GAP: ASSEMBLE REVISION 237 OF AGC PROGRAM COLOSSUS BY NASA 2021111-031 1:17 AUG. 24, 1968Note 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 derived from scans of the
Colossus 237 (Apollo 8 Command Module) program listing from the private collection of original
AGC developer Fred Martin. Scanning was by Ron Burkey. Pre-existing Colossus 249
(Apollo 9 CM) source files were used as a template, and changes between Colossus 249
and Colossus 237 were manually transcribed by a team of volunteers. Note
that the page images
presented online are of reduced quality, and that additional 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 237 OF AGC PROGRAM COLOSSUS BY NASA 2021111-031 1:17 AUG. 24, 1968Note that the date is the date of the printout, not the date of the program revision. |
012157,000002: ## Copyright: Public domain.
012158,000003: ## Filename: CSM_GEOMETRY.agc
012159,000004: ## Purpose: Part of the source code for Colossus build 237.
012160,000005: ## This is for the Command Module's (CM) Apollo Guidance
012161,000006: ## Computer (AGC), for Apollo 8.
012162,000007: ## Assembler: yaYUL
012163,000008: ## Contact: Onno Hommes <ohommes@alumni.cmu.edu>
012164,000009: ## Website: www.ibiblio.org/apollo/index.html
012165,000010: ## Page Scans: www.ibiblio.org/apollo/ScansForConversion/Colossus237/
012166,000011: ## Mod history: 2010-05-30 OH Adapted from corresponding Colossus 249 file.
012167,000012: ## 2010-12-04 JL Remove Colossus 249 header comments. Change to double-hash page numbers.
012168,000013: ## 2010-01-16 JL Minor fixes.
012169,000014: ## 2016-12-30 RSB Proofed comment text using octopus/ProoferComments,
012170,000015: ## and corrected errors found.
012171,000016: ## 2017-01-28 RSB WTIH -> WITH.
012172,000017:
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012174,000019: 22,2000 BANK 22
012175,000020: 23,2000 SETLOC COMGEOM1
012176,000021: 23,2000 BANK
012177,000022:
012178,000023: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
012179,000024: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
012180,000025:
012181,000026: # THE INPUTS ARE 1) THE SEXTANT SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
012182,000027: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
012183,000028: # JOB VAC AREA.
012184,000029:
012185,000030: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
012186,000031: # OUTPUT IS ALSO AVAILABLE AT MPAC.
012187,000032:
012188,000033:
012189,000034: 23,2000 COUNT 23/GEOM
012190,000035:
012191,000036: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
012192,000037: 23,2001 00006 5,1 # TRUNNION = TA
012193,000038: 23,2002 45510 CDULOGIC
012194,000039: 23,2003 41434 RTB PUSH
012195,000040: 23,2004 46027 SXTLOGIC
012196,000041: 23,2005 72556 SIN SL1
012197,000042: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
012198,000043: 23,2007 00004 3,1 # SHAFT = SA
012199,000044: 23,2010 41434 RTB PUSH # PD4 = SA
012200,000045: 23,2011 45510 CDULOGIC
012201,000046:
012202,000047: 23,2012 41346 COS DMP
012203,000048: 23,2013 00003 2
012204,000049: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
012205,000050:
012206,000051: 23,2015 41356 SIN DMP
012207,000052: 23,2016 77626 STADR
012208,000053: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
012209,000054:
012210,000055: 23,2020 77746 COS
012211,000056: 23,2021 24045 STOVL STARM +4
012212,000057: 23,2022 00041 STARM # STARM = 32D
012213,000058: 23,2023 76521 MXV VSL1
012214,000059: 23,2024 06302 NB1NB2
012215,000060: 23,2025 00041 STORE 32D
012216,000061: 23,2026 77616 RVQ
012217,000062:
012218,000063:
012219,000064: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
012220,000065: 23,2030 26154 ADS MPAC
012221,000066: 23,2031 34676 CAF QUARTER
012222,000067: 23,2032 07256 TC SHORTMP
012223,000068: 23,2033 06030 TC DANZIG
012224,000069:
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012226,000071:
012227,000072: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
012228,000073: # OF-SIGHT LIES ALONG THE STAR VECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
012229,000074: # ERENCED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
012230,000075: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
012231,000076:
012232,000077: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO PRESENT STABLE MEMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
012233,000078: # INPUT AS *SMNB*, I.E. SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
012234,000079: # TO CDUTRIG WILL PROVIDE THIS INPUT.
012235,000080:
012236,000081: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012237,000082: # EQUAL TO ZERO).
012238,000083:
012239,000084:
012240,000085: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D,28D,30D,32D-36D
012241,000086: 23,2035 00034 28D
012242,000087: 23,2036 02766 STAR
012243,000088: 23,2037 77624 CALL
012244,000089: 23,2040 47577 *SMNB*
012245,000090: 23,2041 76521 MXV VSL1
012246,000091: 23,2042 06260 NB2NB1
012247,000092: 23,2043 26766 STOVL STAR
012248,000093: 23,2044 15330 HIUNITX
012249,000094: 23,2045 26555 STOVL XNB1
012250,000095: 23,2046 15326 HIUNITY
012251,000096: 23,2047 26563 STOVL YNB1
012252,000097: 23,2050 15324 HIUNITZ
012253,000098: 23,2051 36571 STCALL ZNB1
012254,000099: 23,2052 46076 SXTANG1
012255,000100:
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012257,000102:
012258,000103: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
012259,000104: # SIGHT LIES ALONG THE STAR VECTOR.
012260,000105:
012261,000106: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
012262,000107: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB, AND
012263,000108: # ZNB.
012264,000109:
012265,000110: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012266,000111: # EQUAL TO ZERO).
012267,000112:
012268,000113:
012269,000114: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
012270,000115: 23,2054 00034 28D
012271,000116: 23,2055 45657 TRANSP1 # EREF WRT NB2
012272,000117: 23,2056 64375 VLOAD MXV
012273,000118: 23,2057 02714 XNB
012274,000119: 23,2060 06260 NB2NB1
012275,000120: 23,2061 77772 VSL1
012276,000121: 23,2062 26555 STOVL XNB1
012277,000122: 23,2063 02722 YNB
012278,000123: 23,2064 76521 MXV VSL1
012279,000124: 23,2065 06260 NB2NB1
012280,000125: 23,2066 26563 STOVL YNB1
012281,000126: 23,2067 02730 ZNB
012282,000127: 23,2070 76521 MXV VSL1
012283,000128: 23,2071 06260 NB2NB1
012284,000129: 23,2072 02571 STORE ZNB1
012285,000130:
012286,000131: 23,2073 47034 RTB RTB
012287,000132: 23,2074 45657 TRANSP1
012288,000133: 23,2075 45673 TRANSP2
012289,000134:
012290,000135: 23,2076 47375 SXTANG1 VLOAD VXV
012291,000136: 23,2077 02571 ZNB1
012292,000137: 23,2100 02766 STAR
012293,000138: 23,2101 77600 BOV
012294,000139: 23,2102 46103 +1
012295,000140: 23,2103 40056 UNIT BOV
012296,000141: 23,2104 46145 ZNB=S1
012297,000142: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
012298,000143:
012299,000144: 23,2106 57441 DOT DCOMP
012300,000145: 23,2107 02555 XNB1
012301,000146: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
012302,000147: 23,2111 00027 PDA
012303,000148:
012304,000149: 23,2112 77641 DOT
012305,000150: 23,2113 02563 YNB1
012306,000151: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
012307,000152: 23,2115 47211 ARCTRIG
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012309,000154: 23,2116 77634 RTB
012310,000155: 23,2117 45543 1STO2S
012311,000156: 23,2120 26774 STOVL SAC
012312,000157: 23,2121 02766 STAR
012313,000158: 23,2122 77600 BOV
012314,000159: 23,2123 46124 +1
012315,000160: 23,2124 72441 DOT SL1
012316,000161: 23,2125 02571 ZNB1
012317,000162: 23,2126 77726 ACOS
012318,000163: 23,2127 62440 BMN SL2
012319,000164: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
012320,000165: 23,2131 45200 BOV DSU
012321,000166: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
012322,000167: 23,2133 06331 20DEG-
012323,000168: 23,2134 77634 RTB
012324,000169: 23,2135 45543 1STO2S
012325,000170: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
012326,000171: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEG
012327,000172: 23,2140 01630 CULTFLAG
012328,000173: 23,2141 00034 28D
012329,000174: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
012330,000175: 23,2143 01430 CULTFLAG
012331,000176: 23,2144 00034 28D # SUBROUTINE,ALARM WILL BE SET BY MPI
012332,000177: 23,2145 77745 ZNB=S1 DLOAD
012333,000178: 23,2146 06325 270DEG
012334,000179: 23,2147 16774 STODL SAC
012335,000180: 23,2150 06327 20DEGS-
012336,000181: 23,2151 02776 STORE PAC
012337,000182: 23,2152 77614 CLRGO
012338,000183: 23,2153 01630 CULTFLAG
012339,000184: 23,2154 00034 28D
012340,000185:
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012342,000187:
012343,000188: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
012344,000189: # THE CONIC R,V AND THE DEVIATIONSR,V. THE STATE VECTORS ARE CONVERTED TO
012345,000190: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
012346,000191: # R-OTHER , V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
012347,000192: # OTHER VEHICLES COMPUTER.
012348,000193:
012349,000194: # INPUT
012350,000195: # STATE VECTOR IN TEMPORARY STORAGE AREA
012351,000196: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
012352,000197: # SET X2 TO +2
012353,000198: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
012354,000199: # SET X2 TO 0
012355,000200:
012356,000201: # OUTPUT
012357,000202: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
012358,000203: # OR
012359,000204: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
012360,000205:
012361,000206:
012362,000207: 23,2155 BANK 23
012363,000208: 10,2000 SETLOC COMGEOM2
012364,000209: 10,2000 BANK
012365,000210: 10,2237 COUNT 10/GEOM
012366,000211: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
012367,000212: 10,2240 04756 AVEMIDSW
012368,000213: 10,2241 20242 +1
012369,000214: 10,2242 53775 VLOAD VSL*
012370,000215: 10,2243 01521 TDELTAV
012371,000216: 10,2244 57605 0 -7,2
012372,000217: 10,2245 53655 VAD VSL*
012373,000218: 10,2246 01535 RCV
012374,000219: 10,2247 57576 0,2
012375,000220: 10,2250 25171 STOVL RN
012376,000221: 10,2251 01527 TNUV
012377,000222: 10,2252 53257 VSL* VAD
012378,000223: 10,2253 57602 0 -4,2
012379,000224: 10,2254 01543 VCV
012380,000225: 10,2255 77657 VSL*
012381,000226: 10,2256 57576 0,2
012382,000227: 10,2257 15177 STODL VN
012383,000228: 10,2260 01517 TET
012384,000229: 10,2261 01205 STORE PIPTIME
012385,000230: 10,2262 77616 RVQ
012386,000231:
012387,000232:
012388,000233: 10,2263 53775 SVDWN2 VLOAD VSL*
012389,000234: 10,2264 01521 TDELTAV
012390,000235: 10,2265 57605 0 -7,2
012391,000236: 10,2266 53655 VAD VSL*
012392,000237: 10,2267 01535 RCV
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012394,000239: 10,2270 57576 0,2
012395,000240: 10,2271 25722 STOVL R-OTHER
012396,000241: 10,2272 01527 TNUV
012397,000242: 10,2273 53257 VSL* VAD
012398,000243: 10,2274 57602 0 -4,2
012399,000244: 10,2275 01543 VCV
012400,000245: 10,2276 77657 VSL*
012401,000246: 10,2277 57576 0,2
012402,000247: 10,2300 01730 STORE V-OTHER
012403,000248: 10,2301 77616 RVQ
012404,000249:
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012406,000251:
012407,000252: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
012408,000253:
012409,000254: # ENTRY: CALL
012410,000255: # LOG
012411,000256:
012412,000257: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
012413,000258:
012414,000259: # EBANK IS ARBITRARY..
012415,000260:
012416,000261:
012417,000262: 14,2000 BANK 14
012418,000263: 23,2000 SETLOC POWFLIT2
012419,000264: 23,2000 BANK
012420,000265: 23,2155 COUNT 23/GEOM
012421,000266:
012422,000267: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
012423,000268: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
012424,000269: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
012425,000270: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
012426,000271: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
012427,000272:
012428,000273: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
012429,000274: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
012430,000275: 23,2165 01001 14636 2DEC .031335467
012431,000276: 23,2167 00325 07310 2DEC .0130145859
012432,000277: 23,2171 00541 16735 2DEC .0215738898
012433,000278:
012434,000279: 23,2173 34714 CAF ZERO
012435,000280: 23,2174 54156 TS MPAC +2
012436,000281: 23,2175 00006 EXTEND
012437,000282: 23,2176 32214 DCA CLOG2/32
012438,000283: 23,2177 52155 DXCH MPAC
012439,000284: 23,2200 52160 DXCH MPAC +3
012440,000285: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
012441,000286: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
012442,000287:
012443,000288: 23,2203 52156 DXCH MPAC +1
012444,000289: 23,2204 52155 DXCH MPAC
012445,000290: 23,2205 52160 DXCH MPAC +3
012446,000291: 23,2206 20155 DAS MPAC
012447,000292: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
012448,000293:
012449,000294: 23,2210 77616 RVQ
012450,000295:
012451,000296: 23,2211 37777 37777 NEARLY1 2DEC .999999999
012452,000297:
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012454,000299: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494
012455,000300:
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012457,000302:
012458,000303: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
012459,000304: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
012460,000305: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
012461,000306: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
012462,000307: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
012463,000308: # AND NORMAL COMPONENTS RTEAST AND RTNORM . INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
012464,000309: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
012465,000310: # TARGET VECTOR RT . ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
012466,000311: # THE EQUATIONS ARE
012467,000312: # - - - -
012468,000313: # RT = RTINIT + RTNORM (COS(WT) -1) + RTEAST SIN(WT)
012469,000314: # WHERE WT = WIE DTEAROT
012470,000315: # RTINIT = INITIAL TARGET VECTOR
012471,000316: # - - -
012472,000317: # RTEAST = UNITW*RTINIT
012473,000318: # - - -
012474,000319: # RTNORM = RTEAST*UNITW
012475,000320:
012476,000321: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
012477,000322: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
012478,000323: # STCALL DTEAROT STCALL DTEAROT
012479,000324: # EARROT1 EARROT2
012480,000325: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
012481,000326: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
012482,000327:
012483,000328: # SUBROUTINES USED: NONE
012484,000329: # NORMAL EXIT MODES: RVQ
012485,000330: # ALARMS: NONE
012486,000331: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
012487,000332: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
012488,000333: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
012489,000334: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
012490,000335: # ERASABLE INITIALIZATION REQUIRED:
012491,000336: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
012492,000337: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
012493,000338: # DTEAROT (-28) CS TIME OF FLIGHT LEFT BY CALLER
012494,000339: # DEBRIS: QPRET, PDL+0 ... PDL+5
012495,000340:
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012497,000342:
012498,000343: 23,2215 E7,1451 EBANK= RTINIT
012499,000344:
012500,000345: 23,2215 47375 EARROT1 VLOAD VXV
012501,000346: 23,2216 01714 UNITW # FULL UNIT VECTOR
012502,000347: 23,2217 03452 RTINIT # .5 UNIT
012503,000348: 23,2220 03460 STORE RTEAST # .5 UNIT
012504,000349:
012505,000350: 23,2221 77635 VXV
012506,000351: 23,2222 01714 UNITW # FULL UNIT
012507,000352: 23,2223 17466 STODL RTNORM # .5 UNIT
012508,000353: 23,2224 03606 DTEAROT # (-28) CS
012509,000354:
012510,000355: 23,2225 56204 EARROT2 BOVB DDV
012511,000356: 23,2226 57314 TCDANZIG # RESET OVFIND, IF ON
012512,000357: 23,2227 06256 1/WIE
012513,000358: 23,2230 41400 BOV PUSH
012514,000359: 23,2231 46245 OVERADAY
012515,000360: 23,2232 45346 COS DSU
012516,000361: 23,2233 15330 HIDPHALF
012517,000362: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST
012518,000363: 23,2235 03466 RTNORM # .5 UNIT
012519,000364: 23,2236 74356 SIN VXSC
012520,000365: 23,2237 03460 RTEAST # .5 UNIT
012521,000366: 23,2240 76455 VAD VSL1
012522,000367: 23,2241 53455 VAD UNIT # INSURE THAT RT IS 'UNIT'.
012523,000368: 23,2242 03452 RTINIT # .5 UNIT
012524,000369: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR
012525,000370:
012526,000371: 23,2244 77616 RVQ
012527,000372:
012528,000373: 23,2245 75345 OVERADAY DLOAD SIGN
012529,000374: 23,2246 06256 1/WIE
012530,000375: 23,2247 03606 DTEAROT
012531,000376: 23,2250 77621 BDSU
012532,000377: 23,2251 03606 DTEAROT
012533,000378: 23,2252 03606 STORE DTEAROT
012534,000379:
012535,000380: 23,2253 77650 GOTO
012536,000381: 23,2254 46225 EARROT2
012537,000382:
012538,000383: # WIE 2DEC .1901487997
012539,000384: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28
012540,000385: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1
012541,000386: 23,2261 00000 00000 2DEC 0 B-28
012542,000387: 23,2263 67313 65307 2DEC -.5376381241 B-1
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Page 288 |
012544,000389: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28
012545,000390: 23,2267 20000 00000 HALFNFLT 2DEC .5
012546,000391: 23,2271 00000 00000 2DEC 0 B-28
012547,000392: 23,2273 10464 12470 2DEC +.5376381241 B-1
012548,000393: 23,2275 00000 00000 2DEC 0 B-28
012549,000394: 23,2277 15373 11346 2DEC +.8431756920 B-1
012550,000395:
012551,000396:
012552,000397: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1
012553,000398: 23,2303 00000 00000 2DEC 0 B-28
012554,000399: 23,2305 10464 12470 2DEC +.5376381241 B-1
012555,000400: 23,2307 00000 00000 2DEC 0 B-28
012556,000401: 23,2311 20000 00000 2DEC .5
012557,000402: 23,2313 00000 00000 2DEC 0 B-28
012558,000403:
012559,000404: 23,2315 67313 65307 2DEC -.5376381241 B-1
012560,000405: 23,2317 00000 00000 2DEC 0 B-28
012561,000406: 23,2321 15373 11346 2DEC +.8431756920 B-1
012562,000407:
|
|
Page 289 |
012564,000409:
012565,000410: 23,2323 07020 10DEGS- DEC 3600 B-14
012566,000411:
012567,000412: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 2S COMP.
012568,000413: 23,2325 00000 OCT 00000
012569,000414:
012570,000415: 23,2326 61740 20DEGS- DEC -07199 B-14
012571,000416: 23,2327 77777 DEC -00000 B-14
012572,000417:
012573,000418: 23,2330 07020 20DEG- DEC 03600 B-14
012574,000419: 23,2331 00000 DEC 00000 B-14
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc