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A scan by Ron Burkey has superceded it, made from a more-legible copy from the collection of original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. |
012230,000002: ## Copyright: Public domain.
012231,000003: ## Filename: CSM_GEOMETRY.agc
012232,000004: ## Purpose: Part of the source code for Colossus, build 249.
012233,000005: ## It is part of the source code for the Command Module's (CM)
012234,000006: ## Apollo Guidance Computer (AGC), for Apollo 9.
012235,000007: ## Assembler: yaYUL
012236,000008: ## Reference: pp. 280-291.
012237,000009: ## Contact: Ron Burkey <info@sandroid.org>.
012238,000010: ## Website: www.ibiblio.org/apollo.
012239,000011: ## Mod history: 08/08/04 RSB. Began transcribing.
012240,000012: ## 2017-01-05 RSB Page numbers now agree with those on the
012241,000013: ## original harcopy, as opposed to the PDF page
012242,000014: ## numbers in 1701.pdf.
012243,000015: ## 2017-01-07 RSB Cross-diff'd comment text (not whitespace)
012244,000016: ## vs the already-proofed corresponding Colossus
012245,000017: ## 237 and Comanche 55 source-code files
012246,000018: ## and corrected errors found.
012247,000019: ## 2017-01-28 RSB WTIH -> WITH.
012248,000020: ##
012249,000021: ## The contents of the "Colossus249" files, in general, are transcribed
012250,000022: ## from a scanned copy of the program listing. Notations on this
012251,000023: ## document read, in part:
012252,000024: ##
012253,000025: ## Assemble revision 249 of AGC program Colossus by NASA
012254,000026: ## 2021111-041. October 28, 1968.
012255,000027: ##
012256,000028: ## This AGC program shall also be referred to as
012257,000029: ## Colossus 1A
012258,000030: ##
012259,000031: ## Prepared by
012260,000032: ## Massachusetts Institute of Technology
012261,000033: ## 75 Cambridge Parkway
012262,000034: ## Cambridge, Massachusetts
012263,000035: ## under NASA contract NAS 9-4065.
012264,000036: ##
012265,000037: ## Refer directly to the online document mentioned above for further information.
012266,000038: ## Please report any errors (relative to the scanned pages) to info@sandroid.org.
012267,000039: ##
012268,000040: ## In some cases, where the source code for Luminary 131 overlaps that of
012269,000041: ## Colossus 249, this code is instead copied from the corresponding Luminary 131
012270,000042: ## source file, and then is proofed to incorporate any changes.
012271,000043:
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012273,000045: 22,2000 BANK 22
012274,000046: 23,2000 SETLOC COMGEOM1
012275,000047: 23,2000 BANK
012276,000048:
012277,000049: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
012278,000050: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
012279,000051:
012280,000052: # THE INPUTS ARE 1) THE SEXTANT SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
012281,000053: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
012282,000054: # JOB VAC AREA.
012283,000055:
012284,000056: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
012285,000057: # OUTPUT IS ALSO AVAILABLE AT MPAC.
012286,000058:
012287,000059: 23,2000 COUNT 23/GEOM
012288,000060:
012289,000061: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
012290,000062: 23,2001 00006 5,1 # TRUNNION = TA
012291,000063: 23,2002 45510 CDULOGIC
012292,000064: 23,2003 41434 RTB PUSH
012293,000065: 23,2004 46027 SXTLOGIC
012294,000066: 23,2005 72556 SIN SL1
012295,000067: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
012296,000068: 23,2007 00004 3,1 # SHAFT = SA
012297,000069: 23,2010 41434 RTB PUSH # PD4 = SA
012298,000070: 23,2011 45510 CDULOGIC
012299,000071:
012300,000072: 23,2012 41346 COS DMP
012301,000073: 23,2013 00003 2
012302,000074: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
012303,000075:
012304,000076: 23,2015 41356 SIN DMP
012305,000077: 23,2016 77626 STADR
012306,000078: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
012307,000079:
012308,000080: 23,2020 77746 COS
012309,000081: 23,2021 24045 STOVL STARM +4
012310,000082: 23,2022 00041 STARM # STARM = 32D
012311,000083: 23,2023 76521 MXV VSL1
012312,000084: 23,2024 06302 NB1NB2
012313,000085: 23,2025 00041 STORE 32D
012314,000086: 23,2026 77616 RVQ
012315,000087: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
012316,000088: 23,2030 26154 ADS MPAC
012317,000089: 23,2031 34676 CAF QUARTER
012318,000090: 23,2032 07256 TC SHORTMP
012319,000091: 23,2033 06030 TC DANZIG
012320,000092:
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012322,000094: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
012323,000095: # OF-SIGHT LIES ALONG THE STAR VECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
012324,000096: # ERENCED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
012325,000097: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
012326,000098:
012327,000099: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO PRESENT STABLE MEMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
012328,000100: # INPUT AS *SMNB*, I.E. SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
012329,000101: # TO CDUTRIG WILL PROVIDE THIS INPUT.
012330,000102:
012331,000103: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012332,000104: # EQUAL TO ZERO).
012333,000105:
012334,000106: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D
012335,000107: 23,2035 00034 28D
012336,000108: 23,2036 02766 STAR
012337,000109: 23,2037 77624 CALL
012338,000110: 23,2040 47577 *SMNB*
012339,000111: 23,2041 76521 MXV VSL1
012340,000112: 23,2042 06260 NB2NB1
012341,000113: 23,2043 26766 STOVL STAR
012342,000114: 23,2044 15330 HIUNITX
012343,000115: 23,2045 26555 STOVL XNB1
012344,000116: 23,2046 15326 HIUNITY
012345,000117: 23,2047 26563 STOVL YNB1
012346,000118: 23,2050 15324 HIUNITZ
012347,000119: 23,2051 36571 STCALL ZNB1
012348,000120: 23,2052 46076 SXTANG1
012349,000121:
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012351,000123: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
012352,000124: # SIGHT LIES ALONG THE STAR VECTOR.
012353,000125:
012354,000126: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
012355,000127: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB,AND
012356,000128: # ZNB.
012357,000129:
012358,000130: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012359,000131: # EQUAL TO ZERO).
012360,000132:
012361,000133: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
012362,000134: 23,2054 00034 28D
012363,000135: 23,2055 45657 TRANSP1 # EREF WRT NB2
012364,000136: 23,2056 64375 VLOAD MXV
012365,000137: 23,2057 02714 XNB
012366,000138: 23,2060 06260 NB2NB1
012367,000139: 23,2061 77772 VSL1
012368,000140: 23,2062 26555 STOVL XNB1
012369,000141: 23,2063 02722 YNB
012370,000142: 23,2064 76521 MXV VSL1
012371,000143: 23,2065 06260 NB2NB1
012372,000144: 23,2066 26563 STOVL YNB1
012373,000145: 23,2067 02730 ZNB
012374,000146: 23,2070 76521 MXV VSL1
012375,000147: 23,2071 06260 NB2NB1
012376,000148: 23,2072 02571 STORE ZNB1
012377,000149:
012378,000150: 23,2073 47034 RTB RTB
012379,000151: 23,2074 45657 TRANSP1
012380,000152: 23,2075 45673 TRANSP2
012381,000153:
012382,000154: 23,2076 47375 SXTANG1 VLOAD VXV
012383,000155: 23,2077 02571 ZNB1
012384,000156: 23,2100 02766 STAR
012385,000157: 23,2101 77600 BOV
012386,000158: 23,2102 46103 +1
012387,000159: 23,2103 40056 UNIT BOV
012388,000160: 23,2104 46145 ZNB=S1
012389,000161: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
012390,000162:
012391,000163: 23,2106 57441 DOT DCOMP
012392,000164: 23,2107 02555 XNB1
012393,000165: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
012394,000166: 23,2111 00027 PDA
012395,000167:
012396,000168: 23,2112 77641 DOT
012397,000169: 23,2113 02563 YNB1
012398,000170: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
012399,000171: 23,2115 47211 ARCTRIG
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012401,000173: 23,2116 77634 RTB
012402,000174: 23,2117 45543 1STO2S
012403,000175: 23,2120 26774 STOVL SAC
012404,000176: 23,2121 02766 STAR
012405,000177: 23,2122 77600 BOV
012406,000178: 23,2123 46124 +1
012407,000179: 23,2124 72441 DOT SL1
012408,000180: 23,2125 02571 ZNB1
012409,000181: 23,2126 77726 ACOS
012410,000182: 23,2127 62440 BMN SL2
012411,000183: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
012412,000184: 23,2131 45200 BOV DSU
012413,000185: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
012414,000186: 23,2133 06331 20DEG-
012415,000187: 23,2134 77634 RTB
012416,000188: 23,2135 45543 1STO2S
012417,000189: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
012418,000190: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEG
012419,000191: 23,2140 01630 CULTFLAG
012420,000192: 23,2141 00034 28D
012421,000193: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
012422,000194: 23,2143 01430 CULTFLAG
012423,000195: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI
012424,000196: 23,2145 77745 ZNB=S1 DLOAD
012425,000197: 23,2146 06325 270DEG
012426,000198: 23,2147 16774 STODL SAC
012427,000199: 23,2150 06327 20DEGS-
012428,000200: 23,2151 02776 STORE PAC
012429,000201: 23,2152 77614 CLRGO
012430,000202: 23,2153 01630 CULTFLAG
012431,000203: 23,2154 00034 28D
012432,000204:
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012434,000206: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
012435,000207: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO
012436,000208: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
012437,000209: # R-OTHER, V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
012438,000210: # OTHER VEHICLES COMPUTER.
012439,000211:
012440,000212: # INPUT
012441,000213: # STATE VECTOR IN TEMPORARY STORAGE AREA
012442,000214: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
012443,000215: # SET X2 TO +2
012444,000216: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
012445,000217: # SET X2 TO 0
012446,000218:
012447,000219: # OUTPUT
012448,000220: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
012449,000221: # OR
012450,000222: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
012451,000223:
012452,000224: 23,2155 BANK 23
012453,000225: 10,2000 SETLOC COMGEOM2
012454,000226: 10,2000 BANK
012455,000227: 10,2237 COUNT 10/GEOM
012456,000228: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
012457,000229: 10,2240 04756 AVEMIDSW
012458,000230: 10,2241 20242 +1
012459,000231: 10,2242 53775 VLOAD VSL*
012460,000232: 10,2243 01521 TDELTAV
012461,000233: 10,2244 57605 0 -7,2
012462,000234: 10,2245 53655 VAD VSL*
012463,000235: 10,2246 01535 RCV
012464,000236: 10,2247 57576 0,2
012465,000237: 10,2250 25171 STOVL RN
012466,000238: 10,2251 01527 TNUV
012467,000239: 10,2252 53257 VSL* VAD
012468,000240: 10,2253 57602 0 -4,2
012469,000241: 10,2254 01543 VCV
012470,000242: 10,2255 77657 VSL*
012471,000243: 10,2256 57576 0,2
012472,000244: 10,2257 15177 STODL VN
012473,000245: 10,2260 01517 TET
012474,000246: 10,2261 01205 STORE PIPTIME
012475,000247: 10,2262 77616 RVQ
012476,000248: 10,2263 53775 SVDWN2 VLOAD VSL*
012477,000249: 10,2264 01521 TDELTAV
012478,000250: 10,2265 57605 0 -7,2
012479,000251: 10,2266 53655 VAD VSL*
012480,000252: 10,2267 01535 RCV
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012482,000254: 10,2270 57576 0,2
012483,000255: 10,2271 25722 STOVL R-OTHER
012484,000256: 10,2272 01527 TNUV
012485,000257: 10,2273 53257 VSL* VAD
012486,000258: 10,2274 57602 0 -4,2
012487,000259: 10,2275 01543 VCV
012488,000260: 10,2276 77657 VSL*
012489,000261: 10,2277 57576 0,2
012490,000262: 10,2300 01730 STORE V-OTHER
012491,000263: 10,2301 77616 RVQ
012492,000264:
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012494,000266: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
012495,000267:
012496,000268: # ENTRY: CALL
012497,000269: # LOG
012498,000270:
012499,000271: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
012500,000272:
012501,000273: # EBANK IS ARBITRARY..
012502,000274:
012503,000275: 14,2000 BANK 14
012504,000276: 23,2000 SETLOC POWFLIT2
012505,000277: 23,2000 BANK
012506,000278: 23,2155 COUNT 23/GEOM
012507,000279:
012508,000280: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
012509,000281: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
012510,000282: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
012511,000283: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
012512,000284: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
012513,000285: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
012514,000286: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
012515,000287: 23,2165 01001 14636 2DEC .031335467
012516,000288: 23,2167 00325 07310 2DEC .0130145859
012517,000289: 23,2171 00541 16735 2DEC .0215738898
012518,000290:
012519,000291: 23,2173 34714 CAF ZERO
012520,000292: 23,2174 54156 TS MPAC +2
012521,000293: 23,2175 00006 EXTEND
012522,000294: 23,2176 32214 DCA CLOG2/32
012523,000295: 23,2177 52155 DXCH MPAC
012524,000296: 23,2200 52160 DXCH MPAC +3
012525,000297: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
012526,000298: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
012527,000299:
012528,000300: 23,2203 52156 DXCH MPAC +1
012529,000301: 23,2204 52155 DXCH MPAC
012530,000302: 23,2205 52160 DXCH MPAC +3
012531,000303: 23,2206 20155 DAS MPAC
012532,000304: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
012533,000305:
012534,000306: 23,2210 77616 RVQ
012535,000307:
012536,000308: 23,2211 37777 37777 NEARLY1 2DEC .999999999
012537,000309:
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Page 287 |
012539,000311: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494
012540,000312:
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012542,000314: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
012543,000315: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
012544,000316: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
012545,000317:
012546,000318: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
012547,000319: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
012548,000320: # AND NORMAL COMPONENTS RTEAST AND RTNORM. INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
012549,000321: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
012550,000322: # TARGET VECTOR RT. ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
012551,000323: # THE EQUATIONS ARE
012552,000324: # - - - -
012553,000325: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT)
012554,000326:
012555,000327: # WHERE WT = WIE DTEAROT
012556,000328:
012557,000329: # RTINIT = INITIAL TARGET VECTOR
012558,000330: # - - -
012559,000331: # RTEAST = UNITW * RTINIT
012560,000332: # - - -
012561,000333: # RTNORM = RTEAST * UNITW
012562,000334:
012563,000335: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
012564,000336: #
012565,000337: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
012566,000338: # STCALL DTEAROT STCALL DTEAROT
012567,000339: # EARROT1 EARROT2
012568,000340: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
012569,000341: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
012570,000342:
012571,000343: # SUBROUTINES USED: NONE
012572,000344:
012573,000345: # NORMAL EXIT MODES: RVQ
012574,000346:
012575,000347: # ALARMS: NONE
012576,000348:
012577,000349: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
012578,000350: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
012579,000351: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
012580,000352: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
012581,000353:
012582,000354: # ERASABLE INITIALIZATION REQUIRED:
012583,000355: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
012584,000356: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
012585,000357: # DTEAROT (-28) CS TIME OF FLIGHT LEFT BY CALLER
012586,000358:
012587,000359: # DEBRIS: QPRET, PDL+0 ... PDL+5
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012589,000361: 23,2215 E7,1451 EBANK= RTINIT
012590,000362:
012591,000363: 23,2215 47375 EARROT1 VLOAD VXV
012592,000364: 23,2216 01714 UNITW # FULL UNIT VECTOR
012593,000365: 23,2217 03452 RTINIT # .5 UNIT
012594,000366: 23,2220 03460 STORE RTEAST # .5 UNIT
012595,000367:
012596,000368: 23,2221 77635 VXV
012597,000369: 23,2222 01714 UNITW # FULL UNIT
012598,000370: 23,2223 17466 STODL RTNORM # .5 UNIT
012599,000371: 23,2224 03606 DTEAROT # (-28) CS
012600,000372:
012601,000373: 23,2225 56204 EARROT2 BOVB DDV
012602,000374: 23,2226 57343 TCDANZIG # RESET OVFIND, IF ON
012603,000375: 23,2227 06256 1/WIE
012604,000376: 23,2230 41400 BOV PUSH
012605,000377: 23,2231 46245 OVERADAY
012606,000378: 23,2232 45346 COS DSU
012607,000379: 23,2233 15330 HIDPHALF
012608,000380: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST
012609,000381: 23,2235 03466 RTNORM # .5 UNIT
012610,000382: 23,2236 74356 SIN VXSC
012611,000383: 23,2237 03460 RTEAST # .5 UNIT
012612,000384: 23,2240 76455 VAD VSL1
012613,000385: 23,2241 53455 VAD UNIT # INSURE THAT RT IS 'UNIT'.
012614,000386: 23,2242 03452 RTINIT # .5 UNIT
012615,000387: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR
012616,000388:
012617,000389: 23,2244 77616 RVQ
012618,000390:
012619,000391: 23,2245 75345 OVERADAY DLOAD SIGN
012620,000392: 23,2246 06256 1/WIE
012621,000393: 23,2247 03606 DTEAROT
012622,000394: 23,2250 77621 BDSU
012623,000395: 23,2251 03606 DTEAROT
012624,000396: 23,2252 03606 STORE DTEAROT
012625,000397:
012626,000398: 23,2253 77650 GOTO
012627,000399: 23,2254 46225 EARROT2
012628,000400:
012629,000401: # WIE 2DEC .1901487997
012630,000402: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28
012631,000403: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1
012632,000404: 23,2261 00000 00000 2DEC 0 B-28
012633,000405: 23,2263 67313 65307 2DEC -.5376381241 B-1
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Page 290 |
012635,000407: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28
012636,000408: 23,2267 20000 00000 HALFNFLT 2DEC .5
012637,000409: 23,2271 00000 00000 2DEC 0 B-28
012638,000410: 23,2273 10464 12470 2DEC +.5376381241 B-1
012639,000411: 23,2275 00000 00000 2DEC 0 B-28
012640,000412: 23,2277 15373 11346 2DEC +.8431756920 B-1
012641,000413: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1
012642,000414: 23,2303 00000 00000 2DEC 0 B-28
012643,000415: 23,2305 10464 12470 2DEC +.5376381241 B-1
012644,000416: 23,2307 00000 00000 2DEC 0 B-28
012645,000417: 23,2311 20000 00000 2DEC .5
012646,000418: 23,2313 00000 00000 2DEC 0 B-28
012647,000419: 23,2315 67313 65307 2DEC -.5376381241 B-1
012648,000420: 23,2317 00000 00000 2DEC 0 B-28
012649,000421: 23,2321 15373 11346 2DEC +.8431756920 B-1
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Page 291 |
012651,000423: 23,2323 07020 10DEGS- DEC 3600 B-14
012652,000424: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 2S COMP.
012653,000425: 23,2325 00000 OCT 00000
012654,000426: 23,2326 61740 20DEGS- DEC -07199 B-14
012655,000427: 23,2327 77777 DEC -00000 B-14
012656,000428: 23,2330 07020 20DEG- DEC 03600 B-14
012657,000429: 23,2331 00000 DEC 00000 B-14
012658,000430:
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc