Source Code
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These source-code files are part of a reconstructed copy of Comanche 44, the
initial release (though not the final mission release) of the Apollo 10
Command Module (CM) Apollo Guidance Computer (AGC) software. Subsequent releases
were Comanche 45 and Comanche 45/2 (the flown release on Apollo 10). The reconstruction
is believed to be exactly accurate, but in the absence of an actual Apollo-era
listing of Comanche 44, some explanation of the reconstruction process is needed
to insure confidence in that accuracy.
The starting point was the source code of Comanche 51
(separately previously reconstructed from an Apollo-era listing of Comanche 55,
flown on Apollo 11). Comanche 51 source code was then modified
by undoing changes known to have been made between revisions 44 and 51. The now-reconstructed
Comanche 44 source code was verified by assembling it and checking that the assembled code had
the expected known-correct memory-bank checksums.
Note that page numbers in the reconstructed code match those on the Comanche 55 printout,
although the source code would likely have different page numbers in a contemporary
Comanche 44 listing.
Annotations that were not present in the contemporary source code have been added to the reconstructed
code to justify each change relative to Comanche 51. Here's a guide to the Apollo documentation referenced
in those annotations:
In most cases, only the titles (rather than the full texts) of PCRs are known. In addition to the
explanatory annotations, there is also
a step-by-step commentary about the reconstruction process.
Comments expected to have been present in 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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012290,000002: ## Copyright: Public domain.
012291,000003: ## Filename: CSM_GEOMETRY.agc
012292,000004: ## Purpose: A section of Comanche revision 044.
012293,000005: ## It is part of the reconstructed source code for the
012294,000006: ## original release of the flight software for the Command
012295,000007: ## Module's (CM) Apollo Guidance Computer (AGC) for Apollo 10.
012296,000008: ## The code has been recreated from a copy of Comanche 055. It
012297,000009: ## has been adapted such that the resulting bugger words
012298,000010: ## exactly match those specified for Comanche 44 in NASA drawing
012299,000011: ## 2021153D, which gives relatively high confidence that the
012300,000012: ## reconstruction is correct.
012301,000013: ## Assembler: yaYUL
012302,000014: ## Contact: Ron Burkey <info@sandroid.org>.
012303,000015: ## Website: www.ibiblio.org/apollo/index.html
012304,000016: ## Mod history: 2020-12-03 MAS Created from Comanche 51.
012305,000017:
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012307,000019: 22,2000 BANK 22
012308,000020: 23,2000 SETLOC COMGEOM1
012309,000021: 23,2000 BANK
012310,000022:
012311,000023: # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
012312,000024: # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
012313,000025:
012314,000026: # THE INPUTS ARE 1) THE SEXTANT SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
012315,000027: # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
012316,000028: # JOB VAC AREA.
012317,000029:
012318,000030: # THE OUTPUT IS A HALF-UNIT VECTOR IN NAVIGATION BASE COORDINATES AND STORED AT LOCATION 32D OF THE VAC AREA. THE
012319,000031: # OUTPUT IS ALSO AVAILABLE AT MPAC.
012320,000032:
012321,000033: 23,2000 COUNT 23/GEOM
012322,000034:
012323,000035: 23,2000 47133 SXTNB SLOAD* RTB # PUSHDOWN 00,02,04,(17D-19D),32D-36D
012324,000036: 23,2001 00006 5,1 # TRUNNION = TA
012325,000037: 23,2002 45513 CDULOGIC
012326,000038: 23,2003 41434 RTB PUSH
012327,000039: 23,2004 46027 SXTLOGIC
012328,000040: 23,2005 72556 SIN SL1
012329,000041: 23,2006 66606 PUSH SLOAD* # PD2 = SIN(TA)
012330,000042: 23,2007 00004 3,1 # SHAFT = SA
012331,000043: 23,2010 41434 RTB PUSH # PD4 = SA
012332,000044: 23,2011 45513 CDULOGIC
012333,000045:
012334,000046: 23,2012 41346 COS DMP
012335,000047: 23,2013 00003 2
012336,000048: 23,2014 14041 STODL STARM # COS(SA)SIN(TA)
012337,000049:
012338,000050: 23,2015 41356 SIN DMP
012339,000051: 23,2016 77626 STADR
012340,000052: 23,2017 63734 STODL STARM +2 # SIN(SA)SIN(TA)
012341,000053:
012342,000054: 23,2020 77746 COS
012343,000055: 23,2021 24045 STOVL STARM +4
012344,000056: 23,2022 00041 STARM # STARM = 32D
012345,000057: 23,2023 76521 MXV VSL1
012346,000058: 23,2024 06302 NB1NB2
012347,000059: 23,2025 00041 STORE 32D
012348,000060: 23,2026 77616 RVQ
012349,000061:
012350,000062: 23,2027 32323 SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET
012351,000063: 23,2030 26154 ADS MPAC
012352,000064: 23,2031 35003 CAF QUARTER
012353,000065: 23,2032 07256 TC SHORTMP
012354,000066: 23,2033 06030 TC DANZIG
012355,000067:
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012357,000069: # CALCSXA COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-
012358,000070: # OF-SIGHT LIES ALONG THE STAR VECTOR. THE ROUTINE TAKES THE GIVEN STAR VECTOR AND EXPRESSES IT AS A VECTOR REF-
012359,000071: # ERENCED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES
012360,000072: # REFERENCED TO THE OPTICS COORDINATE SYSTEM.
012361,000073:
012362,000074: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO PRESENT STABLE MEMBER COORDINATES STORED AT STAR. 2) SAME ANGLE
012363,000075: # INPUT AS *SMNB*, I.E. SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL
012364,000076: # TO CDUTRIG WILL PROVIDE THIS INPUT.
012365,000077:
012366,000078: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012367,000079: # EQUAL TO ZERO).
012368,000080:
012369,000081: 23,2034 77220 CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D
012370,000082: 23,2035 00034 28D
012371,000083: 23,2036 02766 STAR
012372,000084: 23,2037 77624 CALL
012373,000085: 23,2040 47644 *SMNB*
012374,000086: 23,2041 76521 MXV VSL1
012375,000087: 23,2042 06260 NB2NB1
012376,000088: 23,2043 26766 STOVL STAR
012377,000089: 23,2044 15333 HIUNITX
012378,000090: 23,2045 26555 STOVL XNB1
012379,000091: 23,2046 15331 HIUNITY
012380,000092: 23,2047 26563 STOVL YNB1
012381,000093: 23,2050 15327 HIUNITZ
012382,000094: 23,2051 36571 STCALL ZNB1
012383,000095: 23,2052 46076 SXTANG1
012384,000096:
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012386,000098: # SXTANG COMPUTES THE SEXTANT SHAFT AND TRUNNION ANGLES REQUIRED TO POSITION THE OPTICS SUCH THAT A STAR LINE-OF-
012387,000099: # SIGHT LIES ALONG THE STAR VECTOR.
012388,000100:
012389,000101: # THE INPUTS ARE 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
012390,000102: # COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB,AND
012391,000103: # ZNB.
012392,000104:
012393,000105: # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
012394,000106: # EQUAL TO ZERO).
012395,000107:
012396,000108: 23,2053 47020 SXTANG ITA RTB # PUSHDOWN 16D,18D,22D-26D,28D
012397,000109: 23,2054 00034 28D
012398,000110: 23,2055 45662 TRANSP1 # EREF WRT NB2
012399,000111: 23,2056 64375 VLOAD MXV
012400,000112: 23,2057 02714 XNB
012401,000113: 23,2060 06260 NB2NB1
012402,000114: 23,2061 77772 VSL1
012403,000115: 23,2062 26555 STOVL XNB1
012404,000116: 23,2063 02722 YNB
012405,000117: 23,2064 76521 MXV VSL1
012406,000118: 23,2065 06260 NB2NB1
012407,000119: 23,2066 26563 STOVL YNB1
012408,000120: 23,2067 02730 ZNB
012409,000121: 23,2070 76521 MXV VSL1
012410,000122: 23,2071 06260 NB2NB1
012411,000123: 23,2072 02571 STORE ZNB1
012412,000124:
012413,000125: 23,2073 47034 RTB RTB
012414,000126: 23,2074 45662 TRANSP1
012415,000127: 23,2075 45676 TRANSP2
012416,000128:
012417,000129: 23,2076 47375 SXTANG1 VLOAD VXV
012418,000130: 23,2077 02571 ZNB1
012419,000131: 23,2100 02766 STAR
012420,000132: 23,2101 77600 BOV
012421,000133: 23,2102 46103 +1
012422,000134: 23,2103 40056 UNIT BOV
012423,000135: 23,2104 46145 ZNB=S1
012424,000136: 23,2105 00027 STORE PDA # PDA = UNIT(ZNB X S)
012425,000137:
012426,000138: 23,2106 57441 DOT DCOMP
012427,000139: 23,2107 02555 XNB1
012428,000140: 23,2110 24023 STOVL SINTH # SIN(SA) = PDA . -XNB
012429,000141: 23,2111 00027 PDA
012430,000142:
012431,000143: 23,2112 77641 DOT
012432,000144: 23,2113 02563 YNB1
012433,000145: 23,2114 34021 STCALL COSTH # COS(SA) = PDA . YNB
012434,000146: 23,2115 47256 ARCTRIG
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012436,000148: 23,2116 77634 RTB
012437,000149: 23,2117 45546 1STO2S
012438,000150: 23,2120 26774 STOVL SAC
012439,000151: 23,2121 02766 STAR
012440,000152: 23,2122 77600 BOV
012441,000153: 23,2123 46124 +1
012442,000154: 23,2124 72441 DOT SL1
012443,000155: 23,2125 02571 ZNB1
012444,000156: 23,2126 77726 ACOS
012445,000157: 23,2127 62440 BMN SL2
012446,000158: 23,2130 46142 SXTALARM # TRUNNION ANGLE NEGATIVE
012447,000159: 23,2131 45200 BOV DSU
012448,000160: 23,2132 46142 SXTALARM # TRUNNION ANGLE GREATER THAN 90 DEGREES
012449,000161: 23,2133 06331 20DEG-
012450,000162: 23,2134 77634 RTB
012451,000163: 23,2135 45546 1STO2S
012452,000164: 23,2136 02776 STORE PAC # FOR FLIGHT USE, CULTFLAG IS ON IF
012453,000165: 23,2137 77614 CLRGO # TRUNION IS GREATER THAN 90 DEG
012454,000166: 23,2140 01630 CULTFLAG
012455,000167: 23,2141 00034 28D
012456,000168: 23,2142 77614 SXTALARM SETGO # ALARM HAS BEEN REMOVED FROM THIS
012457,000169: 23,2143 01430 CULTFLAG
012458,000170: 23,2144 00034 28D # SUBROUTINE, ALARM WILL BE SET BY MPI
012459,000171: 23,2145 77745 ZNB=S1 DLOAD
012460,000172: 23,2146 06325 270DEG
012461,000173: 23,2147 16774 STODL SAC
012462,000174: 23,2150 06327 20DEGS-
012463,000175: 23,2151 02776 STORE PAC
012464,000176: 23,2152 77614 CLRGO
012465,000177: 23,2153 01630 CULTFLAG
012466,000178: 23,2154 00034 28D
012467,000179:
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012469,000181: # THESE TWO ROUTINES COMPUTE THE ACTUAL STATE VECTOR FOR LM, CSM BY ADDING
012470,000182: # THE CONIC R,V AND THE DEVIATIONS R,V. THE STATE VECTORS ARE CONVERTED TO
012471,000183: # METERS B-29 AND METERS/CSEC B-7 AND STORED APPROPRIATELY IN RN,VN OR
012472,000184: # R-OTHER, V-OTHER FOR DOWNLINK. THE ROUTINES NAMES ARE SWITCHED IN THE
012473,000185: # OTHER VEHICLES COMPUTER.
012474,000186:
012475,000187: # INPUT
012476,000188: # STATE VECTOR IN TEMPORARY STORAGE AREA
012477,000189: # IF STATE VECTOR IS SCALED POS B27 AND VEL B5
012478,000190: # SET X2 TO +2
012479,000191: # IF STATE VECTOR IS SCALED POS B29 AND VEL B7
012480,000192: # SET X2 TO 0
012481,000193:
012482,000194: # OUTPUT
012483,000195: # R(T) IN RN, V(T) IN VN, T IN PIPTIME
012484,000196: # OR
012485,000197: # R(T) IN R-OTHER, V(T) IN V-OTHER (T IS DEFINED BY T-OTHER)
012486,000198:
012487,000199: 23,2155 BANK 23
012488,000200: 10,2000 SETLOC COMGEOM2
012489,000201: 10,2000 BANK
012490,000202: 10,2237 COUNT 10/GEOM
012491,000203: 10,2237 43414 SVDWN1 BOF RVQ # SW=1=AVETOMID DOING W-MATRIX INTEG
012492,000204: 10,2240 04756 AVEMIDSW
012493,000205: 10,2241 20242 +1
012494,000206: 10,2242 53775 VLOAD VSL*
012495,000207: 10,2243 01521 TDELTAV
012496,000208: 10,2244 57605 0 -7,2
012497,000209: 10,2245 53655 VAD VSL*
012498,000210: 10,2246 01535 RCV
012499,000211: 10,2247 57576 0,2
012500,000212: 10,2250 25171 STOVL RN
012501,000213: 10,2251 01527 TNUV
012502,000214: 10,2252 53257 VSL* VAD
012503,000215: 10,2253 57602 0 -4,2
012504,000216: 10,2254 01543 VCV
012505,000217: 10,2255 77657 VSL*
012506,000218: 10,2256 57576 0,2
012507,000219: 10,2257 15177 STODL VN
012508,000220: 10,2260 01517 TET
012509,000221: 10,2261 01205 STORE PIPTIME
012510,000222: 10,2262 77616 RVQ
012511,000223:
012512,000224: 10,2263 53775 SVDWN2 VLOAD VSL*
012513,000225: 10,2264 01521 TDELTAV
012514,000226: 10,2265 57605 0 -7,2
012515,000227: 10,2266 53655 VAD VSL*
012516,000228: 10,2267 01535 RCV
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012518,000230: 10,2270 57576 0,2
012519,000231: 10,2271 25722 STOVL R-OTHER
012520,000232: 10,2272 01527 TNUV
012521,000233: 10,2273 53257 VSL* VAD
012522,000234: 10,2274 57602 0 -4,2
012523,000235: 10,2275 01543 VCV
012524,000236: 10,2276 77657 VSL*
012525,000237: 10,2277 57576 0,2
012526,000238: 10,2300 01730 STORE V-OTHER
012527,000239: 10,2301 77616 RVQ
012528,000240:
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012530,000242: # SUBROUTINE TO COMPUTE THE NATURAL LOG OF C(MPAC, MPAC +1).
012531,000243:
012532,000244: # ENTRY: CALL
012533,000245: # LOG
012534,000246:
012535,000247: # SUBROUTINE RETURNS WITH -LOG IN DP MPAC.
012536,000248:
012537,000249: # EBANK IS ARBITRARY..
012538,000250:
012539,000251: 14,2000 BANK 14
012540,000252: 23,2000 SETLOC POWFLIT2
012541,000253: 23,2000 BANK
012542,000254: 23,2155 COUNT 23/GEOM
012543,000255:
012544,000256: 23,2155 44301 LOG NORM BDSU # GENERATES LOG BY SHIFTING ARG
012545,000257: 23,2156 00160 MPAC +3 # UNTIL IT LIES BETWEEN .5 AND 1.
012546,000258: 23,2157 06212 NEARLY1 # THE LOG OF THIS PART IS FOUND AND THE
012547,000259: 23,2160 77776 EXIT # LOG OF THE SHIFTED PART IS COMPUTED
012548,000260: 23,2161 07171 TC POLY # AND ADDED IN. SHIFT COUNT STORED
012549,000261: 23,2162 00002 DEC 2 B-14 # (N-1, SUPPLIED BY SMERZH)
012550,000262: 23,2163 00000 00000 2DEC 0 B-28 # IN MPAC +3.
012551,000263: 23,2165 01001 14636 2DEC .031335467
012552,000264: 23,2167 00325 07310 2DEC .0130145859
012553,000265: 23,2171 00541 16735 2DEC .0215738898
012554,000266:
012555,000267: 23,2173 35021 CAF ZERO
012556,000268: 23,2174 54156 TS MPAC +2
012557,000269: 23,2175 00006 EXTEND
012558,000270: 23,2176 32214 DCA CLOG2/32
012559,000271: 23,2177 52155 DXCH MPAC
012560,000272: 23,2200 52160 DXCH MPAC +3
012561,000273: 23,2201 40000 COM # LOAD POSITIVE SHIFT COUNT IN A.
012562,000274: 23,2202 07256 TC SHORTMP # MULTIPLY BY SHIFT COUNT.
012563,000275:
012564,000276: 23,2203 52156 DXCH MPAC +1
012565,000277: 23,2204 52155 DXCH MPAC
012566,000278: 23,2205 52160 DXCH MPAC +3
012567,000279: 23,2206 20155 DAS MPAC
012568,000280: 23,2207 06006 TC INTPRET # RESULT IN MPAC, MPAC +1
012569,000281:
012570,000282: 23,2210 77616 RVQ
012571,000283:
012572,000284: 23,2211 37777 37777 NEARLY1 2DEC .999999999
012573,000285:
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012575,000287: 23,2213 00542 34414 CLOG2/32 2DEC .0216608494
012576,000288:
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012578,000290: # SUBROUTINE NAME: EARTH ROTATOR (EARROT1 OR EARROT2) DATE: 15 FEB 67
012579,000291: # MOD NO: N +1 LOG SECTION: POWERED FLIGHT SUBROS
012580,000292: # MOD BY: ENTRY GROUP (BAIRNSFATHER)
012581,000293:
012582,000294: # FUNCTIONAL DESCRIPTION: THIS ROUTINE PROJECTS THE INITIAL EARTH TARGET VECTOR RTINIT AHEAD THROUGH
012583,000295: # THE ESTIMATED TIME OF FLIGHT. INITIAL CALL RESOLVES THE INITIAL TARGET VECTOR RTINIT INTO EASTERLY
012584,000296: # AND NORMAL COMPONENTS RTEAST AND RTNORM. INITIAL AND SUBSEQUENT CALLS ROTATE THIS VECTOR
012585,000297: # ABOUT THE (FULL) UNIT POLAR AXIS UNITW THROUGH THE ANGLE WIE DTEAROT TO OBTAIN THE ROTATED
012586,000298: # TARGET VECTOR RT. ALL VECTORS EXCEPT UNITW ARE HALF UNIT.
012587,000299: # THE EQUATIONS ARE
012588,000300: # - - - -
012589,000301: # RT = RTINIT + RTNORM (COS(WT) - 1) + RTEAST SIN(WT)
012590,000302:
012591,000303: # WHERE WT = WIE DTEAROT
012592,000304:
012593,000305: # RTINIT = INITIAL TARGET VECTOR
012594,000306: # - - -
012595,000307: # RTEAST = UNITW * RTINIT
012596,000308: # - - -
012597,000309: # RTNORM = RTEAST * UNITW
012598,000310:
012599,000311: # FOR CONTINUOUS UPDATING, ONLY ONE ENTRY TO EARROT1 IS REQUIRED, WITH SUBSEQUENT ENTRIES AT EARROT2.
012600,000312: #
012601,000313: # CALLING SEQUENCE: FIRST CALL SUBSEQUENT CALL
012602,000314: # STCALL DTEAROT STCALL DTEAROT
012603,000315: # EARROT1 EARROT2
012604,000316: # C(MPAC) UNSPECIFIED C(MPAC) = DTEAROT
012605,000317: # PUSHLOC = PDL+0, ARBITRARY. 6 LOCATIONS USED.
012606,000318:
012607,000319: # SUBROUTINES USED: NONE
012608,000320:
012609,000321: # NORMAL EXIT MODES: RVQ
012610,000322:
012611,000323: # ALARMS: NONE
012612,000324:
012613,000325: # OUTPUT: RTEAST (-1) .5 UNIT VECTOR EAST, COMPNT OF RTINIT LEFT BY FIRST CALL
012614,000326: # RTNORM (-1) .5 UNIT VECTOR NORML, COMPNT OF RTINIT LEFT BY FIRST CALL
012615,000327: # RT (-1) .5 UNIT TARGET VECTOR, ROTATED LEFT BY ALL CALLS
012616,000328: # DTEAROT (-28) CS MAY BE CHANGED BY EARROT2, IF OVER 1 DAY
012617,000329:
012618,000330: # ERASABLE INITIALIZATION REQUIRED:
012619,000331: # UNITW (0) UNIT POLAR VECTOR PAD LOADED
012620,000332: # RTINIT (-1) .5 UNIT INITIAL TARGET VECTOR LEFT BY ENTRY
012621,000333: # DTEAROT (-28) CS TIME OF FLIGHT LEFT BY CALLER
012622,000334:
012623,000335: # DEBRIS: QPRET, PDL+0 ... PDL+5
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012625,000337: 23,2215 E7,1451 EBANK= RTINIT
012626,000338:
012627,000339: 23,2215 47375 EARROT1 VLOAD VXV
012628,000340: 23,2216 01714 UNITW # FULL UNIT VECTOR
012629,000341: 23,2217 03452 RTINIT # .5 UNIT
012630,000342: 23,2220 03460 STORE RTEAST # .5 UNIT
012631,000343:
012632,000344: 23,2221 77635 VXV
012633,000345: 23,2222 01714 UNITW # FULL UNIT
012634,000346: 23,2223 17466 STODL RTNORM # .5 UNIT
012635,000347: 23,2224 03606 DTEAROT # (-28) CS
012636,000348:
012637,000349: 23,2225 56204 EARROT2 BOVB DDV
012638,000350: 23,2226 57352 TCDANZIG # RESET OVFIND, IF ON
012639,000351: 23,2227 06256 1/WIE
012640,000352: 23,2230 41400 BOV PUSH
012641,000353: 23,2231 46245 OVERADAY
012642,000354: 23,2232 45346 COS DSU
012643,000355: 23,2233 15333 HIDPHALF
012644,000356: 23,2234 65361 VXSC PDDL # XCH W PUSH LIST
012645,000357: 23,2235 03466 RTNORM # .5 UNIT
012646,000358: 23,2236 74356 SIN VXSC
012647,000359: 23,2237 03460 RTEAST # .5 UNIT
012648,000360: 23,2240 76455 VAD VSL1
012649,000361: 23,2241 53455 VAD UNIT # INSURE THAT RT IS 'UNIT'.
012650,000362: 23,2242 03452 RTINIT # .5 UNIT
012651,000363: 23,2243 03474 STORE RT # .5 UNIT TARGET VECTOR
012652,000364:
012653,000365: 23,2244 77616 RVQ
012654,000366:
012655,000367: 23,2245 75345 OVERADAY DLOAD SIGN
012656,000368: 23,2246 06256 1/WIE
012657,000369: 23,2247 03606 DTEAROT
012658,000370: 23,2250 77621 BDSU
012659,000371: 23,2251 03606 DTEAROT
012660,000372: 23,2252 03606 STORE DTEAROT
012661,000373:
012662,000374: 23,2253 77650 GOTO
012663,000375: 23,2254 46225 EARROT2
012664,000376:
012665,000377: # WIE 2DEC .1901487997
012666,000378: 23,2255 01015 34732 1/WIE 2DEC 8616410 B-28
012667,000379: 23,2257 15373 11346 NB2NB1 2DEC +.8431756920 B-1
012668,000380: 23,2261 00000 00000 2DEC 0 B-28
012669,000381: 23,2263 67313 65307 2DEC -.5376381241 B-1
|
|
Page 295
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012671,000383: 23,2265 00000 00000 ZERINFLT 2DEC 0 B-28
012672,000384: 23,2267 20000 00000 HALFNFLT 2DEC .5
012673,000385: 23,2271 00000 00000 2DEC 0 B-28
012674,000386: 23,2273 10464 12470 2DEC +.5376381241 B-1
012675,000387: 23,2275 00000 00000 2DEC 0 B-28
012676,000388: 23,2277 15373 11346 2DEC +.8431756920 B-1
012677,000389: 23,2301 15373 11346 NB1NB2 2DEC +.8431756920 B-1
012678,000390: 23,2303 00000 00000 2DEC 0 B-28
012679,000391: 23,2305 10464 12470 2DEC +.5376381241 B-1
012680,000392: 23,2307 00000 00000 2DEC 0 B-28
012681,000393: 23,2311 20000 00000 2DEC .5
012682,000394: 23,2313 00000 00000 2DEC 0 B-28
012683,000395: 23,2315 67313 65307 2DEC -.5376381241 B-1
012684,000396: 23,2317 00000 00000 2DEC 0 B-28
012685,000397: 23,2321 15373 11346 2DEC +.8431756920 B-1
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Page 296
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012687,000399: 23,2323 07020 10DEGS- DEC 3600 B-14
012688,000400: 23,2324 60000 270DEG OCT 60000 # SHAFT 270 DEGREES 2S COMP.
012689,000401: 23,2325 00000 OCT 00000
012690,000402: 23,2326 61740 20DEGS- DEC -07199 B-14
012691,000403: 23,2327 77777 DEC -00000 B-14
012692,000404: 23,2330 07020 20DEG- DEC 03600 B-14
012693,000405: 23,2331 00000 DEC 00000 B-14
012694,000406:
End of include-file CSM_GEOMETRY.agc. Parent file is MAIN.agc