Source Code

012056,000001: # Copyright: Public domain. 012057,000002: # Filename: CSM_GEOMETRY.agc 012058,000003: # Purpose: Part of the source code for Colossus, build 249. 012059,000004: # It is part of the source code for the Command Module's (CM) 012060,000005: # Apollo Guidance Computer (AGC), possibly for Apollo 8 and 9. 012061,000006: # Assembler: yaYUL 012062,000007: # Reference: pp. 282-293 of 1701.pdf. 012063,000008: # Contact: Ron Burkey <info@sandroid.org>. 012064,000009: # Website: www.ibiblio.org/apollo. 012065,000010: # Mod history: 08/08/04 RSB. Began transcribing. 012066,000011: 012067,000012: # The contents of the "Colossus249" files, in general, are transcribed 012068,000013: # from a scanned document obtained from MIT's website, 012069,000014: # http://hrst.mit.edu/hrs/apollo/public/archive/1701.pdf. Notations on this 012070,000015: # document read, in part: 012071,000016: 012072,000017: # Assemble revision 249 of AGC program Colossus by NASA 012073,000018: # 2021111-041. October 28, 1968. 012074,000019: 012075,000020: # This AGC program shall also be referred to as 012076,000021: # Colossus 1A 012077,000022: 012078,000023: # Prepared by 012079,000024: # Massachusetts Institute of Technology 012080,000025: # 75 Cambridge Parkway 012081,000026: # Cambridge, Massachusetts 012082,000027: # under NASA contract NAS 9-4065. 012083,000028: 012084,000029: # Refer directly to the online document mentioned above for further information. 012085,000030: # Please report any errors (relative to 1701.pdf) to info@sandroid.org. 012086,000031: 012087,000032: # In some cases, where the source code for Luminary 131 overlaps that of 012088,000033: # Colossus 249, this code is instead copied from the corresponding Luminary 131 012089,000034: # source file, and then is proofed to incorporate any changes. 012090,000035: 012091,000036: # Page 282 012092,000037: 22,2000 BANK 22 012093,000038: 23,2000 SETLOC COMGEOM1 012094,000039: 23,2000 BANK 012095,000040: 012096,000041: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT 012097,000042: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WTIH THE SEXTAND LINE OF SIGHT. 012098,000043: 012099,000044: # THE INPUTS ARE: 1) THE SEXTAND SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE 012100,000045: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR 012101,000046: # JOB VAC AREA. 012102,000047: 012103,000048: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE 012104,000049: # OUTPUT IS ALSO AVAILABLE AT MPAC. 012105,000050: 012106,000051: 23,2000 COUNT 23/GEOM 012107,000052: 012108,000053: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D 012109,000054: 23,2001 00006 5,1 # TRUNNION = TA 012110,000055: 23,2002 45510 CDULOGIC 012111,000056: 23,2003 41434 RTB PUSH 012112,000057: 23,2004 46027 SXTLOGIC 012113,000058: 23,2005 72556 SIN SL1 012114,000059: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA) 012115,000060: 23,2007 00004 3,1 # SHAFT = SA 012116,000061: 23,2010 41434 RTB PUSH # PD4 = SA 012117,000062: 23,2011 45510 CDULOGIC 012118,000063: 012119,000064: 23,2012 41346 COS DMP 012120,000065: 23,2013 00003 2 012121,000066: 23,2014 14041 STODL STARM # COS(SA)SIN(TA) 012122,000067: 012123,000068: 23,2015 41356 SIN DMP 012124,000069: 23,2016 77626 STADR 012125,000070: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA) 012126,000071: 012127,000072: 23,2020 77746 COS 012128,000073: 23,2021 24045 STOVL STARM +4 012129,000074: 23,2022 00041 STARM # STARM = 32D 012130,000075: 23,2023 76521 MXV VSL1 012131,000076: 23,2024 06302 NB1NB2 012132,000077: 23,2025 00041 STORE 32D 012133,000078: 23,2026 77616 RVQ 012134,000079: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET 012135,000080: 23,2030 26154 ADS MPAC 012136,000081: 23,2031 34676 CAF QUARTER 012137,000082: 23,2032 07256 TC SHORTMP 012138,000083: 23,2033 06030 TC DANZIG 012139,000084: 012140,000085: # Page 283 012141,000086: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE- 012142,000087: # OF-SIGHT LIES ALONG THE STAR FECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF- 012143,000088: # ERENECED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES 012144,000089: # REFERENCED TO THE OPTICS COORDINATE SYSTEM. 012145,000090: 012146,000091: # THE INPUTS ARE: 1) THE STAR VECTOR REFERRED TO THE PRESENT STABLE MEMMBER COORDINATES STORED AT STAR. 2) SAME ANGLE 012147,000092: # INPUT AS *SMNB*, I.E., SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL 012148,000093: # TO CDUTRIG WILL PROVIDE THIS INPUT. 012149,000094: 012150,000095: # THE OUTPUT ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART 012151,000096: # EQUAL TO ZERO). 012152,000097: 012153,000098: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D 012154,000099: 23,2035 00034 28D 012155,000100: 23,2036 02766 STAR 012156,000101: 23,2037 77624 CALL 012157,000102: 23,2040 47577 *SMNB* 012158,000103: 23,2041 76521 MXV VSL1 012159,000104: 23,2042 06260 NB2NB1 012160,000105: 23,2043 26766 STOVL STAR 012161,000106: 23,2044 15330 HIUNITX 012162,000107: 23,2045 26555 STOVL XNB1 012163,000108: 23,2046 15326 HIUNITY 012164,000109: 23,2047 26563 STOVL YNB1 012165,000110: 23,2050 15324 HIUNITZ 012166,000111: 23,2051 36571 STCALL ZNB1 012167,000112: 23,2052 46076 SXTANG1 012168,000113: 012169,000114: # Page 284 012170,000115: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF- 012171,000116: # SIGHT LIES ALONG THE STAR VECTOR. 012172,000117: 012173,000118: # THE INPUTS ARE: 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE 012174,000119: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STROED AT XNB, YNB,AND 012175,000120: # ZNB. 012176,000121: 012177,000122: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART 012178,000123: # EQUAL TO ZERO). 012179,000124: 012180,000125: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D 012181,000126: 23,2054 00034 28D 012182,000127: 23,2055 45657 TRANSP1 # EREF WRT NB2 012183,000128: 23,2056 64375 VLOAD MXV 012184,000129: 23,2057 02714 XNB 012185,000130: 23,2060 06260 NB2NB1 012186,000131: 23,2061 77772 VSL1 012187,000132: 23,2062 26555 STOVL XNB1 012188,000133: 23,2063 02722 YNB 012189,000134: 23,2064 76521 MXV VSL1 012190,000135: 23,2065 06260 NB2NB1 012191,000136: 23,2066 26563 STOVL YNB1 012192,000137: 23,2067 02730 ZNB 012193,000138: 23,2070 76521 MXV VSL1 012194,000139: 23,2071 06260 NB2NB1 012195,000140: 23,2072 02571 STORE ZNB1 012196,000141: 012197,000142: 23,2073 47034 RTB RTB 012198,000143: 23,2074 45657 TRANSP1 012199,000144: 23,2075 45673 TRANSP2 012200,000145: 012201,000146: 23,2076 47375 SXTANG1 VLOAD VXV 012202,000147: 23,2077 02571 ZNB1 012203,000148: 23,2100 02766 STAR 012204,000149: 23,2101 77600 BOV 012205,000150: 23,2102 46103 +1 012206,000151: 23,2103 40056 UNIT BOV 012207,000152: 23,2104 46145 ZNB=S1 012208,000153: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S) 012209,000154: 012210,000155: 23,2106 57441 DOT DCOMP 012211,000156: 23,2107 02555 XNB1 012212,000157: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB 012213,000158: 23,2111 00027 PDA 012214,000159: 012215,000160: 23,2112 77641 DOT 012216,000161: 23,2113 02563 YNB1 012217,000162: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB 012218,000163: 23,2115 47211 ARCTRIG 012219,000164: # Page 285 012220,000165: 23,2116 77634 RTB 012221,000166: 23,2117 45543 1STO2S 012222,000167: 23,2120 26774 STOVL SAC 012223,000168: 23,2121 02766 STAR 012224,000169: 23,2122 77600 BOV 012225,000170: 23,2123 46124 +1 012226,000171: 23,2124 72441 DOT SL1 012227,000172: 23,2125 02571 ZNB1 012228,000173: 23,2126 77726 ACOS 012229,000174: 23,2127 62440 BMN SL2 012230,000175: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE 012231,000176: 23,2131 45200 BOV DSU 012232,000177: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES 012233,000178: 23,2133 06331 20DEG- 012234,000179: 23,2134 77634 RTB 012235,000180: 23,2135 45543 1STO2S 012236,000181: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF 012237,000182: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEGR 012238,000183: 23,2140 01630 CULTFLAG 012239,000184: 23,2141 00034 28D 012240,000185: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS 012241,000186: 23,2143 01430 CULTFLAG 012242,000187: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI 012243,000188: 23,2145 77745 ZNB=S1 DLOAD 012244,000189: 23,2146 06325 270DEG 012245,000190: 23,2147 16774 STODL SAC 012246,000191: 23,2150 06327 20DEGS- 012247,000192: 23,2151 02776 STORE PAC 012248,000193: 23,2152 77614 CLRGO 012249,000194: 23,2153 01630 CULTFLAG 012250,000195: 23,2154 00034 28D 012251,000196: 012252,000197: # Page 286 012253,000198: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING 012254,000199: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO 012255,000200: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPIRATELY IN RN,VN OR 012256,000201: # R-OTHER, V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE 012257,000202: # OTHER VEHICLES COMPUTER. 012258,000203: 012259,000204: # INPUT 012260,000205: # STATE VECTOR IN TEMPORARY STORAGE AREA 012261,000206: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5 012262,000207: # SET X2 TO +2 012263,000208: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7 012264,000209: # SET X2 TO 0 012265,000210: 012266,000211: # OUTPUT 012267,000212: # R(T) IN RN, V(T) IN VN, T IN PIPTIME 012268,000213: # OR 012269,000214: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER) 012270,000215: 012271,000216: 23,2155 BANK 23 012272,000217: 10,2000 SETLOC COMGEOM2 012273,000218: 10,2000 BANK 012274,000219: 10,2237 COUNT 10/GEOM 012275,000220: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG 012276,000221: 10,2240 04756 AVEMIDSW 012277,000222: 10,2241 20242 +1 012278,000223: 10,2242 53775 VLOAD VSL* 012279,000224: 10,2243 01521 TDELTAV 012280,000225: 10,2244 57605 0 -7,2 012281,000226: 10,2245 53655 VAD VSL* 012282,000227: 10,2246 01535 RCV 012283,000228: 10,2247 57576 0,2 012284,000229: 10,2250 25171 STOVL RN 012285,000230: 10,2251 01527 TNUV 012286,000231: 10,2252 53257 VSL* VAD 012287,000232: 10,2253 57602 0 -4,2 012288,000233: 10,2254 01543 VCV 012289,000234: 10,2255 77657 VSL* 012290,000235: 10,2256 57576 0,2 012291,000236: 10,2257 15177 STODL VN 012292,000237: 10,2260 01517 TET 012293,000238: 10,2261 01205 STORE PIPTIME 012294,000239: 10,2262 77616 RVQ 012295,000240: 10,2263 53775 SVDWN2 VLOAD VSL* 012296,000241: 10,2264 01521 TDELTAV 012297,000242: 10,2265 57605 0 -7,2 012298,000243: 10,2266 53655 VAD VSL* 012299,000244: 10,2267 01535 RCV 012300,000245: # Page 287 012301,000246: 10,2270 57576 0,2 012302,000247: 10,2271 25722 STOVL R-OTHER 012303,000248: 10,2272 01527 TNUV 012304,000249: 10,2273 53257 VSL* VAD 012305,000250: 10,2274 57602 0 -4,2 012306,000251: 10,2275 01543 VCV 012307,000252: 10,2276 77657 VSL* 012308,000253: 10,2277 57576 0,2 012309,000254: 10,2300 01730 STORE V-OTHER 012310,000255: 10,2301 77616 RVQ 012311,000256: 012312,000257: # Page 288 012313,000258: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1). 012314,000259: 012315,000260: # ENTRY: CALL 012316,000261: # LOG 012317,000262: 012318,000263: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC. 012319,000264: 012320,000265: # EBANK IS ARBITRARY. 012321,000266: 012322,000267: 14,2000 BANK 14 012323,000268: 23,2000 SETLOC POWFLIT2 012324,000269: 23,2000 BANK 012325,000270: 23,2155 COUNT 23/GEOM 012326,000271: 012327,000272: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG 012328,000273: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1. 012329,000274: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE 012330,000275: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED 012331,000276: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED 012332,000277: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH) 012333,000278: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3. 012334,000279: 23,2165 01001 14636 2DEC .031335467 012335,000280: 23,2167 00325 07310 2DEC .0130145859 012336,000281: 23,2171 00541 16735 2DEC .0215738898 012337,000282: 012338,000283: 23,2173 34714 CAF ZERO 012339,000284: 23,2174 54156 TS MPAC +2 012340,000285: 23,2175 00006 EXTEND 012341,000286: 23,2176 32214 DCA CLOG2/32 012342,000287: 23,2177 52155 DXCH MPAC 012343,000288: 23,2200 52160 DXCH MPAC +3 012344,000289: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A. 012345,000290: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT. 012346,000291: 012347,000292: 23,2203 52156 DXCH MPAC +1 012348,000293: 23,2204 52155 DXCH MPAC 012349,000294: 23,2205 52160 DXCH MPAC +3 012350,000295: 23,2206 20155 DAS MPAC 012351,000296: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1 012352,000297: 012353,000298: 23,2210 77616 RVQ 012354,000299: 012355,000300: 23,2211 37777 37777 NEARLY1 2DEC .999999999 012356,000301: 012357,000302: # Page 289 012358,000303: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494 012359,000304: 012360,000305: # Page 290 012361,000306: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67 012362,000307: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS 012363,000308: # MOD BY: ENTRY GROUP (BAIRNSFATHER) 012364,000309: 012365,000310: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH 012366,000311: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY 012367,000312: # AND NORMAL COMPONENTS RTEAST AND RTNORM. INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR 012368,000313: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED 012369,000314: # TARGET VECTOR RT. ALL VECTORS EXCEPT UNITW ARE HALF UNIT. 012370,000315: # THE EQUATIONS ARE: 012371,000316: # _ _ _ _ 012372,000317: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT) 012373,000318: 012374,000319: # WHERE WT = WIE DTEAROT 012375,000320: 012376,000321: # RTINIT = INITIAL TARGET VECTOR 012377,000322: # _ _ _ 012378,000323: # RTEAST = UNITW * RTINIT 012379,000324: # _ _ _ 012380,000325: # RTNORM = RTEAST * UNITW 012381,000326: 012382,000327: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2. 012383,000328: # 012384,000329: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL 012385,000330: # STCALL DTEAROT STCALL DTEAROT 012386,000331: # EARROT1 EARROT2 012387,000332: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT 012388,000333: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED. 012389,000334: 012390,000335: # SUBROUTINES USED: NONE 012391,000336: 012392,000337: # NORMAL EXIT MODES: RVQ 012393,000338: 012394,000339: # ALARMS: NONE 012395,000340: 012396,000341: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL 012397,000342: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL 012398,000343: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS 012399,000344: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY 012400,000345: 012401,000346: # ERASABLE INITIALIZATION REQUIRED: 012402,000347: # UNITW (0) UNIT POLAR VECTOR PAD LOADED 012403,000348: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY 012404,000349: # DTEAROT (-26) CS TIME OF FLIGHT LEFT BY CALLER 012405,000350: 012406,000351: # DEBRIS: QPRET, PDL+0 ... PDL+5 012407,000352: # Page 291 012408,000353: 23,2215 E7,1451 EBANK= RTINIT 012409,000354: 012410,000355: 23,2215 47375 EARROT1 VLOAD VXV 012411,000356: 23,2216 01714 UNITW # FULL UNIT VECTOR 012412,000357: 23,2217 03452 RTINIT # .5 UNIT 012413,000358: 23,2220 03460 STORE RTEAST # .5 UNIT 012414,000359: 012415,000360: 23,2221 77635 VXV 012416,000361: 23,2222 01714 UNITW # FULL UNIT 012417,000362: 23,2223 17466 STODL RTNORM # .5 UNIT 012418,000363: 23,2224 03606 DTEAROT # (-28) CS 012419,000364: 012420,000365: 23,2225 56204 EARROT2 BOVB DDV 012421,000366: 23,2226 57343 TCDANZIG # RESET OVFIND, IF ON 012422,000367: 23,2227 06256 1/WIE 012423,000368: 23,2230 41400 BOV PUSH 012424,000369: 23,2231 46245 OVERADAY 012425,000370: 23,2232 45346 COS DSU 012426,000371: 23,2233 15330 HIDPHALF 012427,000372: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST 012428,000373: 23,2235 03466 RTNORM # .5 UNIT 012429,000374: 23,2236 74356 SIN VXSC 012430,000375: 23,2237 03460 RTEAST # .5 UNIT 012431,000376: 23,2240 76455 VAD VSL1 012432,000377: 23,2241 53455 VAD UNIT # INSURE THAT RT IS "UNIT". 012433,000378: 23,2242 03452 RTINIT # .5 UNIT 012434,000379: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR 012435,000380: 012436,000381: 23,2244 77616 RVQ 012437,000382: 012438,000383: 23,2245 75345 OVERADAY DLOAD SIGN 012439,000384: 23,2246 06256 1/WIE 012440,000385: 23,2247 03606 DTEAROT 012441,000386: 23,2250 77621 BDSU 012442,000387: 23,2251 03606 DTEAROT 012443,000388: 23,2252 03606 STORE DTEAROT 012444,000389: 012445,000390: 23,2253 77650 GOTO 012446,000391: 23,2254 46225 EARROT2 012447,000392: 012448,000393: # WIE 2DEC .1901487997 012449,000394: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28 012450,000395: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1 012451,000396: 23,2261 00000 00000 2DEC 0 B-28 012452,000397: 23,2263 67313 65307 2DEC -.5376381241 B-1 012453,000398: # Page 292 012454,000399: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28 012455,000400: 23,2267 20000 00000 HALFNFLT 2DEC .5 012456,000401: 23,2271 00000 00000 2DEC 0 B-28 012457,000402: 23,2273 10464 12470 2DEC +.5376381241 B-1 012458,000403: 23,2275 00000 00000 2DEC 0 B-28 012459,000404: 23,2277 15373 11346 2DEC +.8431756920 B-1 012460,000405: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1 012461,000406: 23,2303 00000 00000 2DEC 0 B-28 012462,000407: 23,2305 10464 12470 2DEC +.5376381241 B-1 012463,000408: 23,2307 00000 00000 2DEC 0 B-28 012464,000409: 23,2311 20000 00000 2DEC .5 012465,000410: 23,2313 00000 00000 2DEC 0 B-28 012466,000411: 23,2315 67313 65307 2DEC -.5376381241 B-1 012467,000412: 23,2317 00000 00000 2DEC 0 B-28 012468,000413: 23,2321 15373 11346 2DEC +.8431756920 B-1 012469,000414: # Page 293 012470,000415: 23,2323 07020 10DEGS- DEC 3600 B-14 012471,000416: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 25 COMP. 012472,000417: 23,2325 00000 OCT 00000 012473,000418: 23,2326 61740 20DEGS- DEC -07199 B-14 012474,000419: 23,2327 77777 DEC -00000 B-14 012475,000420: 23,2330 07020 20DEG- DEC 03600 B-14 012476,000421: 23,2331 00000 DEC 00000 B-14 012477,000422: End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc