Source Code
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These source-code files are part of a reconstructed copy of Luminary 163, the
first (unflown) release of the Apollo 14 Lunar Module (LM) Apollo Guidance
Computer (AGC) software.
The reconstruction began with reconstructed source code for Luminary 173. Changes
between revision 163 and 173 were backed out, as described by Luminary memos 157
and 158. The reconstruction was verified by matching memory-bank checksums
to those listed in drawing 2021152N. Note that page numbers in the reconstructed
code match those for the baseline log section mentioned in each file's changelog;
the page numbers for a real Luminary 163 listing would be different.
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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059832,000002: ## Copyright: Public domain.
059833,000003: ## Filename: DAPIDLER_PROGRAM.agc
059834,000004: ## Purpose: A section of Luminary revision 163.
059835,000005: ## It is part of the reconstructed source code for the first
059836,000006: ## (unflown) release of the flight software for the Lunar
059837,000007: ## Module's (LM) Apollo Guidance Computer (AGC) for Apollo 14.
059838,000008: ## The code has been recreated from a reconstructed copy of
059839,000009: ## Luminary 173, as well as Luminary memos 157 amd 158.
059840,000010: ## It has been adapted such that the resulting bugger words
059841,000011: ## exactly match those specified for Luminary 163 in NASA
059842,000012: ## drawing 2021152N, which gives relatively high confidence
059843,000013: ## that the reconstruction is correct.
059844,000014: ## Reference: pp. 1398-1408
059845,000015: ## Assembler: yaYUL
059846,000016: ## Contact: Ron Burkey <info@sandroid.org>.
059847,000017: ## Website: www.ibiblio.org/apollo/index.html
059848,000018: ## Mod history: 2019-08-21 MAS Created from Luminary 173.
059849,000019:
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Page 1398
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059851,000021: # THE DAPIDLER PROGRAM IS STARTED BY FRESH START AND RESTART. THE DAPIDLER PROGRAM IS DONE 10 TIMES
059852,000022: # PER SECOND UNTIL THE ASTRONAUT DESIRES THE DAP TO WAKE UP, AND THE IMU AND CDUS ARE READY FOR USE BY THE DAP.
059853,000023: # THE NECESSARY INITIALIZATION OF THE DAP IS DONE BY THE DAPIDLER PROGRAM.
059854,000024: 16,2000 BANK 16
059855,000025: 16,2000 SETLOC DAPS1
059856,000026: 16,2000 BANK
059857,000027:
059858,000028: 16,2000 E6,1536 EBANK= AOSQ
059859,000029:
059860,000030: 16,2000 COUNT* $$/DAPID
059861,000031:
059862,000032: 16,2000 00006 CHEKBITS EXTEND
059863,000033: 16,2001 00031 READ CHAN31 # IF BOTH BIT13 AND BIT14 ARE ONE, THEN
059864,000034: 16,2002 40000 COM # THE MODE SELECT SWITCH IS IN THE OFF
059865,000035: 16,2003 74355 MASK BIT13-14 # POSITION, AND SO THE DAP SHOULD BE OFF,
059866,000036: 16,2004 00006 EXTEND # WITH NO ATTITUDE ERROR DISPLAY.
059867,000037: 16,2005 12157 BZF MOREIDLE
059868,000038:
059869,000039: 16,2006 41300 CS IMODES33
059870,000040: 16,2007 74746 MASK BIT6
059871,000041: 16,2010 10000 CCS A
059872,000042: 16,2011 12206 TCF JUMPDSP
059873,000043: 16,2012 41262 CS RCSFLAGS # IMU NOT USABLE. SET UP INITIALIZATION
059874,000044: 16,2013 74751 MASK BIT3 # FLAG FOR ATT ERROR DISPLAY ROUTINE.
059875,000045: 16,2014 27262 ADS RCSFLAGS
059876,000046: 16,2015 12163 TCF SHUTDOWN
059877,000047:
059878,000048: 16,2016 34742 CHEKMORE CAF BIT10 # BIT 10 OF 30 IS PGNCS CONTROL OF S/C
059879,000049: 16,2017 00006 EXTEND
059880,000050: 16,2020 02030 RAND CHAN30 # BITS IN 30 ARE INVERTED
059881,000051: 16,2021 10000 CCS A
059882,000052: 16,2022 12157 TCF MOREIDLE
059883,000053:
059884,000054: 16,2023 00002 RETURN
059885,000055:
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Page 1399
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059887,000057: # DAPIDLER ENTRY.
059888,000058:
059889,000059: 16,2024 22016 DAPIDLER LXCH BANKRUPT # INTERRUPT LEAD INS (CONTINUED)
059890,000060: 16,2025 00006 EXTEND
059891,000061: 16,2026 22012 QXCH QRUPT
059892,000062:
059893,000063: 16,2027 31262 CA RCSFLAGS
059894,000064: 16,2030 74737 MASK BIT13
059895,000065: 16,2031 10000 CCS A # CHECK IF 1/ACCJOB HAS BEEN SET UP SINCE
059896,000066: 16,2032 12041 TCF CHECKUP # THE LAST FRESH START OR RESTART.
059897,000067: 16,2033 34737 CA BIT13
059898,000068: 16,2034 27262 ADS RCSFLAGS # BIT 13 IS 1.
059899,000069: 16,2035 37720 CAF PRIO27
059900,000070: 16,2036 05072 TC NOVAC # SET UP JOB TO DO A LITTLE INITIALIZATION
059901,000071: 16,2037 E6,1536 EBANK= AOSQ # AND EXECUTE 1/ACCS.
059902,000072: 16,2037 03630 42106 2CADR 1/ACCSET # (WILL BRANCH TO MOREIDLE ON ACCSOKAY)
059903,000073:
059904,000074:
059905,000075: 16,2041 02000 CHECKUP TC CHEKBITS # CHECK TO SEE IF LM DAP IS TO GO ON AND
059906,000076: # DO ERROR DISPLAY.
059907,000077:
059908,000078: 16,2042 30111 CAE DAPBOOLS # IF 1/ACCS HAS NOT BEEN COMPLETED, IDLE.
059909,000079: 16,2043 74751 MASK ACCSOKAY # NOTE: ONLY FRESH START AND RESTART
059910,000080: 16,2044 00006 EXTEND # KNOCK THIS BIT DOWN.
059911,000081: 16,2045 12157 BZF MOREIDLE
059912,000082:
059913,000083: 16,2046 04674 STARTDAP TC IBNKCALL # ZERO ATTITUDE ERROR AND DESIRED RATES.
059914,000084: 16,2047 40154 FCADR ZATTEROR
059915,000085: 16,2050 34755 CAF ZERO # ********** INITIALIZE: **********
059916,000086: 16,2051 55524 TS TJP
059917,000087: 16,2052 55525 TS TJU
059918,000088: 16,2053 55526 TS TJV
059919,000089: 16,2054 55421 TS OMEGAP # RATES IN BODY (PILOT) COORDINATES.
059920,000090: 16,2055 55422 TS OMEGAQ
059921,000091: 16,2056 55423 TS OMEGAR
059922,000092: 16,2057 55430 TS TRAPEDP
059923,000093: 16,2060 55431 TS TRAPEDQ
059924,000094: 16,2061 55432 TS TRAPEDR
059925,000095: 16,2062 55536 TS AOSQ # OFFSET ACCELERATION ESTIMATES.
059926,000096: 16,2063 55537 TS AOSQ +1
059927,000097: 16,2064 55540 TS AOSR
059928,000098: 16,2065 55541 TS AOSR +1
059929,000099: 16,2066 55424 TS ALPHAQ # COPIES OF OFFSET ESTIMATES FOR DOWNLIST.
059930,000100: 16,2067 55425 TS ALPHAR
059931,000101: 16,2070 55501 TS NEGUQ
059932,000102: 16,2071 55503 TS NEGUR
059933,000103: 16,2072 55544 TS AOSQTERM # QRAXIS RATE DERIVATION TERMS AND KALMAN
059934,000104: 16,2073 55545 TS AOSRTERM # FILTER INITIALIZATION TERMS.
059935,000105: 16,2074 55510 TS QACCDOT # DESCENT ACCELERATION DERIVATIVE EST.
059936,000106: 16,2075 55512 TS RACCDOT
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Page 1400
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059938,000108: 16,2076 55502 TS ALLOWGTS # AOSTASK FLAG FOR QRAXIS RCS CONTROL USE.
059939,000109: 16,2077 55630 TS COTROLER # DO TRYGTS ON FIRST PASS (WILL GO TO RCS)
059940,000110: 16,2100 55632 TS INGTS # RECOGNIZE FIRST GTS PASS AS SUCH.
059941,000111: 16,2101 55631 TS QGIMTIMR # STOP GIMBAL DRIVES. (PROBABLY WOULD BE
059942,000112: 16,2102 55633 TS RGIMTIMR # GOOD ENOUGH JUST TO INACTIVATE TIMERS)
059943,000113: 16,2103 55460 TS OLDPMIN # MINIMUM IMPULSE MODE ERASABLES
059944,000114: 16,2104 55461 TS OLDQRMIN
059945,000115: 16,2105 55766 TS PJETCTR # INITIALIZE DOCKED JET INHIBITION
059946,000116: 16,2106 55767 TS UJETCTR # COUNTERS
059947,000117: 16,2107 55770 TS VJETCTR
059948,000118: 16,2110 4747 CALLGMBL EQUALS BIT5 # RCSFLAGS INITIALIZATION.
059949,000119: 16,2110 42202 CS MANFLAG
059950,000120: 16,2111 71262 MASK RCSFLAGS # NEGUQ(R) HAVE BEEN GENERATED.
059951,000121: 16,2112 55262 TS RCSFLAGS
059952,000122:
059953,000123: # SET UP "OLD" MEASURED CDU ANGLES:
059954,000124:
059955,000125: 16,2113 00006 EXTEND
059956,000126: 16,2114 30033 DCA CDUX # OLDXFORP AND OLDYFORP
059957,000127: 16,2115 53441 DXCH OLDXFORP
059958,000128: 16,2116 30034 CA CDUZ
059959,000129: 16,2117 55442 TS OLDZFORQ
059960,000130: 16,2120 41262 CS RCSFLAGS
059961,000131: 16,2121 74740 MASK BIT12
059962,000132: 16,2122 27262 ADS RCSFLAGS # BIT 12 SET TO 1.
059963,000133: 16,2123 34751 CA FOUR
059964,000134: 16,2124 55534 TS SKIPU
059965,000135: 16,2125 55535 TS SKIPV
059966,000136: 16,2126 34733 CA POSMAX
059967,000137: 16,2127 54031 TS TIME6
059968,000138: 16,2130 55466 TS T6NEXT
059969,000139: 16,2131 55470 TS T6FURTHA
059970,000140: 16,2132 34755 CA ZERO
059971,000141: 16,2133 55467 TS T6NEXT +1
059972,000142: 16,2134 55471 TS T6FURTHA +1
059973,000143: 16,2135 55465 TS NXT6ADR
059974,000144: 16,2136 55472 TS NEXTP
059975,000145: 16,2137 55473 TS NEXTU
059976,000146: 16,2140 55474 TS NEXTV
059977,000147: 16,2141 44363 CS TEN
059978,000148: 16,2142 55756 TS DAPZRUPT # JASK NOT IN PROGRESS, INITIALIZE NEG.
059979,000149: 16,2143 34752 CA TWO
059980,000150: 16,2144 55433 TS NPTRAPS
059981,000151: 16,2145 55434 TS NQTRAPS
059982,000152: 16,2146 55435 TS NRTRAPS
059983,000153: 16,2147 00006 EXTEND
059984,000154: 16,2150 32205 DCA PAXADIDL
059985,000155: 16,2151 53264 DXCH T5ADR
059986,000156: 16,2152 37732 SETTIME5 CAF MS100
059987,000157: 16,2153 54030 TS TIME5
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Page 1401
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059989,000159: 16,2154 15301 TCF RESUME
059990,000160: 16,2155 E6,1536 EBANK= AOSQ
059991,000161: 16,2155 02024 34106 IDLERADR 2CADR DAPIDLER
059992,000162:
059993,000163: 16,2157 04674 MOREIDLE TC IBNKCALL # CALCULATE Q,R-AXES ATTITUDE ERRORS.
059994,000164: 16,2160 36655 CADR QERRCALC
059995,000165:
059996,000166: 16,2161 04674 TC IBNKCALL
059997,000167: 16,2162 35451 CADR CALCPERR # CALCULATE P AXIS ATTITUDE ERRORS.
059998,000168:
059999,000169: 16,2163 00006 SHUTDOWN EXTEND
060000,000170: 16,2164 32156 DCA IDLERADR
060001,000171: 16,2165 53264 DXCH T5ADR
060002,000172:
060003,000173: 16,2166 34755 CAF ZERO # KILL ANY POSSIBLE JET REQUESTS
060004,000174: 16,2167 55472 TS NEXTP
060005,000175: 16,2170 55473 TS NEXTU
060006,000176: 16,2171 55474 TS NEXTV
060007,000177: 16,2172 00006 EXTEND # COMMAND JETS OFF.
060008,000178: 16,2173 01005 WRITE CHAN5
060009,000179: 16,2174 00006 EXTEND
060010,000180: 16,2175 01006 WRITE CHAN6
060011,000181: 16,2176 42203 CS BGIM23 # TURN TRIM GIMBAL OFF
060012,000182: 16,2177 00006 EXTEND
060013,000183: 16,2200 03012 WAND CHAN12
060014,000184: 16,2201 12152 TCF SETTIME5 # RETURN IN 100 MSEC.
060015,000185:
060016,000186: 16,2202 03021 MANFLAG OCT 03021
060017,000187: 16,2203 07400 BGIM23 OCTAL 07400
060018,000188: 16,2204 E6,1421 EBANK= OMEGAP
060019,000189: 16,2204 02213 34106 PAXADIDL 2CADR PAXIS
060020,000190:
060021,000191: 16,2206 7732 MS100 = OCT37766
060022,000192: 16,2206 0061 COSMG = ITEMP1
060023,000193: 16,2206 00006 JUMPDSP EXTEND # TRANSFER TO BANK 20
060024,000194: 16,2207 32212 DCA DSPCADR # FOR ATTITUDE ERROR DISPLAYS
060025,000195: 16,2210 52006 DTCB
060026,000196:
060027,000197: 16,2211 E6,1760 EBANK= AK
060028,000198: 16,2211 02227 40106 DSPCADR 2CADR ALTDSPLY
060029,000199:
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Page 1402
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060031,000201: 20,2227 BANK 20
060032,000202: 20,2000 SETLOC DAPS3
060033,000203: 20,2000 BANK
060034,000204: 20,2227 COUNT* $$/NEEDL
060035,000205:
060036,000206: # PROGRAM: ALTDSPLY
060037,000207:
060038,000208: # MOD 0. 6 DEC 1967
060039,000209:
060040,000210: # AUTHOR: CRAIG WORK, DON KEENE, MIT IL
060041,000211:
060042,000212: # MOD 3 BY DON KEENE AUG 1, 1968 MOVED PROGRAM TO BANK 20
060043,000213:
060044,000214: # PROGRAM DESCRIPTION:
060045,000215:
060046,000216: # ALTDSPLY REVERSES THE DSPLYALT BIT OF RCSFLAGS EACH TIME IT IS CALLED, WHICH IS PRESUMABLY EVERY 100 MS.
060047,000217: # IF THE REVERSED BIT IS ONE, NEEDLER IS CALLED TO DISPLAY ATTITUDE ERRORS. IF THE BIT IS ZERO, THE ATTITUDE ERR-
060048,000218: # ORS ARE CALCULATED AS 1) ESTIMATED RATES (FOLLOWING) IF NEED2FLG = 1, OTHERWISE AS 2) DAP FOLLOWING ERRORS FOR
060049,000219: # NEEDLFLG = 0 AND 3) TOTAL ATTITUDE ERRORS FOR NEEDLFLG = 1.
060050,000220:
060051,000221: # WARNING: ALTDSPLY MAY ONLY BE CALLED WITH INTERRUPT INHIBITED.
060052,000222:
060053,000223: # WARNING: EBANK MUST BE SET TO 6 WHEN USING THIS ROUTINE.
060054,000224:
060055,000225: # INPUT: RCSFLAGS AND 1) IF NEEDLFLG=0, INPUT PERROR,QERROR,RERROR.
060056,000226: # 2) IF NEEDLFLG=1, INPUT CPHI,CTHETA,CPSI,CDUX,CDUY,CDUZ,M11,M21,M32,M22,M32. (GPMATRIX)
060057,000227:
060058,000228: # 3) IF NEED2FLG = 1, INPUT OMEGAP, OMEGAQ, AND OMEGAR.
060059,000229:
060060,000230: # OUTPUTS: RCSFLAGS WITH DSPLYALT REVERSED,AK,AK1,AK2,+ NEEDLER OUTPUTS.
060061,000231:
060062,000232: # ENTRY: TCF ALTDSPLY
060063,000233:
060064,000234: # EXIT: TCF CHEKMORE
060065,000235:
060066,000236: # ALARM OR ABORT EXITS: NONE
060067,000237:
060068,000238: # SUBPROGRAMS CALLED: NEEDLER, OVERSUB2
060069,000239:
060070,000240: # DEBRIS: A,L,AND NEEDLER DEBRIS.
060071,000241:
060072,000242: 20,2227 31262 ALTDSPLY CA RCSFLAGS # INVERT THE DISPLAY ALTERNATION BIT.
060073,000243: 20,2230 54001 TS L
060074,000244: 20,2231 34750 CA DSPLYALT
060075,000245: 20,2232 00006 EXTEND
060076,000246: 20,2233 06001 RXOR LCHAN
060077,000247: 20,2234 55262 TS RCSFLAGS
060078,000248:
060079,000249: 20,2235 74750 MASK DSPLYALT
060080,000250: 20,2236 10000 CCS A # IS ALTERNATION FLAG ZERO?
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Page 1403
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060082,000252: 20,2237 12336 TCF NEEDLER
060083,000253:
060084,000254: 20,2240 40074 CS FLAGWRD0 # CHECK FOR RATE DISPLAY TO ERROR NEEDLES
060085,000255: 20,2241 74735 MASK NEED2BIT # VIA EXTENDED VERB 60
060086,000256: 20,2242 00006 EXTEND
060087,000257: 20,2243 12257 BZF DISPRATE
060088,000258:
060089,000259: 20,2244 30074 CAE FLAGWRD0 # NEEDLFLG WILL INDICATE TOTAL OR DAP AT-
060090,000260: 20,2245 74750 MASK NEEDLBIT # TITUDE ERROR DISPLAY REQUEST.
060091,000261: 20,2246 10000 CCS A
060092,000262: 20,2247 12266 TCF DSPLYTOT # TOTAL ERROR IS NEEDED IN AK,AK +1,AK +2
060093,000263:
060094,000264: 20,2250 41450 CS QERROR # YES. DISPLAY ATT ERRORS ON THE ,-BALL.
060095,000265: 20,2251 55761 TS AK +1 # ERROR COMPLEMENTS ARE INPUT TO NEEDLER.
060096,000266: 20,2252 41452 CS RERROR
060097,000267: 20,2253 55762 TS AK +2
060098,000268: 20,2254 41464 CS PERROR
060099,000269: 20,2255 57760 XCH AK
060100,000270:
060101,000271: 20,2256 12456 TCF RETNMORE # DISPLAY THESE THE NEXT TIME THROUGH
060102,000272:
060103,000273: 20,2257 41422 DISPRATE CS OMEGAQ # LOAD ESTIMATED RATES (FOLLOWING)
060104,000274: 20,2260 55761 TS AK +1
060105,000275: 20,2261 41423 CS OMEGAR
060106,000276: 20,2262 55762 TS AK +2
060107,000277: 20,2263 41421 CS OMEGAP
060108,000278: 20,2264 57760 XCH AK
060109,000279: 20,2265 12456 TCF RETNMORE
060110,000280:
060111,000281: # CALCULATE GIMBAL ANGLE TOTAL ERRORS, RESOLVE INTO PILOT AXES, STORE TOTAL ERRORS FOR NEEDLER. Q-AXIS FIRST.
060112,000282:
060113,000283: 20,2266 00006 DSPLYTOT EXTEND
060114,000284: 20,2267 22061 QXCH ITEMP1 # SAVE Q FOR CHEKBITS RETURN.
060115,000285:
060116,000286: 20,2270 30322 CA CTHETA # DESIRED ATTITUDE, Y-AXIS, 2'S COMP.
060117,000287: 20,2271 00006 EXTEND # SUBTRACT CURRENT ATTITUDE.
060118,000288: 20,2272 20033 MSU CDUY # DIFFERENCE SCALED AT PI, 1'S COMP.
060119,000289: 20,2273 55760 TS AK # SAVE FOR R-ERROR CALCULATION.
060120,000290: 20,2274 00006 EXTEND
060121,000291: 20,2275 71415 MP M21 # (CHTETA-CDUY)*M21 SCALED AT PI RADIANS.
060122,000292: 20,2276 57761 XCH AK +1 # STORE FIRST TERM OF Q ERROR.
060123,000293: 20,2277 30323 CA CPSI # DESIRED ATTITUDE, Z-AXIS, 2'S COMP.
060124,000294: 20,2300 00006 EXTEND # SUBTRACT CURRENT ATTITUDE.
060125,000295: 20,2301 20034 MSU CDUZ # DIFFERENCE SCALED AT PI, 1'S COMP.
060126,000296: 20,2302 55762 TS AK +2 # SAVE Z-AXIS TERM FOR R ERROR CALCULATION
060127,000297: 20,2303 00006 EXTEND
060128,000298: 20,2304 71417 MP M22 # (CPSI-CDUZ)*M22, SCALED AT PI RADIANS.
060129,000299: 20,2305 61761 AD AK +1 # Q ERROR COMPLETE , AT PI RAD.
060130,000300: 20,2306 02451 TC OVERSUB2 # PIN NEEDLES IN CASE OF OVERFLOW.
060131,000301: 20,2307 55761 TS AK +1
060132,000302:
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Page 1404
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060134,000304: # R ERROR CALCULATION NEXT.
060135,000305:
060136,000306: 20,2310 31760 CA AK # Y-AXIS DIFFERENCE STORED BY Q-AXIS CALC.
060137,000307: 20,2311 00006 EXTEND
060138,000308: 20,2312 71416 MP M31 # (CTHETA-CDUY)*M31, SCALED AT PI RADIANS.
060139,000309: 20,2313 57762 XCH AK +2 # FIRST TERM OF R ERROR.
060140,000310: # Z-AXIS DIFFERENCE, STORED BY A CALC. IS
060141,000311: 20,2314 00006 EXTEND # RECOVERED BY THE EXCHANGE.
060142,000312: 20,2315 71420 MP M32 # (CPSI-CDUZ)*M32, SCALED AT PI RADIANS.
060143,000313: 20,2316 61762 AD AK +2 # R ERROR COMPLETE , AT PI RAD.
060144,000314: 20,2317 02451 TC OVERSUB2 # PIN NEEDLES IN CASE OF OVERFLOW.
060145,000315: 20,2320 55762 TS AK +2
060146,000316:
060147,000317: # NOW CALCULATE P ERROR. (NOTE THAT M13 = 1, SCALED AT 1, SO THE MULTIPLICATION IS BY-PASSED.)
060148,000318:
060149,000319: 20,2321 31760 CA AK # Y-AXIS DIFFERENCE STORED BY Q AXIS CALC.
060150,000320: 20,2322 00006 EXTEND
060151,000321: 20,2323 71414 MP M11 # (CTHETA-CDUY)*M11 SCALED AT PI RADIANS.
060152,000322: 20,2324 57760 XCH AK # FIRST TERM OF P ERROR IN AK, AT PI RAD.
060153,000323: 20,2325 30321 CAE CPHI # DESIRED ATTITUDE, X-AXIS, 2'S COMP.
060154,000324: 20,2326 00006 EXTEND # SUBTRACT CURRENT X ATTITUDE.
060155,000325: 20,2327 20032 MSU CDUX # X-AXIS DIFFERENCE, 1'S COMP, AT PI RAD.
060156,000326:
060157,000327: # M13 = 1, SO BYPASS THE MULTIPLICATION.
060158,000328: # EXTEND
060159,000329: # MP M13 (CPHI-CDUX)*M13 SCALED AT PI RADIANS.
060160,000330:
060161,000331: 20,2330 61760 AD AK # P ERROR COMPLETE , SCALED AT PI RAD
060162,000332: 20,2331 02451 TC OVERSUB2 # PIN NEEDLES IN CASE OF OVERFLOW.
060163,000333: 20,2332 55760 TS AK
060164,000334:
060165,000335: 20,2333 00006 EXTEND
060166,000336: 20,2334 22061 QXCH ITEMP1 # RESTORE Q FOR CHEKBITS RETURN.
060167,000337:
060168,000338: 20,2335 12456 TCF RETNMORE # DISPLAY THESE THE NEXT TIME THROUGH
060169,000339:
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Page 1405
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060171,000341: # FDAI ATTITUDE ERROR DISPLAY SUBROUTINE
060172,000342:
060173,000343: # PROGRAM DESCRIPTION: D. KEENE 5/24/67
060174,000344:
060175,000345: # MOD 1 BY CRAIG WORK, 12 DEC 67
060176,000346:
060177,000347: # MOD 2 BY CRAIG WORK, 6 APRIL 68 CONVERTS ATTITUDE ERROR DISPLAY SCALING FROM 16 7/8 DEG. TO 42 3/16 DEGREES.
060178,000348:
060179,000349: # THIS SUBROUTINE IS USED TO DISPLAY ATTITUDE ERRORS ON THE FDAI VIA THE DIGITAL TO ANALOG CONVERTERS (DACS)
060180,000350: # IN THE CDUS. CARE IS TAKEN TO METER OUT THE APPROPRIATE NUMBER OF PULSES TO THE IMU ERROR COUNTERS AND PREVENT
060181,000351: # OVERFLOW, TO CONTROL THE RELAY SEQUENCING, AND TO AVOID INTERFERENCE WITH THE COARSE ALIGN LOOP WHICH ALSO USES
060182,000352: # THE DACS.
060183,000353:
060184,000354:
060185,000355: # CALLING SEQUENCE:
060186,000356:
060187,000357: # DURING THE INITIALIZATION SECTION OF THE USER'S PROGRAM, BIT3 OF RCSFLAGS SHOULD BE SET TO INITIATE THE
060188,000358: # TURN-ON SEQUENCE WITHIN THE NEEDLES PROGRAM:
060189,000359:
060190,000360: # CS RCSFLAGS IN EBANK6
060191,000361: # MASK BIT3
060192,000362: # ADS RCSFLAGS
060193,000363:
060194,000364: # THEREAFTER, THE ATTITUDE ERRORS GENERATED BY THE USER SHOULD BE TRANSFERED TO THE FOLLOWING LOCATIONS IN EBANK6:
060195,000365:
060196,000366: # AK SCALED 180 DEGREES NOTE: THESE LOCATIONS ARE SUBJECT
060197,000367: # AK1 SCALED 180 DEGREES TO CHANGE
060198,000368: # AK2 SCALED 180 DEGREES
060199,000369:
060200,000370: # FULL SCALED DEFLECTION OF THE NEEDLES CORRESPONDS TO 5 1/16 DEGREES, WHILE 384 BITS IN THE IMU ERROR COUNTER
060201,000371: # CORRESPONDS TO 42 3/16 DEGREES. (DAC MAXIMUM CAPACITY IS 384 BITS.) 46 BITS EFFECTIVELY PIN THE NEEDLES.
060202,000372:
060203,000373: # FOR RATE DISPLAY, FULL SCALE NEEDLE DEFLECTION IS 1 17/64 DEG/SEC, AND A FULL COUNTER IS ABOUT 10.5 DEG/SEC.
060204,000374: # A CALL TO NEEDLER WILL THEN UPDATE THE DISPLAY:
060205,000375:
060206,000376: # INHINT
060207,000377: # TC IBNKCALL NOTE: EBANK SHOULD BE SET TO E6
060208,000378: # CADR NEEDLER
060209,000379: # RELINT
060210,000380:
060211,000381: # THIS PROCESS SHOULD BE REPEATED EACH TIME THE ERRORS ARE UPDATED. AT LEAST 3 PASSES THRU THE PROGRAM ARE
060212,000382: # REQUIRED BEFORE ANYTHING IS ACTUALLY DISPLAYED ON THE ERROR METERS.
060213,000383: # NOTE: EACH CALL TO NEEDLER MUST BE SEPARATED BY AT LEAST 50MS TO ASSURE PROPER RELAY SEQUENCING.
060214,000384:
060215,000385: # ERASABLE USED:
060216,000386: # AK CDUXCMD
060217,000387: # AK1 CDUYCMD
060218,000388: # AK2 CDUZCMD
060219,000389: # EDRIVEX A,L,Q
060220,000390: # EDRIVEY T5TEMP
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Page 1406
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060222,000392: # EDRIVEZ DINDX
060223,000393:
060224,000394: # SWITCHES: RCSFLAGS BITS 3,2
060225,000395:
060226,000396: # I/O CHANNELS: CHAN12 BIT 4 (COARSE ALIGN - READ ONLY)
060227,000397: # CHAN12 BIT 6 (IMU ERROR COUNTER ENABLE)
060228,000398: # CHAN14 BIT 13,14,15 (DAC ACTIVITY)
060229,000399:
060230,000400:
060231,000401: # SIGN CONVENTION< AK = THETAC - THETA
060232,000402: # WHERE THETAC = COMMAND ANGLE
060233,000403: # THETA = PRESENT ANGLE
060234,000404:
060235,000405:
060236,000406: 20,2336 31262 NEEDLER CA RCSFLAGS
060237,000407: 20,2337 76245 MASK SIX
060238,000408: 20,2340 00006 EXTEND
060239,000409: 20,2341 12376 BZF NEEDLES3
060240,000410: 20,2342 74751 MASK BIT3
060241,000411: 20,2343 00006 EXTEND
060242,000412: 20,2344 12367 BZF NEEDLER2 # BIT3 = 0, BIT2 = 1
060243,000413:
060244,000414: 20,2345 44746 CS BIT6 # FIRST PASS BIT3 = 1
060245,000415: 20,2346 00006 EXTEND # DISABLE IMU ERROR COUNTER TO ZERO DACS
060246,000416: 20,2347 03012 WAND CHAN12 # MUST WAIT AT LEAST 60 MS BEFORE
060247,000417: 20,2350 44755 NEEDLE11 CS ZERO # ENABLING COUNTERS.
060248,000418: 20,2351 55760 TS AK # ZERO THE INPUTS ON FIRST PASS
060249,000419: 20,2352 55761 TS AK1
060250,000420: 20,2353 55762 TS AK2
060251,000421: 20,2354 55763 TS EDRIVEX # ZERO THE DISPLAY REGISTERS
060252,000422: 20,2355 55764 TS EDRIVEY
060253,000423: 20,2356 55765 TS EDRIVEZ
060254,000424: 20,2357 54050 TS CDUXCMD # ZERO THE OUT COUNTERS
060255,000425: 20,2360 54051 TS CDUYCMD
060256,000426: 20,2361 54052 TS CDUZCMD
060257,000427: 20,2362 46245 CS SIX # RESET RCSFLAGS FOR PASS2
060258,000428: 20,2363 71262 MASK RCSFLAGS
060259,000429: 20,2364 64752 AD BIT2
060260,000430: 20,2365 55262 TS RCSFLAGS
060261,000431: 20,2366 12456 TCF RETNMORE
060262,000432:
060263,000433: 20,2367 34746 NEEDLER2 CAF BIT6 # ENABLE IMU ERROR COUNTERS
060264,000434: 20,2370 00006 EXTEND
060265,000435: 20,2371 05012 WOR CHAN12
060266,000436: 20,2372 46245 CS SIX # RESET RCSFLAGS TO DISPLAY ATTITUDE
060267,000437: 20,2373 71262 MASK RCSFLAGS # ERRORS WAIT ATLEAST 4 MS FOR
060268,000438: 20,2374 55262 TS RCSFLAGS # RELAY CLOSURE
060269,000439: 20,2375 12456 TCF RETNMORE
060270,000440:
060271,000441: 20,2376 34746 NEEDLES3 CAF BIT6 # CHECK TO SEE IF IMU ERROR COUNTER
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Page 1407
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060273,000443: 20,2377 00006 EXTEND # IS ENABLED
060274,000444: 20,2400 02012 RAND CHAN12
060275,000445: 20,2401 10000 CCS A # IF NOT, RE-INITIALIZE NEEDLER.
060276,000446: 20,2402 12407 TCF NEEDLES
060277,000447:
060278,000448: 20,2403 41262 CS RCSFLAGS # SET UP INITIALIZATION FLAG IN RCSFLAGS.
060279,000449: 20,2404 74751 MASK BIT3
060280,000450: 20,2405 27262 ADS RCSFLAGS
060281,000451: 20,2406 12456 TCF RETNMORE
060282,000452:
060283,000453: 20,2407 34752 NEEDLES CAF TWO
060284,000454: 20,2410 54063 DACLOOP TS DINDX
060285,000455: 20,2411 42450 CS ONETENTH # RESCALE INPUTS TO + OR - 1800 DEGREES.
060286,000456: 20,2412 00006 EXTEND
060287,000457: 20,2413 50063 INDEX DINDX
060288,000458: 20,2414 71760 MP AK
060289,000459: 20,2415 54001 TS L
060290,000460: 20,2416 10000 CCS A
060291,000461: 20,2417 32446 CA DACLIMIT
060292,000462: 20,2420 12422 TCF +2
060293,000463: 20,2421 42446 CS DACLIMIT
060294,000464: 20,2422 60001 AD L
060295,000465: 20,2423 54061 TS T5TEMP # OVFLO CHK
060296,000466: 20,2424 12430 TCF +4
060297,000467: 20,2425 50000 INDEX A # ON OVERFLOW LIMIT OUTPUT TO +-384
060298,000468: 20,2426 32446 CAF DACLIMIT
060299,000469: 20,2427 54001 TS L
060300,000470: 20,2430 50063 INDEX DINDX
060301,000471: 20,2431 41763 CS EDRIVEX # CURRENT VALUE OF DAC
060302,000472: 20,2432 60001 AD L
060303,000473: 20,2433 50063 INDEX DINDX
060304,000474: 20,2434 26050 ADS CDUXCMD
060305,000475: 20,2435 50063 INDEX DINDX
060306,000476: 20,2436 23763 LXCH EDRIVEX
060307,000477: 20,2437 10063 CCS DINDX
060308,000478: 20,2440 12410 TCF DACLOOP
060309,000479: 20,2441 37743 CAF 13,14,15
060310,000480: 20,2442 00006 EXTEND
060311,000481: 20,2443 05014 WOR CHAN14 # SET DAC ACTIVITY BITS
060312,000482: 20,2444 12456 TCF RETNMORE
060313,000483:
060314,000484: 20,2445 77177 DEC -384 B-14
060315,000485: 20,2446 37200 DACLIMIT DEC 16000 B-14
060316,000486: 20,2447 00600 DEC 384 B-14
060317,000487:
060318,000488: 20,2450 03146 ONETENTH OCT 03146 # DECIMAL +0.1, SCALED AT 1.
060319,000489: 20,2451 4750 DSPLYALT EQUALS BIT4 # 100 MS ALTERNATION BIT IN RCSFLAGS
060320,000490:
060321,000491:
060322,000492: 20,2451 54007 OVERSUB2 TS 7 # RETURNS A UNCHANGED OR LIMITED TO
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Page 1408
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060324,000494: 20,2452 00002 TC Q # POSMAX OR NEGMAX IF A HAS OVERFLOW
060325,000495: 20,2453 50000 INDEX A
060326,000496: 20,2454 44734 CS LIMITS # DUPLICATE CODING IN BANK 16
060327,000497: 20,2455 00002 TC Q
060328,000498:
060329,000499:
060330,000500: 20,2456 00006 RETNMORE EXTEND # RETURN TO CHEKMORE
060331,000501: 20,2457 32462 DCA MORECADR
060332,000502: 20,2460 52006 DTCB
060333,000503:
060334,000504: 20,2461 E6,1536 EBANK= AOSQ
060335,000505: 20,2461 02016 34106 MORECADR 2CADR CHEKMORE
060336,000506:
End of include-file DAPIDLER_PROGRAM.agc. Parent file is MAIN.agc