Source Code
|
These source-code files are part of a reconstructed copy of Comanche 051, the
original release of the Apollo 11 Command Module (CM) Apollo Guidance Computer
(AGC) software.
The reconstruction began with source code of Comanche 055 previously transcribed
from a digitized copy of that program. The code was then updated by undoing
changes related to the R-2 lunar potential model, using hints from program
comments and change-indicating asterisks in the Comanche 055 listing as a guide.
The reconstruction was verified by matching memory-bank checksums to those listed
in drawing 2021153D. Note that page numbers in the reconstructed code match those
on the Comanche 055 printout, although the added code would likely have changed page
numbers for a real Comanche 051 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.
|
016659,000002: ## Copyright: Public domain.
016660,000003: ## Filename: R60,R62.agc
016661,000004: ## Purpose: A section of Comanche revision 051.
016662,000005: ## It is part of the reconstructed source code for the
016663,000006: ## original release of the flight software for the Command
016664,000007: ## Module's (CM) Apollo Guidance Computer (AGC) for Apollo 11.
016665,000008: ## The code has been recreated from a copy of Comanche 055. It
016666,000009: ## has been adapted such that the resulting bugger words
016667,000010: ## exactly match those specified for Comanche 51 in NASA drawing
016668,000011: ## 2021153D, which gives relatively high confidence that the
016669,000012: ## reconstruction is correct.
016670,000013: ## Reference: pp. 390-398
016671,000014: ## Assembler: yaYUL
016672,000015: ## Contact: Ron Burkey <info@sandroid.org>.
016673,000016: ## Website: www.ibiblio.org/apollo/index.html
016674,000017: ## Mod history: 2019-07-30 MAS Created from Comanche 55.
016675,000018:
|
|
Page 390
|
016677,000020: 34,2002 BANK 34
016678,000021: 27,2000 SETLOC MANUVER
016679,000022: 27,2000 BANK
016680,000023:
016681,000024: 27,2000 1146 EBANK= TEMPR60
016682,000025:
016683,000026: 27,2000 COUNT 27/R60
016684,000027:
016685,000028: # R60CSM
016686,000029: # REV 13 CONFORMS TO GSOP CHAPTER FOUR REVISION LOGIC 09 JAN 18, 1968
016687,000030:
016688,000031: 27,2000 04711 R60CSM TC MAKECADR
016689,000032: 27,2001 55146 TS TEMPR60
016690,000033:
016691,000034: # INSERT PRIODSP CHECK WITH R22 (V06N49) WITH JENNINGS BRODEUR
016692,000035:
016693,000036: 27,2002 35012 REDOMANN CAF BIT6
016694,000037: 27,2003 70101 MASK FLAGWRD5 # IS 3-AXIS FLAG SET
016695,000038: 27,2004 10000 CCS A
016696,000039: 27,2005 12013 TCF TOBALL # YES
016697,000040: 27,2006 06006 TC INTPRET
016698,000041: 27,2007 77624 CALL
016699,000042: 27,2010 56126 VECPOINT # TO COMPUTE FINAL ANGLES
016700,000043: 27,2011 01156 STORE CPHI # STORE FINAL ANGLES - CPHI, CTHETA, CPSI
016701,000044: 27,2012 77776 EXIT
016702,000045:
016703,000046: 27,2013 32125 TOBALL CAF V06N18
016704,000047: 27,2014 04662 TC BANKCALL
016705,000048: 27,2015 21132 CADR GOPERF2R # DISPLAY PLEASE PERFORM AUTO MANEUVER
016706,000049: 27,2016 02114 TC R61TEST
016707,000050: 27,2017 02023 TC REDOMANC # PROCEED
016708,000051: 27,2020 12052 TCF ENDMANU1 # ENTER I.E. FINISHED WITH R60
016709,000052:
016710,000053: 27,2021 02056 TC CHKLINUS # TO CHECK FOR PRIORITY DISPLAYS
016711,000054: 27,2022 05217 TC ENDOFJOB
016712,000055:
016713,000056: 27,2023 35012 REDOMANC CAF BIT6
016714,000057: 27,2024 70101 MASK FLAGWRD5 # IS 3-AXIS FLAG SET
016715,000058: 27,2025 10000 CCS A
016716,000059: 27,2026 12034 TCF TOBALLC # YES
016717,000060: 27,2027 06006 TC INTPRET
016718,000061: 27,2030 77624 CALL
016719,000062: 27,2031 56126 VECPOINT # TO COMPUTE FINAL ANGLES
016720,000063: 27,2032 01156 STORE CPHI # STORE ANGLES
016721,000064: 27,2033 77776 EXIT
016722,000065:
016723,000066: 27,2034 34371 TOBALLC CAF PRIO30 # IS MODE AUTO AND CTL GNC
|
|
Page 391
|
016725,000068: 27,2035 00006 EXTEND
016726,000069: 27,2036 06031 RXOR CHAN31
016727,000070: 27,2037 77707 MASK 13,14,15
016728,000071: 27,2040 00006 EXTEND
016729,000072: 27,2041 12043 BZF +2 # AUTO, NON-FLASH N18
016730,000073: 27,2042 12013 TCF TOBALL # NOT AUTO
016731,000074:
016732,000075: 27,2043 32125 CAF V06N18 # SET UP NON-FLASHING V06 N18
016733,000076: 27,2044 04662 TC BANKCALL
016734,000077: 27,2045 20676 CADR GODSPR
016735,000078: 27,2046 02056 TC CHKLINUS
016736,000079:
016737,000080: 27,2047 04662 STARTMNV TC BANKCALL
016738,000081: 27,2050 17627 CADR GOMANUR
016739,000082: 27,2051 12013 ENDMANUV TCF TOBALL # FINISHED MANEUVER
016740,000083:
016741,000084: 27,2052 05560 ENDMANU1 TC DOWNFLAG # RESET 3-AXIS FLAG
016742,000085: 27,2053 00124 ADRES 3AXISFLG # BIT 6 FLAG 5
016743,000086: 27,2054 31146 CAE TEMPR60 # -
016744,000087: 27,2055 04704 TC BANKJUMP # -
016745,000088:
016746,000089: 27,2056 40100 CHKLINUS CS FLAGWRD4
016747,000090: 27,2057 75004 MASK BIT12 # IS PRIORITY DISPLAY FLAG SET -
016748,000091: 27,2060 10000 CCS A # -
016749,000092: 27,2061 00002 TC Q # NO - EXIT
016750,000093: 27,2062 30002 CA Q
016751,000094: 27,2063 54156 TS MPAC +2 # SAVE RETURN
016752,000095: 27,2064 46214 CS THREE # OBTAIN LOCATION FOR RESTART.
016753,000096: 27,2065 60133 AD BUF2 # HOLDS Q OF LAST DISPALY
016754,000097: 27,2066 55053 TS TBASE1
016755,000098:
016756,000099: 27,2067 05412 TC PHASCHNG
016757,000100: 27,2070 00071 OCT 71 # 1.7SPOT FOR RELINUS
016758,000101:
016759,000102: 27,2071 35011 CAF BIT7
016760,000103: 27,2072 05526 TC LINUS # GO SET BITS FOR PRIORITY DISPLAY -
016761,000104: 27,2073 00156 TC MPAC +2
016762,000105:
016763,000106: 27,2074 35013 RELINUS CAF BIT5 # IS TRACK FLAG ON
016764,000107: 27,2075 70075 MASK FLAGWRD1
016765,000108: 27,2076 00006 EXTEND
016766,000109: 27,2077 12111 BZF GOREDO20 # NO
016767,000110:
016768,000111: 27,2100 05546 TC UPFLAG
016769,000112: 27,2101 00077 ADRES PDSPFLAG # R60 PRIODSP FLAG
016770,000113:
016771,000114: 27,2102 05546 TC UPFLAG
016772,000115: 27,2103 00024 ADRES TARG1FLG # FOR R52
016773,000116:
016774,000117: 27,2104 35021 CAF ZERO # RESET TO ZERO, SINCE
|
|
Page 392
|
016776,000119: 27,2105 55303 TS OPTIND # OPTIND WAS SET TO -1 BY V379
016777,000120:
016778,000121: 27,2106 35066 CAF PRIO14 # RESTORE ORIGINAL PRIORITY
016779,000122: 27,2107 05210 TC PRIOCHNG
016780,000123:
016781,000124: 27,2110 01053 TC TBASE1
016782,000125:
016783,000126: 27,2111 05412 GOREDO20 TC PHASCHNG
016784,000127: 27,2112 00111 OCT 111 # 1.11 FOR PIKUP20
016785,000128:
016786,000129: 27,2113 05217 TC ENDOFJOB
016787,000130:
016788,000131: 27,2114 31011 R61TEST CA MODREG # ARE WE IN P00. IF YES THIS MUST BE
016789,000132: 27,2115 00006 EXTEND # VERB49 OR VERB89 SO DO ENDEXT.
016790,000133: 27,2116 12052 BZF ENDMANU1 # RESET 3-AXIS & RUTURN. USER DOES ENDEXT
016791,000134: 27,2117 30100 CA FLAGWRD4 # ARE WE IN R61 (P20)
016792,000135: 27,2120 75004 MASK BIT12
016793,000136: 27,2121 00006 EXTEND
016794,000137: 27,2122 14106 BZF GOTOPOOH # NO
016795,000138: 27,2123 04622 TC GOTOV56 # YES
016796,000139:
016797,000140: 27,2124 20100 BIT14+7 OCT 20100 # -
016798,000141: 27,2125 01422 V06N18 VN 0618
016799,000142:
|
|
Page 393
|
016801,000144: # PROGRAM DESCRIPTION - VECPOINT
016802,000145:
016803,000146: # THIS INTERPRETIVE SUBROUTINE MAY BE USED TO POINT A SPACECRAFT AXIS IN A DESIRED DIRECTION. THE AXIS
016804,000147: # TO BE POINTED MUST APPEAR AS A HALF UNIT DOUBLE PRECISION VECTOR IN SUCCESSIVE LOCATIONS OF ERASABLE MEMORY
016805,000148: # BEGINNING WITH THE LOCATION CALLED SCAXIS. THE COMPONENTS OF THIS VECTOR ARE GIVEN IN SPACECRAFT COORDINATES.
016806,000149: # THE DIRECTION IN WHICH THIS AXIS IS TO BE POINTED MUST APPEAR AS A HALF UNIT DOUBLE PRECISION VECTOR IN
016807,000150: # SUCCESSIVE LOCATIONS OF ERASABLE MEMORY BEGINNING WITH THE ADDRESS CALLED POINTVSM. THE COMPONENTS OF THIS
016808,000151: # VECTOR ARE GIVEN IN STABLE MEMBER COORDINATES. WITH THIS INFORMATION VECPOINT COMPUTES A SET OF THREE GIMBAL
016809,000152: # ANGLES (2S COMPLEMENT) CORRESPONDING TO THE CROSS-PRODUCT ROTATION BETWEEN SCAXIS AND POINTVSM AND STORES THEM
016810,000153: # IN T(MPAC) BEFORE RETURNING TO THE CALLER.
016811,000154:
016812,000155: # THIS ROTATION, HOWEVER, MAY BRING THE S/C INTO GIMBAL LOCK. WHEN POINTING A VECTOR IN THE Y-Z PLANE,
016813,000156: # THE TRANSPONDER AXIS, OR THE AOT FOR THE LEM, THE PROGRAM WILL CORRECT THIS PROBLEM BY ROTATING THE CROSS-
016814,000157: # PRODUCT ATTITUDE ABOUT POINTVSM BY A FIXED AMOUNT SUFFICIENT TO ROTATE THE DESIRED S/C ATTITUDE OUT OF GIMBAL
016815,000158: # 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,
016816,000159: # THE ADDITIONAL ROTATION TO AVOID GIMAL LOCK IS 35 DEGREES. IF THE AXIS IS MORE THAN 60.5 DEGEES FROM +X (OR -X)
016817,000160: # THE ADDITIONAL ROTATION IS 35 DEGREES. THE GIMBAL ANGLES CORRESPONDING TO THIS ATTITUDE ARE THEN COMPUTED AND
016818,000161: # STORED AS 2S COMPLIMENT ANGLES IN T(MPAC) BEFORE RETURNING TO THE CALLER.
016819,000162:
016820,000163: # WHEN POINTING THE X-AXIS, OR THE THRUST VECTOR, OR ANY VECTOR WITHIN 40.6 DEG OF THE X-AXIS, VECPOINT
016821,000164: # CANNOT CORRECT FOR A CROSS-PRODUCT ROTATION INTO GIMBAL LOCK. IN THIS CASE A PLATFORM REALIGNMENT WOULD BE
016822,000165: # REQUIRED TO POINT THE VECTOR IN THE DESIRED DIRECTION. AT PRESENT NO INDICATION IS GIVEN FOR THIS SITUATION
016823,000166: # EXCEPT THAT THE FINAL MIDDLE GIMBAL ANGLE IN MPAC +2 IS GREATER THAN 59 DEGREES.
016824,000167:
016825,000168: # CALLING SEQUENCE -
016826,000169:
016827,000170: # 1) LOAD SCAXIS, POINTVSM
016828,000171: # 2) CALL
016829,000172: # VECPOINT
016830,000173:
016831,000174: # RETURNS WITH
016832,000175:
016833,000176: # 1) DESIRED OUTER GIMBAL ANGLE IN MPAC
016834,000177: # 2) DESIRED INNER GIMBAL ANGLE IN MPAC +1
016835,000178: # 3) DESIRED MIDDLE GIMBAL ANGLE IN MPAC +2
016836,000179:
016837,000180: # ERASABLES USED -
016838,000181:
016839,000182: # 1) SCAXIS 6
016840,000183: # 2) POINTVSM 6
016841,000184: # 3) MIS 18
016842,000185: # 4) DEL 18
016843,000186: # 5) COF 6
016844,000187: # 6) VECQTEMP 1
016845,000188: # 7) ALL OF VAC AREA 43
016846,000189:
016847,000190: # TOTAL 99
016848,000191:
016849,000192: 27,2000 SETLOC VECPT
016850,000193: 27,2000 BANK
|
|
Page 394
|
016852,000195: 27,2126 E6,1661 EBANK= BCDU
016853,000196:
016854,000197: 27,2126 COUNT 27/VECPT
016855,000198:
016856,000199: 27,2126 40020 VECPOINT STQ BOV # SAVE RETURN ADDRESS
016857,000200: 27,2127 03310 VECQTEMP
016858,000201: 27,2130 56131 VECLEAR # AND CLEAR OVFIND
016859,000202: 27,2131 47164 VECLEAR AXC,2 RTB
016860,000203: 27,2132 03320 MIS # READ THE PRESENT CDU ANGLES AND
016861,000204: 27,2133 44376 READCDUK # STORE THEM IN PD25, 26, 27
016862,000205: 27,2134 34032 STCALL 25D
016863,000206: 27,2135 44405 CDUTODCM # S/C AXES TO STABLE MEMBER AXES (MIS)
016864,000207: 27,2136 61375 VLOAD VXM
016865,000208: 27,2137 03357 POINTVSM # RESOLVE THE POINTING DIRECTION VF INTO
016866,000209: 27,2140 03321 MIS # INITIAL S/C AXES (VF = POINTVSM)
016867,000210: 27,2141 77656 UNIT
016868,000211: 27,2142 00035 STORE 28D
016869,000212: # PD 28 29 30 31 32 33
016870,000213: 27,2143 53435 VXV UNIT # TAKE THE CROSS PRODUCT VF X VI
016871,000214: 27,2144 03351 SCAXIS # WHERE VI = SCAXIS
016872,000215: 27,2145 57400 BOV VCOMP
016873,000216: 27,2146 56256 PICKAXIS
016874,000217: 27,2147 17343 STODL COF # CHECK MAGNITUDE
016875,000218: 27,2150 00045 36D # OF CROSS PRODUCT
016876,000219: 27,2151 50025 DSU BMN # VECTOR, IF LESS
016877,000220: 27,2152 16327 DPB-14 # THAN B-14 ASSUME
016878,000221: 27,2153 56256 PICKAXIS # UNIT OPERATION
016879,000222: 27,2154 50375 VLOAD DOT # INVALID.
016880,000223: 27,2155 03351 SCAXIS
016881,000224: 27,2156 00035 28D
016882,000225: 27,2157 65552 SL1 ARCCOS
016883,000226: 27,2160 77624 COMPMATX CALL # NOW COMPUTE THE TRANSFORMATION FROM
016884,000227: 27,2161 44530 DELCOMP # FINAL S/C AXES TO INITIAL S/C AXES MFI
016885,000228: 27,2162 75160 AXC,1 AXC,2
016886,000229: 27,2163 03320 MIS # COMPUTE THE TRANSFORMATION FROM FINAL
016887,000230: 27,2164 03425 DEL # S/C AXES TO STABLE MEMBER AXES
016888,000231: 27,2165 77624 CALL # MFS = MIS MFI
016889,000232: 27,2166 44304 MXM3 # (IN PD LIST)
016890,000233:
016891,000234: 27,2167 51545 DLOAD ABS
016892,000235: 27,2170 00007 6 # MFS6 = SIN(CPSI) $2
016893,000236: 27,2171 50025 DSU BMN
016894,000237: 27,2172 16314 SINGIMLC # = SIN(59 DEGS) $2
016895,000238: 27,2173 56246 FINDGIMB # /CPSI/ LESS THAN 59 DEGS
016896,000239: # I.E. DESIRED ATTITUDE NOT IN GIMBAL LOCK
016897,000240:
016898,000241: 27,2174 51545 DLOAD ABS # CHECK TO SEE IF WE ARE POINTING
016899,000242: 27,2175 03351 SCAXIS # THE THRUST AXIS
016900,000243: 27,2176 51025 DSU BPL
016901,000244: 27,2177 16316 SINVEC1 # SIN 49.4 DEGS $2
|
|
Page 395
|
016903,000246: 27,2200 56246 FINDGIMB # IF SO, WE ARE TRYING TO POINT IT INTO
016904,000247: 27,2201 77775 VLOAD # GIMBAL LOCK, ABORT COULD GO HERE
016905,000248: 27,2202 77626 STADR
016906,000249: 27,2203 50442 STOVL MIS +12D
016907,000250: 27,2204 77626 STADR # STORE MFS (IN PD LIST) IN MIS
016908,000251: 27,2205 50450 STOVL MIS +6
016909,000252: 27,2206 77626 STADR
016910,000253: 27,2207 50456 STOVL MIS
016911,000254: 27,2210 03327 MIS +6 # INNER GIMBAL AXIS IN FINAL S/C AXES
016912,000255: 27,2211 57444 BPL VCOMP # LOCATE THE IG AXIS DIRECTION CLOSEST TO
016913,000256: 27,2212 56213 IGSAMEX # FINAL X S/C AXIS
016914,000257:
016915,000258: 27,2213 50035 IGSAMEX VXV BMN # FIND THE SHORTEST WAY OF ROTATING THE
016916,000259: 27,2214 03351 SCAXIS # S/C OUT OF GIMBAL LOCK BY A ROTATION
016917,000260: 27,2215 56222 U=SCAXIS # ABOUT +- SCAXIS, I.E. IF (IG (SGN MFS3)
016918,000261: # X SCAXIS . XF) LESS THAN 0, U = SCAXIS
016919,000262: # OTHERWISE U = -SCAXIS
016920,000263:
016921,000264: 27,2216 57575 VLOAD VCOMP
016922,000265: 27,2217 03351 SCAXIS
016923,000266: 27,2220 37343 STCALL COF # ROTATE ABOUT -SCAXIS
016924,000267: 27,2221 56225 CHEKAXIS
016925,000268: 27,2222 77775 U=SCAXIS VLOAD
016926,000269: 27,2223 03351 SCAXIS
016927,000270: 27,2224 03343 STORE COF # ROTATE ABOUT + SCAXIS
016928,000271: 27,2225 51545 CHEKAXIS DLOAD ABS
016929,000272: 27,2226 03351 SCAXIS # SEE IF WE ARE POINTING THE AOT
016930,000273: 27,2227 51025 DSU BPL
016931,000274: 27,2230 16320 SINVEC2 # SIN 29.5 DEGS $2
016932,000275: 27,2231 56235 PICKANG1 # IF SO, ROTATE 50 DEGS ABOUT +- SCAXIS
016933,000276: 27,2232 52145 DLOAD GOTO # IF NOT, MUST BE POINTING THE TRANSPONDER
016934,000277: 27,2233 16324 VECANG2 # OR SOME VECTOR IN THE Y, OR Z PLANE
016935,000278: 27,2234 56237 COMPMFSN # IN THIS CASE ROTATE 35 DEGS TO GET OUT
016936,000279: # OF GIMBAL LOCK (VECANG2 $360)
016937,000280: 27,2235 77745 PICKANG1 DLOAD
016938,000281: 27,2236 16322 VECANG1 # = 50 DEGS $ 360
016939,000282: 27,2237 77624 COMPMFSN CALL
016940,000283: 27,2240 44530 DELCOMP # COMPUTE THE ROTATION ABOUT SCAXIS TO
016941,000284: 27,2241 75160 AXC,1 AXC,2 # BRING MFS OUT OF GIMBAL LOCK
016942,000285: 27,2242 03320 MIS
016943,000286: 27,2243 03425 DEL
016944,000287: 27,2244 77624 CALL # COMPUTE THE NEW TRANSFORMATION FROM
016945,000288: 27,2245 44304 MXM3 # DESIRED S/C AXES TO STABLE MEMBER AXES
016946,000289: # WHICH WILL ALIGN VI WITH VF AND AVOID
016947,000290: # GIMBAL LOCK
016948,000291: 27,2246 45160 FINDGIMB AXC,1 CALL
016949,000292: 27,2247 00000 0 # EXTRACT THE COMMANDED CDU ANGLES FROM
016950,000293: 27,2250 44655 DCMTOCDU # THIS MATRIX
016951,000294: 27,2251 40234 RTB SETPD
016952,000295: 27,2252 45552 V1STO2S # CONVERT TO 2:S COMPLEMENT
|
|
Page 396
|
016954,000297: 27,2253 00001 0
016955,000298: 27,2254 77650 GOTO
016956,000299: 27,2255 03310 VECQTEMP # RETURN TO CALLER
016957,000300:
016958,000301: 27,2256 50375 PICKAXIS VLOAD DOT # IF VF X VI = 0, FIND VF . VI
016959,000302: 27,2257 00035 28D
016960,000303: 27,2260 03351 SCAXIS
016961,000304: 27,2261 72240 BMN TLOAD
016962,000305: 27,2262 56266 ROT180
016963,000306: 27,2263 00032 25D
016964,000307: 27,2264 77650 GOTO # IF VF = VI, CDU DESIRED = PRESENT CDU
016965,000308: 27,2265 03310 VECQTEMP # PRESENT CDU ANGLES
016966,000309:
016967,000310: 27,2266 47375 ROT180 VLOAD VXV # IF VF, VI ANTIPARALLEL, 180 DEG ROTATION
016968,000311: 27,2267 03327 MIS +6 # IS REQUIRED. Y STABLE MEMBER AXIS IN
016969,000312: 27,2270 15333 HIUNITX # INITIAL S/C AXIS.
016970,000313: 27,2271 47256 UNIT VXV # FIND Y(SM) X X(I)
016971,000314: 27,2272 03351 SCAXIS # FIND UNIT(VI X UNIT(Y(SM) X X(I)))
016972,000315: 27,2273 40056 UNIT BOV # I.E. PICK A VECTOR IN THE PLANE OF X(I),
016973,000316: 27,2274 56310 PICKX # Y(SM) PERPENDICULAR TO VI
016974,000317: 27,2275 17343 STODL COF
016975,000318: 27,2276 00045 36D # CHECK MAGNITUDE
016976,000319: 27,2277 50025 DSU BMN # OF THIS VECTOR.
016977,000320: 27,2300 16327 DPB-14 # IF LESS THAN B-14,
016978,000321: 27,2301 56310 PICKX # PICK X-AXIS.
016979,000322: 27,2302 77775 VLOAD
016980,000323: 27,2303 03343 COF
016981,000324: 27,2304 17343 XROT STODL COF
016982,000325: 27,2305 15333 HIDPHALF
016983,000326: 27,2306 77650 GOTO
016984,000327: 27,2307 56160 COMPMATX
016985,000328: 27,2310 52175 PICKX VLOAD GOTO # PICK THE XAXIS IN THIS CASE
016986,000329: 27,2311 15333 HIUNITX
016987,000330: 27,2312 56304 XROT
016988,000331: 35,2000 BANK 35
016989,000332: 27,2000 SETLOC MANUVER1
016990,000333: 27,2000 BANK
016991,000334:
016992,000335: 27,2313 15555 35172 SINGIMLC 2DEC .4285836003 # = SIN(59) $2
016993,000336:
016994,000337: 27,2315 14113 36326 SINVEC1 2DEC .3796356537 # = SIN(49.4) $2
016995,000338:
016996,000339: 27,2317 07701 35703 SINVEC2 2DEC .2462117800 # = SIN(29.5) $2
016997,000340:
016998,000341: 27,2321 04343 21616 VECANG1 2DEC .1388888889 # = 50 DEGREES $360
016999,000342:
017000,000343: 27,2323 03070 34344 VECANG2 2DEC .09722222222 # = 35 DEGREES $360
017001,000344:
017002,000345:
017003,000346: 27,2325 00000 1BITDP OCT 0 # KEEP THIS BEFORE DPB(-14) *********
017004,000347: 27,2326 00001 DPB-14 OCT 00001
|
|
Page 397
|
017006,000349: 27,2327 00000 OCT 00000
017007,000350: 34,2002 BANK 34
017008,000351: 27,2000 SETLOC MANUVER
017009,000352: 27,2000 BANK
017010,000353:
|
|
Page 398
|
017012,000355: # ROUTINE FOR INITIATING AUTOMATIC MANEUVER VIA KEYBOARD (V49)
017013,000356:
017014,000357: 27,2330 1155 EBANK= CPHI
017015,000358:
017016,000359: 27,2330 COUNT 27/R62
017017,000360:
017018,000361: 27,2330 35052 R62DISP CAF V06N22 # DISPLAY COMMAND ICDUS CPHI, CTHETA, CPHI
017019,000362: 27,2331 04662 TC BANKCALL
017020,000363: 27,2332 20720 CADR GOFLASH
017021,000364: 27,2333 15534 TCF ENDEXT
017022,000365: 27,2334 12336 TCF GOMOVE # PROCEED
017023,000366: 27,2335 12330 TCF R62DISP # ENTER
017024,000367:
017025,000368: # ASTRONAUT MAY LOAD NEW ICDUS AT THIS
017026,000369: # POINT
017027,000370: 27,2336 05546 GOMOVE TC UPFLAG # SET 3-AXIS FLAG
017028,000371: 27,2337 00124 ADRES 3AXISFLG # BIT 6 FLAG 5
017029,000372:
017030,000373: 27,2340 04662 TC BANKCALL
017031,000374: 27,2341 56000 CADR R60CSM
017032,000375: 27,2342 15534 TCF ENDEXT
017033,000376:
End of include-file R60,R62.agc. Parent file is MAIN.agc