Source Code
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This is the source-code for the Apollo 9 Command Module's Guidance Computer.
These files were derived originally from the scan from MIT's Dibner Institute's
now-discontinued website titled "History of Recent Science and Technology", which
in turn was originally created by Gary Neff, though his high-quality scans were
unfortunately reduced in legibility when presented online.
The markings on the front of the
printout imply that it was the original AGC developer Norm Brodeur's copy.
A scan by Ron Burkey has superceded it, made from a more-legible copy from the collection of original
AGC developer Fred Martin. The source code was transcribed from
those images by Ron Burkey. 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:ASSEMBLE REVISION 249 OF AGC PROGRAM COLOSSUS BY NASA 2021111-041 20'35 OCT. 28,1968Note that the date is the date of the printout, not the date of the program revision. |
012222,000002: ## Copyright: Public domain.
012223,000003: ## Filename: CSM_GEOMETRY.agc
012224,000004: ## Purpose: Part of the source code for Colossus, build 249.
012225,000005: ## It is part of the source code for the Command Module's (CM)
012226,000006: ## Apollo Guidance Computer (AGC), for Apollo 9.
012227,000007: ## Assembler: yaYUL
012228,000008: ## Reference: pp. 280-291.
012229,000009: ## Contact: Ron Burkey <info@sandroid.org>.
012230,000010: ## Website: www.ibiblio.org/apollo.
012231,000011: ## Mod history: 08/08/04 RSB. Began transcribing.
012232,000012: ## 2017-01-05 RSB Page numbers now agree with those on the
012233,000013: ## original harcopy, as opposed to the PDF page
012234,000014: ## numbers in 1701.pdf.
012235,000015: ## 2017-01-07 RSB Cross-diff'd comment text (not whitespace)
012236,000016: ## vs the already-proofed corresponding Colossus
012237,000017: ## 237 and Comanche 55 source-code files
012238,000018: ## and corrected errors found.
012239,000019: ## 2017-01-28 RSB WTIH -> WITH.
012240,000020: ##
012241,000021: ## The contents of the "Colossus249" files, in general, are transcribed
012242,000022: ## from a scanned copy of the program listing. Notations on this
012243,000023: ## document read, in part:
012244,000024: ##
012245,000025: ## Assemble revision 249 of AGC program Colossus by NASA
012246,000026: ## 2021111-041. October 28, 1968.
012247,000027: ##
012248,000028: ## This AGC program shall also be referred to as
012249,000029: ## Colossus 1A
012250,000030: ##
012251,000031: ## Prepared by
012252,000032: ## Massachusetts Institute of Technology
012253,000033: ## 75 Cambridge Parkway
012254,000034: ## Cambridge, Massachusetts
012255,000035: ## under NASA contract NAS 9-4065.
012256,000036: ##
012257,000037: ## Refer directly to the online document mentioned above for further information.
012258,000038: ## Please report any errors (relative to the scanned pages) to info@sandroid.org.
012259,000039: ##
012260,000040: ## In some cases, where the source code for Luminary 131 overlaps that of
012261,000041: ## Colossus 249, this code is instead copied from the corresponding Luminary 131
012262,000042: ## source file, and then is proofed to incorporate any changes.
012263,000043:
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012265,000045: 22,2000 BANK 22
012266,000046: 23,2000 SETLOC COMGEOM1
012267,000047: 23,2000 BANK
012268,000048:
012269,000049: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
012270,000050: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
012271,000051:
012272,000052: # THE INPUTS ARE 1) THE SEXTANT SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
012273,000053: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
012274,000054: # JOB VAC AREA.
012275,000055:
012276,000056: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
012277,000057: # OUTPUT IS ALSO AVAILABLE AT MPAC.
012278,000058:
012279,000059: 23,2000 COUNT 23/GEOM
012280,000060:
012281,000061: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
012282,000062: 23,2001 00006 5,1 # TRUNNION = TA
012283,000063: 23,2002 45510 CDULOGIC
012284,000064: 23,2003 41434 RTB PUSH
012285,000065: 23,2004 46027 SXTLOGIC
012286,000066: 23,2005 72556 SIN SL1
012287,000067: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
012288,000068: 23,2007 00004 3,1 # SHAFT = SA
012289,000069: 23,2010 41434 RTB PUSH # PD4 = SA
012290,000070: 23,2011 45510 CDULOGIC
012291,000071:
012292,000072: 23,2012 41346 COS DMP
012293,000073: 23,2013 00003 2
012294,000074: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
012295,000075:
012296,000076: 23,2015 41356 SIN DMP
012297,000077: 23,2016 77626 STADR
012298,000078: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
012299,000079:
012300,000080: 23,2020 77746 COS
012301,000081: 23,2021 24045 STOVL STARM +4
012302,000082: 23,2022 00041 STARM # STARM = 32D
012303,000083: 23,2023 76521 MXV VSL1
012304,000084: 23,2024 06302 NB1NB2
012305,000085: 23,2025 00041 STORE 32D
012306,000086: 23,2026 77616 RVQ
012307,000087: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
012308,000088: 23,2030 26154 ADS MPAC
012309,000089: 23,2031 34676 CAF QUARTER
012310,000090: 23,2032 07256 TC SHORTMP
012311,000091: 23,2033 06030 TC DANZIG
012312,000092:
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012314,000094: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
012315,000095: # OF-SIGHT LIES ALONG THE STAR VECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
012316,000096: # ERENCED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
012317,000097: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
012318,000098:
012319,000099: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO PRESENT STABLE MEMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
012320,000100: # INPUT AS *SMNB*, I.E. SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
012321,000101: # TO CDUTRIG WILL PROVIDE THIS INPUT.
012322,000102:
012323,000103: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012324,000104: # EQUAL TO ZERO).
012325,000105:
012326,000106: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D
012327,000107: 23,2035 00034 28D
012328,000108: 23,2036 02766 STAR
012329,000109: 23,2037 77624 CALL
012330,000110: 23,2040 47577 *SMNB*
012331,000111: 23,2041 76521 MXV VSL1
012332,000112: 23,2042 06260 NB2NB1
012333,000113: 23,2043 26766 STOVL STAR
012334,000114: 23,2044 15330 HIUNITX
012335,000115: 23,2045 26555 STOVL XNB1
012336,000116: 23,2046 15326 HIUNITY
012337,000117: 23,2047 26563 STOVL YNB1
012338,000118: 23,2050 15324 HIUNITZ
012339,000119: 23,2051 36571 STCALL ZNB1
012340,000120: 23,2052 46076 SXTANG1
012341,000121:
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012343,000123: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
012344,000124: # SIGHT LIES ALONG THE STAR VECTOR.
012345,000125:
012346,000126: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
012347,000127: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB,AND
012348,000128: # ZNB.
012349,000129:
012350,000130: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012351,000131: # EQUAL TO ZERO).
012352,000132:
012353,000133: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
012354,000134: 23,2054 00034 28D
012355,000135: 23,2055 45657 TRANSP1 # EREF WRT NB2
012356,000136: 23,2056 64375 VLOAD MXV
012357,000137: 23,2057 02714 XNB
012358,000138: 23,2060 06260 NB2NB1
012359,000139: 23,2061 77772 VSL1
012360,000140: 23,2062 26555 STOVL XNB1
012361,000141: 23,2063 02722 YNB
012362,000142: 23,2064 76521 MXV VSL1
012363,000143: 23,2065 06260 NB2NB1
012364,000144: 23,2066 26563 STOVL YNB1
012365,000145: 23,2067 02730 ZNB
012366,000146: 23,2070 76521 MXV VSL1
012367,000147: 23,2071 06260 NB2NB1
012368,000148: 23,2072 02571 STORE ZNB1
012369,000149:
012370,000150: 23,2073 47034 RTB RTB
012371,000151: 23,2074 45657 TRANSP1
012372,000152: 23,2075 45673 TRANSP2
012373,000153:
012374,000154: 23,2076 47375 SXTANG1 VLOAD VXV
012375,000155: 23,2077 02571 ZNB1
012376,000156: 23,2100 02766 STAR
012377,000157: 23,2101 77600 BOV
012378,000158: 23,2102 46103 +1
012379,000159: 23,2103 40056 UNIT BOV
012380,000160: 23,2104 46145 ZNB=S1
012381,000161: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
012382,000162:
012383,000163: 23,2106 57441 DOT DCOMP
012384,000164: 23,2107 02555 XNB1
012385,000165: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
012386,000166: 23,2111 00027 PDA
012387,000167:
012388,000168: 23,2112 77641 DOT
012389,000169: 23,2113 02563 YNB1
012390,000170: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
012391,000171: 23,2115 47211 ARCTRIG
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012393,000173: 23,2116 77634 RTB
012394,000174: 23,2117 45543 1STO2S
012395,000175: 23,2120 26774 STOVL SAC
012396,000176: 23,2121 02766 STAR
012397,000177: 23,2122 77600 BOV
012398,000178: 23,2123 46124 +1
012399,000179: 23,2124 72441 DOT SL1
012400,000180: 23,2125 02571 ZNB1
012401,000181: 23,2126 77726 ACOS
012402,000182: 23,2127 62440 BMN SL2
012403,000183: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
012404,000184: 23,2131 45200 BOV DSU
012405,000185: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
012406,000186: 23,2133 06331 20DEG-
012407,000187: 23,2134 77634 RTB
012408,000188: 23,2135 45543 1STO2S
012409,000189: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
012410,000190: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEG
012411,000191: 23,2140 01630 CULTFLAG
012412,000192: 23,2141 00034 28D
012413,000193: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
012414,000194: 23,2143 01430 CULTFLAG
012415,000195: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI
012416,000196: 23,2145 77745 ZNB=S1 DLOAD
012417,000197: 23,2146 06325 270DEG
012418,000198: 23,2147 16774 STODL SAC
012419,000199: 23,2150 06327 20DEGS-
012420,000200: 23,2151 02776 STORE PAC
012421,000201: 23,2152 77614 CLRGO
012422,000202: 23,2153 01630 CULTFLAG
012423,000203: 23,2154 00034 28D
012424,000204:
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012426,000206: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
012427,000207: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO
012428,000208: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
012429,000209: # R-OTHER, V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
012430,000210: # OTHER VEHICLES COMPUTER.
012431,000211:
012432,000212: # INPUT
012433,000213: # STATE VECTOR IN TEMPORARY STORAGE AREA
012434,000214: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
012435,000215: # SET X2 TO +2
012436,000216: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
012437,000217: # SET X2 TO 0
012438,000218:
012439,000219: # OUTPUT
012440,000220: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
012441,000221: # OR
012442,000222: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
012443,000223:
012444,000224: 23,2155 BANK 23
012445,000225: 10,2000 SETLOC COMGEOM2
012446,000226: 10,2000 BANK
012447,000227: 10,2237 COUNT 10/GEOM
012448,000228: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
012449,000229: 10,2240 04756 AVEMIDSW
012450,000230: 10,2241 20242 +1
012451,000231: 10,2242 53775 VLOAD VSL*
012452,000232: 10,2243 01521 TDELTAV
012453,000233: 10,2244 57605 0 -7,2
012454,000234: 10,2245 53655 VAD VSL*
012455,000235: 10,2246 01535 RCV
012456,000236: 10,2247 57576 0,2
012457,000237: 10,2250 25171 STOVL RN
012458,000238: 10,2251 01527 TNUV
012459,000239: 10,2252 53257 VSL* VAD
012460,000240: 10,2253 57602 0 -4,2
012461,000241: 10,2254 01543 VCV
012462,000242: 10,2255 77657 VSL*
012463,000243: 10,2256 57576 0,2
012464,000244: 10,2257 15177 STODL VN
012465,000245: 10,2260 01517 TET
012466,000246: 10,2261 01205 STORE PIPTIME
012467,000247: 10,2262 77616 RVQ
012468,000248: 10,2263 53775 SVDWN2 VLOAD VSL*
012469,000249: 10,2264 01521 TDELTAV
012470,000250: 10,2265 57605 0 -7,2
012471,000251: 10,2266 53655 VAD VSL*
012472,000252: 10,2267 01535 RCV
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012474,000254: 10,2270 57576 0,2
012475,000255: 10,2271 25722 STOVL R-OTHER
012476,000256: 10,2272 01527 TNUV
012477,000257: 10,2273 53257 VSL* VAD
012478,000258: 10,2274 57602 0 -4,2
012479,000259: 10,2275 01543 VCV
012480,000260: 10,2276 77657 VSL*
012481,000261: 10,2277 57576 0,2
012482,000262: 10,2300 01730 STORE V-OTHER
012483,000263: 10,2301 77616 RVQ
012484,000264:
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012486,000266: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
012487,000267:
012488,000268: # ENTRY: CALL
012489,000269: # LOG
012490,000270:
012491,000271: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
012492,000272:
012493,000273: # EBANK IS ARBITRARY..
012494,000274:
012495,000275: 14,2000 BANK 14
012496,000276: 23,2000 SETLOC POWFLIT2
012497,000277: 23,2000 BANK
012498,000278: 23,2155 COUNT 23/GEOM
012499,000279:
012500,000280: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
012501,000281: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
012502,000282: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
012503,000283: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
012504,000284: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
012505,000285: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
012506,000286: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
012507,000287: 23,2165 01001 14636 2DEC .031335467
012508,000288: 23,2167 00325 07310 2DEC .0130145859
012509,000289: 23,2171 00541 16735 2DEC .0215738898
012510,000290:
012511,000291: 23,2173 34714 CAF ZERO
012512,000292: 23,2174 54156 TS MPAC +2
012513,000293: 23,2175 00006 EXTEND
012514,000294: 23,2176 32214 DCA CLOG2/32
012515,000295: 23,2177 52155 DXCH MPAC
012516,000296: 23,2200 52160 DXCH MPAC +3
012517,000297: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
012518,000298: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
012519,000299:
012520,000300: 23,2203 52156 DXCH MPAC +1
012521,000301: 23,2204 52155 DXCH MPAC
012522,000302: 23,2205 52160 DXCH MPAC +3
012523,000303: 23,2206 20155 DAS MPAC
012524,000304: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
012525,000305:
012526,000306: 23,2210 77616 RVQ
012527,000307:
012528,000308: 23,2211 37777 37777 NEARLY1 2DEC .999999999
012529,000309:
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Page 287 |
012531,000311: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494
012532,000312:
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012534,000314: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
012535,000315: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
012536,000316: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
012537,000317:
012538,000318: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
012539,000319: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
012540,000320: # AND NORMAL COMPONENTS RTEAST AND RTNORM. INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
012541,000321: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
012542,000322: # TARGET VECTOR RT. ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
012543,000323: # THE EQUATIONS ARE
012544,000324: # - - - -
012545,000325: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT)
012546,000326:
012547,000327: # WHERE WT = WIE DTEAROT
012548,000328:
012549,000329: # RTINIT = INITIAL TARGET VECTOR
012550,000330: # - - -
012551,000331: # RTEAST = UNITW * RTINIT
012552,000332: # - - -
012553,000333: # RTNORM = RTEAST * UNITW
012554,000334:
012555,000335: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
012556,000336: #
012557,000337: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
012558,000338: # STCALL DTEAROT STCALL DTEAROT
012559,000339: # EARROT1 EARROT2
012560,000340: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
012561,000341: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
012562,000342:
012563,000343: # SUBROUTINES USED: NONE
012564,000344:
012565,000345: # NORMAL EXIT MODES: RVQ
012566,000346:
012567,000347: # ALARMS: NONE
012568,000348:
012569,000349: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
012570,000350: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
012571,000351: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
012572,000352: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
012573,000353:
012574,000354: # ERASABLE INITIALIZATION REQUIRED:
012575,000355: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
012576,000356: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
012577,000357: # DTEAROT (-28) CS TIME OF FLIGHT LEFT BY CALLER
012578,000358:
012579,000359: # DEBRIS: QPRET, PDL+0 ... PDL+5
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012581,000361: 23,2215 E7,1451 EBANK= RTINIT
012582,000362:
012583,000363: 23,2215 47375 EARROT1 VLOAD VXV
012584,000364: 23,2216 01714 UNITW # FULL UNIT VECTOR
012585,000365: 23,2217 03452 RTINIT # .5 UNIT
012586,000366: 23,2220 03460 STORE RTEAST # .5 UNIT
012587,000367:
012588,000368: 23,2221 77635 VXV
012589,000369: 23,2222 01714 UNITW # FULL UNIT
012590,000370: 23,2223 17466 STODL RTNORM # .5 UNIT
012591,000371: 23,2224 03606 DTEAROT # (-28) CS
012592,000372:
012593,000373: 23,2225 56204 EARROT2 BOVB DDV
012594,000374: 23,2226 57343 TCDANZIG # RESET OVFIND, IF ON
012595,000375: 23,2227 06256 1/WIE
012596,000376: 23,2230 41400 BOV PUSH
012597,000377: 23,2231 46245 OVERADAY
012598,000378: 23,2232 45346 COS DSU
012599,000379: 23,2233 15330 HIDPHALF
012600,000380: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST
012601,000381: 23,2235 03466 RTNORM # .5 UNIT
012602,000382: 23,2236 74356 SIN VXSC
012603,000383: 23,2237 03460 RTEAST # .5 UNIT
012604,000384: 23,2240 76455 VAD VSL1
012605,000385: 23,2241 53455 VAD UNIT # INSURE THAT RT IS 'UNIT'.
012606,000386: 23,2242 03452 RTINIT # .5 UNIT
012607,000387: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR
012608,000388:
012609,000389: 23,2244 77616 RVQ
012610,000390:
012611,000391: 23,2245 75345 OVERADAY DLOAD SIGN
012612,000392: 23,2246 06256 1/WIE
012613,000393: 23,2247 03606 DTEAROT
012614,000394: 23,2250 77621 BDSU
012615,000395: 23,2251 03606 DTEAROT
012616,000396: 23,2252 03606 STORE DTEAROT
012617,000397:
012618,000398: 23,2253 77650 GOTO
012619,000399: 23,2254 46225 EARROT2
012620,000400:
012621,000401: # WIE 2DEC .1901487997
012622,000402: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28
012623,000403: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1
012624,000404: 23,2261 00000 00000 2DEC 0 B-28
012625,000405: 23,2263 67313 65307 2DEC -.5376381241 B-1
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Page 290 |
012627,000407: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28
012628,000408: 23,2267 20000 00000 HALFNFLT 2DEC .5
012629,000409: 23,2271 00000 00000 2DEC 0 B-28
012630,000410: 23,2273 10464 12470 2DEC +.5376381241 B-1
012631,000411: 23,2275 00000 00000 2DEC 0 B-28
012632,000412: 23,2277 15373 11346 2DEC +.8431756920 B-1
012633,000413: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1
012634,000414: 23,2303 00000 00000 2DEC 0 B-28
012635,000415: 23,2305 10464 12470 2DEC +.5376381241 B-1
012636,000416: 23,2307 00000 00000 2DEC 0 B-28
012637,000417: 23,2311 20000 00000 2DEC .5
012638,000418: 23,2313 00000 00000 2DEC 0 B-28
012639,000419: 23,2315 67313 65307 2DEC -.5376381241 B-1
012640,000420: 23,2317 00000 00000 2DEC 0 B-28
012641,000421: 23,2321 15373 11346 2DEC +.8431756920 B-1
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Page 291 |
012643,000423: 23,2323 07020 10DEGS- DEC 3600 B-14
012644,000424: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 2S COMP.
012645,000425: 23,2325 00000 OCT 00000
012646,000426: 23,2326 61740 20DEGS- DEC -07199 B-14
012647,000427: 23,2327 77777 DEC -00000 B-14
012648,000428: 23,2330 07020 20DEG- DEC 03600 B-14
012649,000429: 23,2331 00000 DEC 00000 B-14
012650,000430:
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc