000204:
012631,000205: # INPUT
012632,000206: # STATE VECTOR IN TEMPORARY STORAGE AREA
012633,000207: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
012634,000208: # SET X2 TO +2
012635,000209: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
012636,000210: # SET X2 TO 0
012637,000211:
012638,000212: # OUTPUT
012639,000213: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
012640,000214: # OR
012641,000215: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
012642,000216:
012643,000217: 23,2155 BANK 23
012644,000218: 10,2000 SETLOC COMGEOM2
012645,000219: 10,2000 BANK
012646,000220: 10,2237 COUNT 10/GEOM
012647,000221: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
012648,000222: 10,2240 04756 AVEMIDSW
012649,000223: 10,2241 20242 +1
012650,000224: 10,2242 53775 VLOAD VSL*
012651,000225: 10,2243 01521 TDELTAV
012652,000226: 10,2244 57605 0 -7,2
012653,000227: 10,2245 53655 VAD VSL*
012654,000228: 10,2246 01535 RCV
012655,000229: 10,2247 57576 0,2
012656,000230: 10,2250 25171 STOVL RN
012657,000231: 10,2251 01527 TNUV
012658,000232: 10,2252 53257 VSL* VAD
012659,000233: 10,2253 57602 0 -4,2
012660,000234: 10,2254 01543 VCV
012661,000235: 10,2255 77657 VSL*
012662,000236: 10,2256 57576 0,2
012663,000237: 10,2257 15177 STODL VN
012664,000238: 10,2260 01517 TET
012665,000239: 10,2261 01205 STORE PIPTIME
012666,000240: 10,2262 77616 RVQ
012667,000241:
012668,000242: 10,2263 53775 SVDWN2 VLOAD VSL*
012669,000243: 10,2264 01521 TDELTAV
012670,000244: 10,2265 57605 0 -7,2
012671,000245: 10,2266 53655 VAD VSL*
012672,000246: 10,2267 01535 RCV
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Page 290 |
012674,000248: 10,2270 57576 0,2
012675,000249: 10,2271 25722 STOVL R-OTHER
012676,000250: 10,2272 01527 TNUV
012677,000251: 10,2273 53257 VSL* VAD
012678,000252: 10,2274 57602 0 -4,2
012679,000253: 10,2275 01543 VCV
012680,000254: 10,2276 77657 VSL*
012681,000255: 10,2277 57576 0,2
012682,000256: 10,2300 01730 STORE V-OTHER
012683,000257: 10,2301 77616 RVQ
012684,000258:
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Page 291 |
012686,000260: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
012687,000261:
012688,000262: # ENTRY: CALL
012689,000263: # LOG
012690,000264:
012691,000265: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
012692,000266:
012693,000267: # EBANK IS ARBITRARY..
012694,000268:
012695,000269: 14,2000 BANK 14
012696,000270: 23,2000 SETLOC POWFLIT2
012697,000271: 23,2000 BANK
012698,000272: 23,2155 COUNT 23/GEOM
012699,000273:
012700,000274: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
012701,000275: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
012702,000276: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
012703,000277: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
012704,000278: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
012705,000279: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
012706,000280: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
012707,000281: 23,2165 01001 14636 2DEC .031335467
012708,000282: 23,2167 00325 07310 2DEC .0130145859
012709,000283: 23,2171 00541 16735 2DEC .0215738898
012710,000284:
012711,000285: 23,2173 35021 CAF ZERO
012712,000286: 23,2174 54156 TS MPAC +2
012713,000287: 23,2175 00006 EXTEND
012714,000288: 23,2176 32214 DCA CLOG2/32
012715,000289: 23,2177 52155 DXCH MPAC
012716,000290: 23,2200 52160 DXCH MPAC +3
012717,000291: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
012718,000292: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
012719,000293:
012720,000294: 23,2203 52156 DXCH MPAC +1
012721,000295: 23,2204 52155 DXCH MPAC
012722,000296: 23,2205 52160 DXCH MPAC +3
012723,000297: 23,2206 20155 DAS MPAC
012724,000298: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
012725,000299:
012726,000300: 23,2210 77616 RVQ
012727,000301:
012728,000302: 23,2211 37777 37777 NEARLY1 2DEC .999999999
012729,000303:
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012731,000305: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494
012732,000306:
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Page 293 |
012734,000308: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
012735,000309: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
012736,000310: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
012737,000311:
012738,000312: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
012739,000313: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
012740,000314: # AND NORMAL COMPONENTS RTEAST AND RTNORM. INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
012741,000315: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
012742,000316: # TARGET VECTOR RT. ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
012743,000317: # THE EQUATIONS ARE
012744,000318: # - - - -
012745,000319: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT)
012746,000320:
012747,000321: # WHERE WT = WIE DTEAROT
012748,000322:
012749,000323: # RTINIT = INITIAL TARGET VECTOR
012750,000324: # - - -
012751,000325: # RTEAST = UNITW * RTINIT
012752,000326: # - - -
012753,000327: # RTNORM = RTEAST * UNITW
012754,000328:
012755,000329: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
012756,000330: #
012757,000331: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
012758,000332: # STCALL DTEAROT STCALL DTEAROT
012759,000333: # EARROT1 EARROT2
012760,000334: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
012761,000335: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
012762,000336:
012763,000337: # SUBROUTINES USED: NONE
012764,000338:
012765,000339: # NORMAL EXIT MODES: RVQ
012766,000340:
012767,000341: # ALARMS: NONE
012768,000342:
012769,000343: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
012770,000344: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
012771,000345: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
012772,000346: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
012773,000347:
012774,000348: # ERASABLE INITIALIZATION REQUIRED:
012775,000349: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
012776,000350: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
012777,000351: # DTEAROT (-28) CS TIME OF FLIGHT LEFT BY CALLER
012778,000352:
012779,000353: # DEBRIS: QPRET, PDL+0 ... PDL+5
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012781,000355: 23,2215 E7,1451 EBANK= RTINIT
012782,000356:
012783,000357: 23,2215 47375 EARROT1 VLOAD VXV
012784,000358: 23,2216 01714 UNITW # FULL UNIT VECTOR
012785,000359: 23,2217 03452 RTINIT # .5 UNIT
012786,000360: 23,2220 03460 STORE RTEAST # .5 UNIT
012787,000361:
012788,000362: 23,2221 77635 VXV
012789,000363: 23,2222 01714 UNITW # FULL UNIT
012790,000364: 23,2223 17466 STODL RTNORM # .5 UNIT
012791,000365: 23,2224 03606 DTEAROT # (-28) CS
012792,000366:
012793,000367: 23,2225 56204 EARROT2 BOVB DDV
012794,000368: 23,2226 57352 TCDANZIG # RESET OVFIND, IF ON
012795,000369: 23,2227 06256 1/WIE
012796,000370: 23,2230 41400 BOV PUSH
012797,000371: 23,2231 46245 OVERADAY
012798,000372: 23,2232 45346 COS DSU
012799,000373: 23,2233 15333 HIDPHALF
012800,000374: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST
012801,000375: 23,2235 03466 RTNORM # .5 UNIT
012802,000376: 23,2236 74356 SIN VXSC
012803,000377: 23,2237 03460 RTEAST # .5 UNIT
012804,000378: 23,2240 76455 VAD VSL1
012805,000379: 23,2241 53455 VAD UNIT # INSURE THAT RT IS 'UNIT'.
012806,000380: 23,2242 03452 RTINIT # .5 UNIT
012807,000381: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR
012808,000382:
012809,000383: 23,2244 77616 RVQ
012810,000384:
012811,000385: 23,2245 75345 OVERADAY DLOAD SIGN
012812,000386: 23,2246 06256 1/WIE
012813,000387: 23,2247 03606 DTEAROT
012814,000388: 23,2250 77621 BDSU
012815,000389: 23,2251 03606 DTEAROT
012816,000390: 23,2252 03606 STORE DTEAROT
012817,000391:
012818,000392: 23,2253 77650 GOTO
012819,000393: 23,2254 46225 EARROT2
012820,000394:
012821,000395: # WIE 2DEC .1901487997
012822,000396: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28
012823,000397: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1
012824,000398: 23,2261 00000 00000 2DEC 0 B-28
012825,000399: 23,2263 67313 65307 2DEC -.5376381241 B-1
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Page 295 |
012827,000401: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28
012828,000402: 23,2267 20000 00000 HALFNFLT 2DEC .5
012829,000403: 23,2271 00000 00000 2DEC 0 B-28
012830,000404: 23,2273 10464 12470 2DEC +.5376381241 B-1
012831,000405: 23,2275 00000 00000 2DEC 0 B-28
012832,000406: 23,2277 15373 11346 2DEC +.8431756920 B-1
012833,000407: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1
012834,000408: 23,2303 00000 00000 2DEC 0 B-28
012835,000409: 23,2305 10464 12470 2DEC +.5376381241 B-1
012836,000410: 23,2307 00000 00000 2DEC 0 B-28
012837,000411: 23,2311 20000 00000 2DEC .5
012838,000412: 23,2313 00000 00000 2DEC 0 B-28
012839,000413: 23,2315 67313 65307 2DEC -.5376381241 B-1
012840,000414: 23,2317 00000 00000 2DEC 0 B-28
012841,000415: 23,2321 15373 11346 2DEC +.8431756920 B-1
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Page 296 |
012843,000417: 23,2323 07020 10DEGS- DEC 3600 B-14
012844,000418: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 2S COMP.
012845,000419: 23,2325 00000 OCT 00000
012846,000420: 23,2326 61740 20DEGS- DEC -07199 B-14
012847,000421: 23,2327 77777 DEC -00000 B-14
012848,000422: 23,2330 07020 20DEG- DEC 03600 B-14
012849,000423: 23,2331 00000 DEC 00000 B-14
012850,000424:
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc