Source Code
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These source-code files are part of a reconstructed copy of Artemis 071, the
first release of the Apollo 15 through 17 Command Module (CM) Apollo Guidance
Computer (AGC) software.
The reconstruction began with source code of Artemis 072 previously transcribed
from a digitized copy of that program. The code was then updated by undoing
changes between the two versions. The reconstruction was verified by matching
memory-bank checksums to those listed in drawing 2021154-. Note that page
numbers in the reconstructed code match those on the Artemis 072 printout,
although the changed code would likely have changed page numbers for a real
Artemis 071 listing.
Comments from the original source code are prefixed with a single '#' symbol,
whereas comments added later are prefixed by "##" or "###". Report any errors
noted by creating an
issue report at the Virtual AGC
project's GitHub repository.
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013124,000002: ## Copyright: Public domain.
013125,000003: ## Filename: CSM_GEOMETRY.agc
013126,000004: ## Purpose: A section of Artemis revision 071.
013127,000005: ## It is part of the reconstructed source code for the first
013128,000006: ## release of the flight software for the Command Module's
013129,000007: ## (CM) Apollo Guidance Computer (AGC) for Apollo 15 through
013130,000008: ## 17. The code has been recreated from a copy of Artemis 072.
013131,000009: ## It has been adapted such that the resulting bugger words
013132,000010: ## exactly match those specified for Artemis 071 in NASA
013133,000011: ## drawing 2021154-, which gives relatively high confidence
013134,000012: ## that the reconstruction is correct.
013135,000013: ## Reference: 297
013136,000014: ## Assembler: yaYUL
013137,000015: ## Contact: Ron Burkey <info@sandroid.org>.
013138,000016: ## Website: www.ibiblio.org/apollo/index.html
013139,000017: ## Mod history: 2019-08-14 MAS Created from Artemis 072.
013140,000018:
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Page 297
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013142,000020:
013143,000021: 23,2000 SETLOC COMGEOM1
013144,000022: 23,2000 BANK
013145,000023:
013146,000024: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
013147,000025: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
013148,000026:
013149,000027: # THE INPUTS ARE 1) THE SEXTANT SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
013150,000028: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
013151,000029: # JOB VAC AREA.
013152,000030:
013153,000031: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
013154,000032: # OUTPUT IS ALSO AVAILABLE AT MPAC.
013155,000033:
013156,000034: 23,2000 COUNT* $$/GEOM
013157,000035: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
013158,000036: 23,2001 00006 5,1 # TRUNNION = TA
013159,000037: 23,2002 51754 CDULOGIC
013160,000038: 23,2003 41434 RTB PUSH
013161,000039: 23,2004 46027 SXTLOGIC
013162,000040: 23,2005 72556 SIN SL1
013163,000041: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
013164,000042: 23,2007 00004 3,1 # SHAFT = SA
013165,000043: 23,2010 41434 RTB PUSH # PD4 = SA
013166,000044: 23,2011 51754 CDULOGIC
013167,000045:
013168,000046: 23,2012 41346 COS DMP
013169,000047: 23,2013 00003 2
013170,000048: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
013171,000049:
013172,000050: 23,2015 41356 SIN DMP
013173,000051: 23,2016 77626 STADR
013174,000052: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
013175,000053:
013176,000054: 23,2020 77746 COS
013177,000055: 23,2021 24045 STOVL STARM +4
013178,000056: 23,2022 00041 STARM # STARM = 32D
013179,000057: 23,2023 76521 MXV VSL1
013180,000058: 23,2024 06300 NB1NB2
013181,000059: 23,2025 00041 STORE 32D
013182,000060: 23,2026 77616 RVQ
013183,000061:
013184,000062: 23,2027 32321 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
013185,000063: 23,2030 26154 ADS MPAC
013186,000064: 23,2031 34754 CAF QUARTER
013187,000065: 23,2032 07256 TC SHORTMP
013188,000066: 23,2033 06030 TC DANZIG
013189,000067:
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Page 298
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013191,000069:
013192,000070: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
013193,000071: # OF-SIGHT LIES ALONG THE STAR VECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
013194,000072: # ERENCED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
013195,000073: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
013196,000074:
013197,000075: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO PRESENT STABLE MEMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
013198,000076: # INPUT AS *SMNB*, I.E. SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
013199,000077: # TO CDUTRIG WILL PROVIDE THIS INPUT.
013200,000078:
013201,000079: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
013202,000080: # EQUAL TO ZERO).
013203,000081:
013204,000082: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D,28D,30D,32D-36D
013205,000083: 23,2035 00034 28D
013206,000084: 23,2036 02766 STAR
013207,000085: 23,2037 77624 CALL
013208,000086: 23,2040 47633 *SMNB*
013209,000087: 23,2041 76521 MXV VSL1
013210,000088: 23,2042 06256 NB2NB1
013211,000089: 23,2043 26766 STOVL STAR
013212,000090: 23,2044 15334 HIUNITX
013213,000091: 23,2045 26555 STOVL XNB1
013214,000092: 23,2046 15332 HIUNITY
013215,000093: 23,2047 26563 STOVL YNB1
013216,000094: 23,2050 15330 HIUNITZ
013217,000095: 23,2051 36571 STCALL ZNB1
013218,000096: 23,2052 46076 SXTANG1
013219,000097:
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013221,000099:
013222,000100: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
013223,000101: # SIGHT LIES ALONG THE STAR VECTOR.
013224,000102:
013225,000103: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
013226,000104: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB, AND
013227,000105: # ZNB.
013228,000106:
013229,000107: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
013230,000108: # EQUAL TO ZERO).
013231,000109:
013232,000110: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
013233,000111: 23,2054 00034 28D
013234,000112: 23,2055 45731 TRANSP1 # EREF WRT NB2
013235,000113: 23,2056 64375 VLOAD MXV
013236,000114: 23,2057 02714 XNB
013237,000115: 23,2060 06256 NB2NB1
013238,000116: 23,2061 77772 VSL1
013239,000117: 23,2062 26555 STOVL XNB1
013240,000118: 23,2063 02722 YNB
013241,000119: 23,2064 76521 MXV VSL1
013242,000120: 23,2065 06256 NB2NB1
013243,000121: 23,2066 26563 STOVL YNB1
013244,000122: 23,2067 02730 ZNB
013245,000123: 23,2070 76521 MXV VSL1
013246,000124: 23,2071 06256 NB2NB1
013247,000125: 23,2072 02571 STORE ZNB1
013248,000126:
013249,000127: 23,2073 47034 RTB RTB
013250,000128: 23,2074 45731 TRANSP1
013251,000129: 23,2075 45745 TRANSP2
013252,000130:
013253,000131: 23,2076 47375 SXTANG1 VLOAD VXV
013254,000132: 23,2077 02571 ZNB1
013255,000133: 23,2100 02766 STAR
013256,000134: 23,2101 77600 BOV
013257,000135: 23,2102 46103 +1
013258,000136: 23,2103 40056 UNIT BOV
013259,000137: 23,2104 46145 ZNB=S1
013260,000138: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
013261,000139:
013262,000140: 23,2106 57441 DOT DCOMP
013263,000141: 23,2107 02555 XNB1
013264,000142: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
013265,000143: 23,2111 00027 PDA
013266,000144:
013267,000145: 23,2112 77641 DOT
013268,000146: 23,2113 02563 YNB1
013269,000147: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
013270,000148: 23,2115 47311 ARCTRIG
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Page 300
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013272,000150: 23,2116 77634 RTB
013273,000151: 23,2117 45640 1STO2S
013274,000152: 23,2120 26774 STOVL SAC
013275,000153: 23,2121 02766 STAR
013276,000154: 23,2122 77600 BOV
013277,000155: 23,2123 46124 +1
013278,000156: 23,2124 72441 DOT SL1
013279,000157: 23,2125 02571 ZNB1
013280,000158: 23,2126 77726 ACOS
013281,000159: 23,2127 62440 BMN SL2
013282,000160: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
013283,000161: 23,2131 45200 BOV DSU
013284,000162: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
013285,000163: 23,2133 06327 20DEG-
013286,000164: 23,2134 77634 RTB
013287,000165: 23,2135 45640 1STO2S
013288,000166: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
013289,000167: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEG
013290,000168: 23,2140 01630 CULTFLAG
013291,000169: 23,2141 00034 28D
013292,000170: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
013293,000171: 23,2143 01430 CULTFLAG
013294,000172: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI
013295,000173: 23,2145 77745 ZNB=S1 DLOAD
013296,000174: 23,2146 06323 270DEG
013297,000175: 23,2147 16774 STODL SAC
013298,000176: 23,2150 06325 20DEGS-
013299,000177: 23,2151 02776 STORE PAC
013300,000178: 23,2152 77614 CLRGO
013301,000179: 23,2153 01630 CULTFLAG
013302,000180: 23,2154 00034 28D
013303,000181:
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013305,000183:
013306,000184: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
013307,000185: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO
013308,000186: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
013309,000187: # R-OTHER , V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
013310,000188: # OTHER VEHICLES COMPUTER.
013311,000189:
013312,000190: # INPUT
013313,000191: # STATE VECTOR IN TEMPORARY STORAGE AREA
013314,000192: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
013315,000193: # SET X2 TO +2
013316,000194: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
013317,000195: # SET X2 TO 0
013318,000196:
013319,000197: # OUTPUT
013320,000198: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
013321,000199: # OR
013322,000200: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
013323,000201:
013324,000202: 10,2000 SETLOC COMGEOM2
013325,000203: 10,2000 BANK
013326,000204: 10,2240 COUNT* $$/GEOM
013327,000205: 10,2240 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
013328,000206: 10,2241 04756 AVEMIDSW
013329,000207: 10,2242 20243 +1
013330,000208: 10,2243 53775 VLOAD VSL*
013331,000209: 10,2244 01521 TDELTAV
013332,000210: 10,2245 57605 0 -7,2
013333,000211: 10,2246 53655 VAD VSL*
013334,000212: 10,2247 01535 RCV
013335,000213: 10,2250 57576 0,2
013336,000214: 10,2251 25030 STOVL RN
013337,000215: 10,2252 01527 TNUV
013338,000216: 10,2253 53257 VSL* VAD
013339,000217: 10,2254 57602 0 -4,2
013340,000218: 10,2255 01543 VCV
013341,000219: 10,2256 77657 VSL*
013342,000220: 10,2257 57576 0,2
013343,000221: 10,2260 15036 STODL VN
013344,000222: 10,2261 01517 TET
013345,000223: 10,2262 01044 STORE PIPTIME
013346,000224: 10,2263 77616 RVQ
013347,000225:
013348,000226: 10,2264 53775 SVDWN2 VLOAD VSL*
013349,000227: 10,2265 01521 TDELTAV
013350,000228: 10,2266 57605 0 -7,2
013351,000229: 10,2267 53655 VAD VSL*
013352,000230: 10,2270 01535 RCV
013353,000231: 10,2271 57576 0,2
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013355,000233: 10,2272 25720 STOVL R-OTHER
013356,000234: 10,2273 01527 TNUV
013357,000235: 10,2274 53257 VSL* VAD
013358,000236: 10,2275 57602 0 -4,2
013359,000237: 10,2276 01543 VCV
013360,000238: 10,2277 77657 VSL*
013361,000239: 10,2300 57576 0,2
013362,000240: 10,2301 01726 STORE V-OTHER
013363,000241: 10,2302 77616 RVQ
013364,000242:
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Page 303
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013366,000244:
013367,000245: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
013368,000246:
013369,000247: # ENTRY: CALL
013370,000248: # LOG
013371,000249:
013372,000250: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
013373,000251:
013374,000252: # EBANK IS ARBITRARY..
013375,000253:
013376,000254: 23,2000 SETLOC POWFLIT2
013377,000255: 23,2000 BANK
013378,000256: 23,2155 COUNT* $$/GEOM
013379,000257: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
013380,000258: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
013381,000259: 23,2157 15344 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
013382,000260: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
013383,000261:
013384,000262: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
013385,000263:
013386,000264: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
013387,000265: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
013388,000266: 23,2165 01001 14636 2DEC .031335467
013389,000267: 23,2167 00325 07310 2DEC .0130145859
013390,000268: 23,2171 00541 16735 2DEC .0215738898
013391,000269:
013392,000270: 23,2173 34772 CAF ZERO
013393,000271: 23,2174 54156 TS MPAC +2
013394,000272: 23,2175 00006 EXTEND
013395,000273: 23,2176 32212 DCA CLOG2/32
013396,000274: 23,2177 52155 DXCH MPAC
013397,000275: 23,2200 52160 DXCH MPAC +3
013398,000276: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
013399,000277: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
013400,000278:
013401,000279: 23,2203 52156 DXCH MPAC +1
013402,000280: 23,2204 52155 DXCH MPAC
013403,000281: 23,2205 52160 DXCH MPAC +3
013404,000282: 23,2206 20155 DAS MPAC
013405,000283: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
013406,000284:
013407,000285: 23,2210 77616 RVQ
013408,000286:
013409,000287: 23,2211 26,3343 NEARLY1 = NEARONE
013410,000288: 23,2211 00542 34414 CLOG2/32 2DEC .0216608494
013411,000289:
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Page 304
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013413,000291:
013414,000292: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
013415,000293: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
013416,000294: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
013417,000295:
013418,000296: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
013419,000297: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
013420,000298: # AND NORMAL COMPONENTS RTEAST AND RTNORM . INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
013421,000299: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
013422,000300: # TARGET VECTOR RT . ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
013423,000301: # THE EQUATIONS ARE
013424,000302: # - - - -
013425,000303: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT)
013426,000304:
013427,000305: # WHERE WT = WIE DTEAROT
013428,000306:
013429,000307: # RTINIT = INITIAL TARGET VECTOR
013430,000308: # - - -
013431,000309: # RTEAST = UNITW * RTINIT
013432,000310: # - - -
013433,000311: # RTNORM = RTEAST * UNITW
013434,000312:
013435,000313: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
013436,000314:
013437,000315: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
013438,000316: # STCALL DTEAROT STCALL DTEAROT
013439,000317: # EARROT1 EARROT2
013440,000318: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
013441,000319: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
013442,000320:
013443,000321: # SUBROUTINES USED: NONE
013444,000322:
013445,000323: # NORMAL EXIT MODES: RVQ
013446,000324:
013447,000325: # ALARMS: NONE
013448,000326:
013449,000327: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
013450,000328: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
013451,000329: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
013452,000330: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
013453,000331:
013454,000332: # ERASABLE INITIALIZATION REQUIRED:
013455,000333: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
013456,000334: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
013457,000335: # DTEAROT (-28) CS TIME OF FLIGHT LEFT BY CALLER
013458,000336:
013459,000337: # DEBRIS: QPRET, PDL+0 ... PDL+5
013460,000338:
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013462,000340: 23,2213 E7,1451 EBANK= RTINIT
013463,000341:
013464,000342: 23,2213 47375 EARROT1 VLOAD VXV
013465,000343: 23,2214 01712 UNITW # FULL UNIT VECTOR
013466,000344: 23,2215 03452 RTINIT # .5 UNIT
013467,000345: 23,2216 03460 STORE RTEAST # .5 UNIT
013468,000346:
013469,000347: 23,2217 77635 VXV
013470,000348: 23,2220 01712 UNITW # FULL UNIT
013471,000349: 23,2221 17466 STODL RTNORM # .5 UNIT
013472,000350: 23,2222 03606 DTEAROT # (-28) CS
013473,000351:
013474,000352: 23,2223 56204 EARROT2 BOVB DDV
013475,000353: 23,2224 57544 TCDANZIG # RESET OVFIND, IF ON
013476,000354: 23,2225 06254 1/WIE
013477,000355: 23,2226 41400 BOV PUSH
013478,000356: 23,2227 46243 OVERADAY
013479,000357: 23,2230 45346 COS DSU
013480,000358: 23,2231 15334 HIDPHALF
013481,000359: 23,2232 65361 VXSC PDDL # XCH W PUSH LIST
013482,000360: 23,2233 03466 RTNORM # .5 UNIT
013483,000361: 23,2234 74356 SIN VXSC
013484,000362: 23,2235 03460 RTEAST # .5 UNIT
013485,000363: 23,2236 76455 VAD VSL1
013486,000364: 23,2237 53455 VAD UNIT # INSURE THAT RT IS 'UNIT'.
013487,000365: 23,2240 03452 RTINIT # .5 UNIT
013488,000366: 23,2241 03474 STORE RT # .5 UNIT TARGET VECTOR
013489,000367:
013490,000368: 23,2242 77616 RVQ
013491,000369:
013492,000370: 23,2243 75345 OVERADAY DLOAD SIGN
013493,000371: 23,2244 06254 1/WIE
013494,000372: 23,2245 03606 DTEAROT
013495,000373: 23,2246 77621 BDSU
013496,000374: 23,2247 03606 DTEAROT
013497,000375: 23,2250 03606 STORE DTEAROT
013498,000376:
013499,000377: 23,2251 77650 GOTO
013500,000378: 23,2252 46223 EARROT2
013501,000379:
013502,000380: # WIE 2DEC .1901487997
013503,000381: 23,2253 01015 34732 1/WIE 2DEC 8616410 B-28
013504,000382:
013505,000383: 23,2255 15373 11346 NB2NB1 2DEC +.8431756920 B-1
013506,000384: 23,2257 00000 00000 2DEC 0 B-28
013507,000385: 23,2261 67313 65307 2DEC -.5376381241 B-1
013508,000386:
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013510,000388:
013511,000389: 23,2263 00000 00000 ZERINFLT 2DEC 0 B-28
013512,000390:
013513,000391: 23,2265 20000 00000 HALFNFLT 2DEC .5
013514,000392: 23,2267 00000 00000 2DEC 0 B-28
013515,000393: 23,2271 10464 12470 2DEC +.5376381241 B-1
013516,000394: 23,2273 00000 00000 2DEC 0 B-28
013517,000395: 23,2275 15373 11346 2DEC +.8431756920 B-1
013518,000396:
013519,000397: 23,2277 15373 11346 NB1NB2 2DEC +.8431756920 B-1
013520,000398: 23,2301 00000 00000 2DEC 0 B-28
013521,000399: 23,2303 10464 12470 2DEC +.5376381241 B-1
013522,000400: 23,2305 00000 00000 2DEC 0 B-28
013523,000401: 23,2307 20000 00000 2DEC .5
013524,000402: 23,2311 00000 00000 2DEC 0 B-28
013525,000403: 23,2313 67313 65307 2DEC -.5376381241 B-1
013526,000404: 23,2315 00000 00000 2DEC 0 B-28
013527,000405: 23,2317 15373 11346 2DEC +.8431756920 B-1
013528,000406:
|
|
Page 307
|
013530,000408:
013531,000409: 23,2321 07020 10DEGS- DEC 3600 B-14
013532,000410:
013533,000411: 23,2322 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 2S COMP.
013534,000412: 23,2323 00000 OCT 00000
013535,000413:
013536,000414: 23,2324 61740 20DEGS- DEC -07199 B-14
013537,000415: 23,2325 77777 DEC -00000 B-14
013538,000416:
013539,000417: 23,2326 07020 20DEG- DEC 03600 B-14
013540,000418: 23,2327 00000 DEC 00000 B-14
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc