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
|
|
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. |
016776,000002: ## Copyright: Public domain.
016777,000003: ## Filename: R60,R62.agc
016778,000004: ## Purpose: Part of the source code for Colossus build 237.
016779,000005: ## This is for the Command Module's (CM) Apollo Guidance
016780,000006: ## Computer (AGC), for Apollo 8.
016781,000007: ## Assembler: yaYUL
016782,000008: ## Contact: Jim Lawton <jim DOT lawton AT gmail DOT com>
016783,000009: ## Website: www.ibiblio.org/apollo/index.html
016784,000010: ## Page Scans: www.ibiblio.org/apollo/ScansForConversion/Colossus237/
016785,000011: ## Mod history: 2011-01-27 JL Adapted from corresponding Colossus 249 file.
016786,000012: ## 2016-12-30 RSB Proofed comment text using octopus/ProoferComments,
016787,000013: ## and corrected errors found.
016788,000014: ## 2021-05-30 ABS Removed STORANG symbol not present in scans.
016789,000015:
|
|
Page 381 |
016791,000017: 34,2002 BANK 34
016792,000018: 27,2000 SETLOC MANUVER
016793,000019: 27,2000 BANK
016794,000020:
016795,000021: 27,2000 1146 EBANK= TEMPR60
016796,000022:
016797,000023: 27,2000 COUNT 27/R60
016798,000024:
016799,000025:
016800,000026: # R60CSM
016801,000027: # REV 13 CONFORMS TO GSOP CHAPTER FOUR REVISION LOGIC 09 JAN 18,1968
016802,000028:
016803,000029:
016804,000030:
016805,000031: 27,2000 04604 R60CSM TC MAKECADR
016806,000032: 27,2001 55146 TS TEMPR60
016807,000033:
016808,000034: # INSERT PRIODSP CHECK WITH R22 (V06N49) WITH JENNINGS BRODEUR
016809,000035:
016810,000036: 27,2002 34705 REDOMANN CAF BIT6
016811,000037: 27,2003 70101 MASK FLAGWRD5 # IS 3-AXIS FLAG SET
016812,000038: 27,2004 10000 CCS A
016813,000039: 27,2005 12013 TCF TOBALL # YES
016814,000040: 27,2006 06006 TC INTPRET
016815,000041: 27,2007 77624 CALL
016816,000042: 27,2010 56126 VECPOINT # TO COMPUTE FINAL ANGLES
016817,000043: 27,2011 01156 STORE CPHI # STORE FINAL ANGLES - CPHI,CTHETA,CPSI
016818,000044: 27,2012 77776 EXIT
016819,000045:
016820,000046: 27,2013 32125 TOBALL CAF V06N18
016821,000047: 27,2014 04555 TC BANKCALL
016822,000048: 27,2015 21036 CADR GOPERF2R # DISPLAY PLEASE PERFORM AUTO MANEUVER
016823,000049: 27,2016 02114 TC R61TEST
016824,000050: 27,2017 02023 TC REDOMANC # PROCEED
016825,000051: 27,2020 12052 TCF ENDMANU1 # ENTER I.E. FINISHED WITH R60
016826,000052:
016827,000053: 27,2021 02056 TC CHKLINUS # TO CHECK FOR PRIORITY DISPLAYS
016828,000054: 27,2022 05112 TC ENDOFJOB
016829,000055:
016830,000056: 27,2023 34705 REDOMANC CAF BIT6
016831,000057: 27,2024 70101 MASK FLAGWRD5 # IS 3-AXIS FLAG SET
016832,000058: 27,2025 10000 CCS A
016833,000059: 27,2026 12034 TCF TOBALLC # YES
016834,000060: 27,2027 06006 TC INTPRET
016835,000061: 27,2030 77624 CALL
016836,000062: 27,2031 56126 VECPOINT # TO COMPUTE FINAL ANGLES
016837,000063: 27,2032 01156 STORE CPHI # STORE ANGLES
016838,000064: 27,2033 77776 EXIT
016839,000065:
016840,000066: 27,2034 34371 TOBALLC CAF PRIO30 # IS MODE AUTO AND CTL GNC
|
|
Page 382 |
016842,000068: 27,2035 00006 EXTEND
016843,000069: 27,2036 06031 RXOR CHAN31
016844,000070: 27,2037 77707 MASK 13,14,15
016845,000071: 27,2040 00006 EXTEND
016846,000072: 27,2041 12043 BZF +2 # AUTO, NON-FLASH N18
016847,000073: 27,2042 12013 TCF TOBALL # NOT AUTO
016848,000074:
016849,000075: 27,2043 32125 CAF V06N18 # SET UP NON-FLASHING V06 N18
016850,000076: 27,2044 04555 TC BANKCALL
016851,000077: 27,2045 20602 CADR GODSPR
016852,000078: 27,2046 02056 TC CHKLINUS
016853,000079:
016854,000080: 27,2047 04555 STARTMNV TC BANKCALL
016855,000081: 27,2050 17547 CADR GOMANUR
016856,000082: 27,2051 12013 ENDMANUV TCF TOBALL # FINISHED MANEUVER
016857,000083:
016858,000084: 27,2052 05447 ENDMANU1 TC DOWNFLAG # RESET 3-AXIS FLAG
016859,000085: 27,2053 00124 ADRES 3AXISFLG # BIT 6 FLAG 5
016860,000086: 27,2054 31146 CAE TEMPR60 # -
016861,000087: 27,2055 04577 TC BANKJUMP # -
016862,000088:
016863,000089: 27,2056 40100 CHKLINUS CS FLAGWRD4
016864,000090: 27,2057 74677 MASK BIT12 # IS PRIORITY DISPLAY FLAG SET -
016865,000091: 27,2060 10000 CCS A # -
016866,000092: 27,2061 00002 TC Q # NO - EXIT
016867,000093: 27,2062 30002 CA Q
016868,000094: 27,2063 54156 TS MPAC +2 # SAVE RETURN
016869,000095: 27,2064 46214 CS THREE # OBTAIN LOCATION FOR RESTART.
016870,000096: 27,2065 60133 AD BUF2 # HOLDS Q OF LAST DISPALY
016871,000097: 27,2066 55053 TS TBASE1
016872,000098:
016873,000099: 27,2067 05301 TC PHASCHNG
016874,000100: 27,2070 00071 OCT 71 # 1.7SPOT FOR RELINUS
016875,000101: 27,2071 34704 CAF BIT7
016876,000102: 27,2072 05415 TC LINUS # GO SET BITS FOR PRIORITY DISPLAY -
016877,000103: 27,2073 00156 TC MPAC +2
016878,000104:
016879,000105: 27,2074 34706 RELINUS CAF BIT5 # IS TRACK FLAG ON
016880,000106: 27,2075 70075 MASK FLAGWRD1
016881,000107: 27,2076 00006 EXTEND
016882,000108: 27,2077 12111 BZF GOREDO20 # NO
016883,000109:
016884,000110: 27,2100 05435 TC UPFLAG
016885,000111: 27,2101 00077 ADRES PDSPFLAG # R60 PRIODSP FLAG
016886,000112:
016887,000113: 27,2102 05435 TC UPFLAG
016888,000114: 27,2103 00024 ADRES TARG1FLG # FOR R52
016889,000115:
016890,000116: 27,2104 34714 CAF ZERO # RESET TO ZERO, SINCE
|
|
Page 383 |
016892,000118: 27,2105 55303 TS OPTIND # OPTIND WAS SET TO -1 BY V379
016893,000119:
016894,000120: 27,2106 34761 CAF PRIO14 # RESTORE ORIGINAL PRIORITY
016895,000121: 27,2107 05103 TC PRIOCHNG
016896,000122:
016897,000123: 27,2110 01053 TC TBASE1
016898,000124:
016899,000125: 27,2111 05301 GOREDO20 TC PHASCHNG
016900,000126: 27,2112 00111 OCT 111 # 1.11 FOR PIKUP20
016901,000127:
016902,000128: 27,2113 05112 TC ENDOFJOB
016903,000129:
016904,000130: 27,2114 31011 R61TEST CA MODREG # ARE WE IN P00. IF YES THIS MUST BE
016905,000131: 27,2115 00006 EXTEND # VERB49 OR VERB89 SO DO ENDEXT.
016906,000132: 27,2116 12052 BZF ENDMANU1 # RESET 3-AXIS & RUTURN. USER DOES ENDEXT
016907,000133: 27,2117 30100 CA FLAGWRD4 # ARE WE IN R61 (P20)
016908,000134: 27,2120 74677 MASK BIT12
016909,000135: 27,2121 00006 EXTEND
016910,000136: 27,2122 14106 BZF GOTOPOOH # NO
016911,000137: 27,2123 04550 TC GOTOV56 # YES
016912,000138:
016913,000139: 27,2124 20100 BIT14+7 OCT 20100 # -
016914,000140: 27,2125 01422 V06N18 VN 0618
016915,000141:
|
|
Page 384 |
016917,000143: # PROGRAM DESCRIPTION - VECPOINT
016918,000144:
016919,000145:
016920,000146: # THIS INTERPRETIVE SUBROUTINE MAY BE USED TO POINT A SPACECRAFT AXIS IN A DESIRED DIRECTION. THE AXIS
016921,000147: # TO BE POINTED MUST APPEAR AS A HALF UNIT DOUBLE PRECISION VECTOR IN SUCCESSIVE LOCATIONS OF ERASABLE MEMORY
016922,000148: # BEGINNING WITH THE LOCATION CALLED SCAXIS. THE COMPONENTS OF THIS VECTOR ARE GIVEN IN SPACECRAFT COORDINATES.
016923,000149: # THE DIRECTION IN WHICH THIS AXIS IS TO BE POINTED MUST APPEAR AS A HALF UNIT DOUBLE PRECISION VECTOR IN
016924,000150: # SUCCESSIVE LOCATIONS OF ERASABLE MEMORY BEGINNING WITH THE ADDRESS CALLED POINTVSM. THE COMPONENTS OF THIS
016925,000151: # VECTOR ARE GIVEN IN STABLE MEMBER COORDINATES. WITH THIS INFORMATION VECPOINT COMPUTES A SET OF THREE GIMBAL
016926,000152: # ANGLES (2S COMPLEMENT) CORRESPONDING TO THE CROSS-PRODUCT ROTATION BETWEEN SCAXIS AND POINTVSM AND STORES THEM
016927,000153: # IN T(MPAC) BEFORE RETURNING TO THE CALLER.
016928,000154: # THIS ROTATION, HOWEVER, MAY BRING THE S/C INTO GIMBAL LOCK. WHEN POINTING A VECTOR IN THE Y-Z PLANE,
016929,000155: # THE TRANSPONDER AXIS, OR THE AOT FOR THE LEM, THE PROGRAM WILL CORRECT THIS PROBLEM BY ROTATING THE CROSS-
016930,000156: # PRODUCT ATTITUDE ABOUT POINTVSM BY A FIXED AMOUNT SUFFICIENT TO ROTATE THE DESIRED S/C ATTITUDE OUT OF GIMBAL
016931,000157: # LOCK. IF THE AXIS TO BE POINTED IS MORE THAN 40.6 DEGREES BUT LESS THAN 60.5 DEG FROM THE +X (OR-X) AXIS,
016932,000158: # THE ADDITIONAL ROTATION TO AVOID GIMAL LOCK IS 35 DEGREES. IF THE AXIS IS MORE THAN 60.5 DEGEES FROM +X (OR -X)
016933,000159: # THE ADDITIONAL ROTATION IS 35 DEGREES. THE GIMBAL ANGLES CORRESPONDING TO THIS ATTITUDE ARE THEN COMPUTED AND
016934,000160: # STORED AS 2S COMPLIMENT ANGLES IN T(MPAC) BEFORE RETURNING TO THE CALLER.
016935,000161: # WHEN POINTING THE X-AXIS, OR THE THRUST VECTOR, OR ANY VECTOR WITHIN 40.6 DEG OF THE X-AXIS, VECPOINT
016936,000162: # CANNOT CORRECT FOR A CROSS-PRODUCT ROTATION INTO GIMBAL LOCK. IN THIS CASE A PLATFORM REALIGNMENT WOULD BE
016937,000163: # REQUIRED TO POINT THE VECTOR IN THE DESIRED DIRECTION. AT PRESENT NO INDICATION IS GIVEN FOR THIS SITUATION
016938,000164: # EXCEPT THAT THE FINAL MIDDLE GIMBAL ANGLE IN MPAC +2 IS GREATER THAN 59 DEGREES.
016939,000165:
016940,000166: # CALLING SEQUENCE -
016941,000167: # 1) LOAD SCAXIS, POINTVSM
016942,000168: # 2) CALL
016943,000169: # VECPOINT
016944,000170:
016945,000171: # RETURNS WITH
016946,000172:
016947,000173: # 1) DESIRED OUTER GIMBAL ANGLE IN MPAC
016948,000174: # 2) DESIRED INNER GIMBAL ANGLE IN MPAC +1
016949,000175: # 3) DESIRED MIDDLE GIMBAL ANGLE IN MPAC +2
016950,000176:
016951,000177:
016952,000178: # ERASABLES USED -
016953,000179:
016954,000180: # 1) SCAXIS 6
016955,000181: # 2) POINTVSM 6
016956,000182: # 3) MIS 18
016957,000183: # 4) DEL 18
016958,000184: # 5) COF 6
016959,000185: # 6) VECQTEMP 1
016960,000186: # 7) ALL OF VAC AREA 43
016961,000187:
016962,000188: # TOTAL 99
016963,000189:
016964,000190:
016965,000191: 27,2000 SETLOC VECPT
016966,000192: 27,2000 BANK
|
|
Page 385 |
016968,000194: 27,2126 E6,1661 EBANK= BCDU
016969,000195:
016970,000196: 27,2126 COUNT 27/VECPT
016971,000197:
016972,000198: 27,2126 40020 VECPOINT STQ BOV # SAVE RETURN ADDRESS
016973,000199: 27,2127 03310 VECQTEMP
016974,000200: 27,2130 56131 VECLEAR # AND CLEAR OVFIND
016975,000201: 27,2131 47164 VECLEAR AXC,2 RTB
016976,000202: 27,2132 03320 MIS # READ THE PRESENT CDU ANGLES AND
016977,000203: 27,2133 44376 READCDUK # STORE THEM IN PD25, 26, 27
016978,000204: 27,2134 34032 STCALL 25D
016979,000205: 27,2135 44405 CDUTODCM # S/C AXES TO STABLE MEMBER AXES (MIS)
016980,000206: 27,2136 61375 VLOAD VXM
016981,000207: 27,2137 03357 POINTVSM # RESOLVE THE POINTING DIRECTION VF INTO
016982,000208: 27,2140 03321 MIS # INITIAL S/C AXES ( VF = POINTVSM)
016983,000209: 27,2141 77656 UNIT
016984,000210: 27,2142 00035 STORE 28D
016985,000211: # PD 28 29 30 31 32 33
016986,000212: 27,2143 53435 VXV UNIT # TAKE THE CROSS PRODUCT VF X VI
016987,000213: 27,2144 03351 SCAXIS # WHERE VI = SCAXIS
016988,000214: 27,2145 57400 BOV VCOMP
016989,000215: 27,2146 56256 PICKAXIS
016990,000216: 27,2147 17343 STODL COF # CHECK MAGNITUDE
016991,000217: 27,2150 00045 36D # OF CROSS PRODUCT
016992,000218: 27,2151 50025 DSU BMN # VECTOR, IF LESS
016993,000219: 27,2152 16327 DPB-14 # THAN B-14 ASSUME
016994,000220: 27,2153 56256 PICKAXIS # UNIT OPERATION
016995,000221: 27,2154 50375 VLOAD DOT # INVALID.
016996,000222: 27,2155 03351 SCAXIS
016997,000223: 27,2156 00035 28D
016998,000224: 27,2157 65552 SL1 ARCCOS
016999,000225: 27,2160 77624 COMPMATX CALL # NOW COMPUTE THE TRANSFORMATION FROM
017000,000226: 27,2161 44530 DELCOMP # FINAL S/C AXES TO INITIAL S/C AXES MFI
017001,000227: 27,2162 75160 AXC,1 AXC,2
017002,000228: 27,2163 03320 MIS # COMPUTE THE TRANSFORMATION FROM FINAL
017003,000229: 27,2164 03425 DEL # S/C AXES TO STABLE MEMBER AXES
017004,000230: 27,2165 77624 CALL # MFS = MIS MFI
017005,000231: 27,2166 44304 MXM3 # (IN PD LIST)
017006,000232:
017007,000233: 27,2167 51545 DLOAD ABS
017008,000234: 27,2170 00007 6 # MFS6 = SIN(CPSI) $2
017009,000235: 27,2171 50025 DSU BMN
017010,000236: 27,2172 16314 SINGIMLC # = SIN(59 DEGS) $2
017011,000237: 27,2173 56246 FINDGIMB # /CPSI/ LESS THAN 59 DEGS
017012,000238: # I.E. DESIRED ATTITUDE NOT IN GIMBAL LOCK
017013,000239:
017014,000240: 27,2174 51545 DLOAD ABS # CHECK TO SEE IF WE ARE POINTING
017015,000241: 27,2175 03351 SCAXIS # THE THRUST AXIS
017016,000242: 27,2176 51025 DSU BPL
017017,000243: 27,2177 16316 SINVEC1 # SIN 49.4 DEGS $2
|
|
Page 386 |
017019,000245: 27,2200 56246 FINDGIMB # IF SO, WE ARE TRYING TO POINT IT INTO
017020,000246: 27,2201 77775 VLOAD # GIMBAL LOCK, ABORT COULD GO HERE
017021,000247: 27,2202 77626 STADR
017022,000248: 27,2203 50442 STOVL MIS +12D
017023,000249: 27,2204 77626 STADR # STORE MFS (IN PD LIST) IN MIS
017024,000250: 27,2205 50450 STOVL MIS +6
017025,000251: 27,2206 77626 STADR
017026,000252: 27,2207 50456 STOVL MIS
017027,000253: 27,2210 03327 MIS +6 # INNER GIMBAL AXIS IN FINAL S/C AXES
017028,000254: 27,2211 57444 BPL VCOMP # LOCATE THE IG AXIS DIRECTION CLOSEST TO
017029,000255: 27,2212 56213 IGSAMEX # FINAL X S/C AXIS
017030,000256:
017031,000257: 27,2213 50035 IGSAMEX VXV BMN # FIND THE SHORTEST WAY OF ROTATING THE
017032,000258: 27,2214 03351 SCAXIS # S/C OUT OF GIMBAL LOCK BY A ROTATION
017033,000259: 27,2215 56222 U=SCAXIS # ABOUT +- SCAXIS, I.E. IF (IG (SGN MFS3)
017034,000260: # X SCAXIS . XF) LESS THAN 0, U = SCAXIS
017035,000261: # OTHERWISE U = -SCAXIS
017036,000262:
017037,000263: 27,2216 57575 VLOAD VCOMP
017038,000264: 27,2217 03351 SCAXIS
017039,000265: 27,2220 37343 STCALL COF # ROTATE ABOUT -SCAXIS
017040,000266: 27,2221 56225 CHEKAXIS
017041,000267: 27,2222 77775 U=SCAXIS VLOAD
017042,000268: 27,2223 03351 SCAXIS
017043,000269: 27,2224 03343 STORE COF # ROTATE ABOUT + SCAXIS
017044,000270: 27,2225 51545 CHEKAXIS DLOAD ABS
017045,000271: 27,2226 03351 SCAXIS # SEE IF WE ARE POINTING THE AOT
017046,000272: 27,2227 51025 DSU BPL
017047,000273: 27,2230 16320 SINVEC2 # SIN 29.5 DEGS $2
017048,000274: 27,2231 56235 PICKANG1 # IF SO, ROTATE 50 DEGS ABOUT +- SCAXIS
017049,000275: 27,2232 52145 DLOAD GOTO # IF NOT, MUST BE POINTING THE TRANSPONDER
017050,000276: 27,2233 16324 VECANG2 # OR SOME VECTOR IN THE Y, OR Z PLANE
017051,000277: 27,2234 56237 COMPMFSN # IN THIS CASE ROTATE 35 DEGS TO GET OUT
017052,000278: # OF GIMBAL LOCK (VECANG2 $360)
017053,000279: 27,2235 77745 PICKANG1 DLOAD
017054,000280: 27,2236 16322 VECANG1 # = 50 DEGS $ 360
017055,000281: 27,2237 77624 COMPMFSN CALL
017056,000282: 27,2240 44530 DELCOMP # COMPUTE THE ROTATION ABOUT SCAXIS TO
017057,000283: 27,2241 75160 AXC,1 AXC,2 # BRING MFS OUT OF GIMBAL LOCK
017058,000284: 27,2242 03320 MIS
017059,000285: 27,2243 03425 DEL
017060,000286: 27,2244 77624 CALL # COMPUTE THE NEW TRANSFORMATION FROM
017061,000287: 27,2245 44304 MXM3 # DESIRED S/C AXES TO STABLE MEMBER AXES
017062,000288: # WHICH WILL ALIGN VI WITH VF AND AVOID
017063,000289: # GIMBAL LOCK
017064,000290: 27,2246 45160 FINDGIMB AXC,1 CALL
017065,000291: 27,2247 00000 0 # EXTRACT THE COMMANDED CDU ANGLES FROM
017066,000292: 27,2250 44655 DCMTOCDU # THIS MATRIX
017067,000293: 27,2251 40234 RTB SETPD
017068,000294: 27,2252 45547 V1STO2S # CONVERT TO 2:S COMPLEMENT
|
|
Page 387 |
017070,000296: 27,2253 00001 0
017071,000297: 27,2254 77650 GOTO
017072,000298: 27,2255 03310 VECQTEMP # RETURN TO CALLER
017073,000299:
017074,000300: 27,2256 50375 PICKAXIS VLOAD DOT # IF VF X VI = 0, FIND VF . VI
017075,000301: 27,2257 00035 28D
017076,000302: 27,2260 03351 SCAXIS
017077,000303: 27,2261 72240 BMN TLOAD
017078,000304: 27,2262 56266 ROT180
017079,000305: 27,2263 00032 25D
017080,000306: 27,2264 77650 GOTO # IF VF = VI, CDU DESIRED = PRESENT CDU
017081,000307: 27,2265 03310 VECQTEMP # PRESENT CDU ANGLES
017082,000308:
017083,000309: 27,2266 47375 ROT180 VLOAD VXV # IF VF, VI ANTIPARALLEL, 180 DEG ROTATION
017084,000310: 27,2267 03327 MIS +6 # IS REQUIRED. Y STABLE MEMBER AXIS IN
017085,000311: 27,2270 15330 HIUNITX # INITIAL S/C AXIS.
017086,000312: 27,2271 47256 UNIT VXV # FIND Y(SM) X X(I)
017087,000313: 27,2272 03351 SCAXIS # FIND UNIT(VI X UNIT(Y(SM) X X(I)))
017088,000314: 27,2273 40056 UNIT BOV # I.E. PICK A VECTOR IN THE PLANE OF X(I),
017089,000315: 27,2274 56310 PICKX # Y(SM) PERPENDICULAR TO VI
017090,000316: 27,2275 17343 STODL COF
017091,000317: 27,2276 00045 36D # CHECK MAGNITUDE
017092,000318: 27,2277 50025 DSU BMN # OF THIS VECTOR.
017093,000319: 27,2300 16327 DPB-14 # IF LESS THAN B-14,
017094,000320: 27,2301 56310 PICKX # PICK X-AXIS.
017095,000321: 27,2302 77775 VLOAD
017096,000322: 27,2303 03343 COF
017097,000323: 27,2304 17343 XROT STODL COF
017098,000324: 27,2305 15330 HIDPHALF
017099,000325: 27,2306 77650 GOTO
017100,000326: 27,2307 56160 COMPMATX
017101,000327: 27,2310 52175 PICKX VLOAD GOTO # PICK THE XAXIS IN THIS CASE
017102,000328: 27,2311 15330 HIUNITX
017103,000329: 27,2312 56304 XROT
017104,000330: 35,2000 BANK 35
017105,000331: 27,2000 SETLOC MANUVER1
017106,000332: 27,2000 BANK
017107,000333:
017108,000334: 27,2313 15555 35172 SINGIMLC 2DEC .4285836003 # =SIN(59) $2
017109,000335: 27,2315 14113 36326 SINVEC1 2DEC .3796356537 # =SIN(49.4) $2
017110,000336: 27,2317 07701 35703 SINVEC2 2DEC .2462117800 # =SIN(29.5) $2
017111,000337: 27,2321 04343 21616 VECANG1 2DEC .1388888889 # = 50 DEGREES $360
017112,000338: 27,2323 03070 34344 VECANG2 2DEC .09722222222 # = 35 DEGREES $360
017113,000339: 27,2325 00000 1BITDP OCT 0 # KEEP THIS BEFORE DPB(-14) *********
017114,000340: 27,2326 00001 DPB-14 OCT 00001
|
|
Page 388 |
017116,000342: 27,2327 00000 OCT 00000
017117,000343: 34,2002 BANK 34
017118,000344: 27,2000 SETLOC MANUVER
017119,000345: 27,2000 BANK
017120,000346:
|
|
Page 389 |
017122,000348: # ROUTINE FOR INITIATING AUTOMATIC MANEUVER VIA KEYBOARD (V49)
017123,000349:
017124,000350:
017125,000351: 27,2330 1155 EBANK= CPHI
017126,000352:
017127,000353: 27,2330 COUNT 27/R62
017128,000354:
017129,000355: 27,2330 34745 R62DISP CAF V06N22 # DISPLAY COMMAND ICDUS CPHI, CTHETA, CPHI
017130,000356: 27,2331 04555 TC BANKCALL
017131,000357: 27,2332 20624 CADR GOFLASH
017132,000358: 27,2333 15423 TCF ENDEXT
017133,000359: 27,2334 12336 TCF GOMOVE # PROCEED
017134,000360: 27,2335 12330 TCF R62DISP # ENTER
017135,000361:
017136,000362:
017137,000363: # ASTRONAUT MAY LOAD NEW ICDUS AT THIS
017138,000364: # POINT
017139,000365: 27,2336 05435 GOMOVE TC UPFLAG # SET 3-AXIS FLAG
017140,000366: 27,2337 00124 ADRES 3AXISFLG # BIT 6 FLAG 5
017141,000367:
017142,000368: 27,2340 04555 TC BANKCALL
017143,000369: 27,2341 56000 CADR R60CSM
017144,000370: 27,2342 15423 TCF ENDEXT
End of include-file R60,R62.agc. Parent file is MAIN.agc