Source Code
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This is a reconstructed version of Luminary 130, the initial AGC program released
in November 1969 for the Apollo 13 LM. Three more releases
followed before the flown revision was finally manufactured in February 1970.
This reconstruction was created from a previous transcription of the original listing of
Luminary 131, combined with Luminary memo #129 which describes the small difference
between the Luminary 130 and 131. The reconstructed source code was verified by
matching memory-bank checksums to those listed for Luminary 130 in drawing 2021152G.
In this source code, program comments from the original (Luminary 131) code are
prefixed with '#', while those added later by the Virtual AGC project are prefixed
with '##'.
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030321,000002: ## Copyright: Public domain.
030322,000003: ## Filename: R30.agc
030323,000004: ## Purpose: A section of the reconstructed source code for Luminary 130.
030324,000005: ## This was the original program released for the Apollo 13 LM,
030325,000006: ## although several more revisions would follow. It has been
030326,000007: ## reconstructed from a listing of Luminary 131, from which it
030327,000008: ## differs on only two lines in P70-P71. The difference is
030328,000009: ## described in detail in Luminary memo #129, which was used
030329,000010: ## to perform the reconstruction. This file is intended to be a
030330,000011: ## faithful reconstruction, except that the code format has been
030331,000012: ## changed to conform to the requirements of the yaYUL assembler
030332,000013: ## rather than the original YUL assembler.
030333,000014: ## Reference: pp. 714-724
030334,000015: ## Contact: Ron Burkey <info@sandroid.org>.
030335,000016: ## Website: www.ibiblio.org/apollo/index.html
030336,000017: ## Mod history: 05/24/03 RSB. Began transcribing.
030337,000018: ## 05/14/05 RSB Corrected website reference above.
030338,000019: ## 2017-01-06 RSB Page numbers now agree with those on the
030339,000020: ## original harcopy, as opposed to the PDF page
030340,000021: ## numbers in 1701.pdf.
030341,000022: ## 2017-02-08 RSB Comment-text fixes discovered while proofing Artemis 72.
030342,000023: ## 2017-02-24 RSB Proofed comment text using octopus/ProoferComments.
030343,000024: ## 2017-02-28 RSB Fixed lingering typos.
030344,000025: ## 2017-03-09 RSB Comment-text fixes noted in proofing Luminary 116.
030345,000026: ## 2017-03-16 RSB Comment-text fixes identified in 5-way
030346,000027: ## side-by-side diff of Luminary 69/99/116/131/210.
030347,000028: ## 2017-03-17 RSB Comment-text fixes identified in diff'ing
030348,000029: ## Luminary 99 vs Comanche 55.
030349,000030: ## 2018-09-04 MAS Copied from Luminary 131 for Luminary 130.
030350,000031:
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Page 714
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030352,000033: # SUBROUTINE NAME: V82CALL
030353,000034: # MOD NO: 0 DATE: 16 FEB 67
030354,000035: # MOD BY: RR BAIRNSFATHER LOG SECTION: R30
030355,000036: # MOD NO: 1 MOD BY: RR BAIRNSFATHER DATE: 11 APR 67 SR30.1 CHANGED TO ALLOW MONITOR OPERN
030356,000037: # MOD NO: 2 MOD BY ALONSO DATE: 11 DEC 67 VB82 PROGRAM REWRITTEN
030357,000038: # MOD NO: 3 MOD BY ALONSO DATE: 26 MAR 68 PROG MOD TO HANDLE DIF EARTH/MOON SCALE
030358,000039:
030359,000040: # NEW FUNCTIONAL DESCRIPTION: CALLED BY VERB 82 ENTER. PRIORITY 10
030360,000041: # USED THROUGHOUT. CALCULATE AND DISPLAY ORBITAL PARAMETERS
030361,000042:
030362,000043: # 1. IF AVERAGE G IS OFF:
030363,000044: # FLASH DISPLAY V04N06. R2 INDICATES WHICH SHIP'S STATE VECTOR IS
030364,000045: # TO BE UPDATED. INITIAL CHOICE IS THIS SHIP (R2=1). ASTRONAUT
030365,000046: # CAN CHANGE TO OTHER SHIP BY V22EXE, WHERE X NOT EQ 1.
030366,000047: # SELECTED STATE VECTOR UPDATED BY THISPREC (OTHPREC).
030367,000048: # CALLS SR30.1 (WHICH CALLS TFFCONMU + TFFRP/RA) TO CALCULATE
030368,000049: # RPER (PERIGEE RADIUS), RAPO (APOGEE RADIUS), HPER (PERIGEE
030369,000050: # HEIGHT ABOVE LAUNCH PAD OR LUNAR LANDING SITE), HAPO (APOGEE
030370,000051: # HEIGHT AS ABOVE), TPER (TIME TO PERIGEE), TFF (TIME TO
030371,000052: # INTERSECT 300 KFT ABOVE PAD OR 35KFT ABOVE LANDING SITE).
030372,000053: # FLASH MONITOR V16N44 (HAPO, HPER, TFF). TFF IS -59M59S IF IT WAS
030373,000054: # NOT COMPUTABLE, OTHERWISE IT INCREMENTS ONCE PER SECOND.
030374,000055: # ASTRONAUT HAS OPTION TO MONITOR TPER BY KEYING IN N 32 E.
030375,000056: # DISPLAY IS IN HMS, IS NEGATIVE (AS WAS TFF), AND INCREMENTS
030376,000057: # ONCE PER SECOND ONLY IF TFF DISPLAY WAS -59M59S.
030377,000058: # 2. IF AVERAGE G IS ON:
030378,000059: # CALLS SR30.1 APPROX EVERY TWO SECS. STATE VECTOR IS ALWAYS
030379,000060: # FOR THIS VEHICLE. V82 DOES NOT DISTURB STATE VECTOR. RESULTS
030380,000061: # OF SR30.1 ARE RAPO, RPER, HAPO, HPER, TPER, TFF.
030381,000062: # FLASH MONITOR V16N44 (HAPO, HPER, TFF).
030382,000063: # ADDENDUM: HAPO AND HPER SHOULD BE CHANGED TO READ HAPOX AND HPERX IN THE
030383,000064: # ABOVE REMARKS.
030384,000065:
030385,000066: # CALLING SEQUENCE: VERB 82 ENTER.
030386,000067:
030387,000068: # SUBROUTINES CALLED: SR30.1, GOXDSPF
030388,000069: # MAYBE - THISPREC, OTHPREC, LOADTIME, DELRSPL
030389,000070:
030390,000071: # NORMAL EXIT MODES: TC ENDEXT
030391,000072:
030392,000073: # ALARMS: NONE
030393,000074:
030394,000075: # OUTPUT: HAPOX (-29) M
030395,000076: # HPERX (-29) M
030396,000077: # RAPO (-29) M EARTH
030397,000078: # (-27) M MOON
030398,000079: # RPER (-29) M EARTH
030399,000080: # (-27) M MOON
030400,000081: # TFF (-28) CS CONTAINS NEGATIVE QUANTITY
030401,000082: # -TPER (-28) CS CONTAINS NEGATIVE QUANTITY
030402,000083:
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Page 715
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030404,000085: # ERASABLE INITIALIZATION REQUIRED: STATE VECTOR.
030405,000086:
030406,000087: # DEBRIS: QPRET, RONE, VONE, TFF/RTMU, HPERMIN, RPADTEM, V82EMFLG.
030407,000088: # MAYBE: TSTART82, V82FLAGS, TDEC1.
030408,000089:
030409,000090: 13,2347 E4,1517 EBANK= HAPOX
030410,000091: 31,2144 BANK 31
030411,000092: 22,2000 SETLOC R30LOC
030412,000093: 22,2000 BANK
030413,000094: 22,3242 COUNT* $$/R30
030414,000095:
030415,000096: 22,3242 06042 V82CALL TC INTPRET
030416,000097: 22,3243 52014 BON GOTO
030417,000098: 22,3244 03712 AVEGFLAG
030418,000099: 22,3245 45465 V82GON # IF AVERAGE G ON
030419,000100: 22,3246 45247 V82GOFF # IF AVERAGE G OFF
030420,000101:
030421,000102: 22,3247 77776 V82GOFF EXIT # ALLOW ASTRONAUT TO SELECT VEHICLE
030422,000103: 22,3250 34752 CAF TWO # DESIRED FOR ORBITAL PARAMETERS
030423,000104: 22,3251 55050 TS OPTIONX # CALCULATION AND DISPLAY.
030424,000105: 22,3252 34753 CAF ONE
030425,000106: 22,3253 55051 TS OPTIONX +1
030426,000107: 22,3254 33316 CAF OPTIONVN # V 04 N 06
030427,000108: 22,3255 04616 TC BANKCALL
030428,000109: 22,3256 20334 CADR GOXDSPF
030429,000110: 22,3257 05472 TC ENDEXT # TERMINATE
030430,000111: 22,3260 03262 TC +2 # PROCEED
030431,000112: 22,3261 03254 TC -5 # DATA IN. OPTION1+1 = 1 FOR THIS VEHICLE.
030432,000113: # UNEQ 1 FOR OTHER VEHICLE.
030433,000114: 22,3262 34750 CAF BIT4 # 80 MS
030434,000115: 22,3263 05203 TC WAITLIST
030435,000116: 22,3264 E4,1540 EBANK= TFF
030436,000117: 22,3264 03430 44064 2CADR TICKTEST
030437,000118:
030438,000119: 22,3266 00003 RELINT
030439,000120: 22,3267 33320 V82GOFLP CAF TFFBANK # MAJOR RECYCLE LOOP ENTRY
030440,000121: 22,3270 54003 TS EBANK
030441,000122: 22,3271 34755 CAF ZERO
030442,000123: 22,3272 55537 TS V82FLAGS # ZERO FLAGS FOR TICKTEST. INHIBITS
030443,000124: # DECREMENTING OF TFF AND -TPER.
030444,000125: 22,3273 35021 CAF PRIO7
030445,000126: 22,3274 05105 TC FINDVAC # V82GOFF1 WILL EXECUTE STATE VECTOR
030446,000127: 22,3275 E4,1540 EBANK= TFF # UPDATE AND ORBIT CALCULATIONS FOR
030447,000128: 22,3275 03321 44064 2CADR V82GOFF1 # SELECTED VEHICLE ABOUT PROPER BODY.
030448,000129:
030449,000130: 22,3277 00003 RELINT
030450,000131: 22,3300 36250 V82STALL CAF THREE # STALL IN THIS LOOP AND WITHOLD V 16 N 44
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Page 716
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030452,000133: 22,3301 71537 MASK V82FLAGS # UNTIL STATE VECTOR UPDATE SETS ONE OF
030453,000134: 22,3302 10000 CCS A # OUR FLAG BITS.
030454,000135: 22,3303 03310 TC FLAGGON # EXIT FROM STALL LOOP.
030455,000136: 22,3304 34777 CAF 1SEC
030456,000137: 22,3305 04616 TC BANKCALL
030457,000138: 22,3306 01736 CADR DELAYJOB
030458,000139: 22,3307 03300 TC V82STALL
030459,000140:
030460,000141: 22,3310 33317 FLAGGON CAF V16N44 # MONITOR HAPO,HPER,TFF.
030461,000142: 22,3311 04616 TC BANKCALL
030462,000143: 22,3312 20334 CADR GOXDSPF
030463,000144: 22,3313 05563 TC B5OFF # TERM THIS TELLS TICKTEST TO KILL ITSELF
030464,000145: 22,3314 05563 TC B5OFF # PROCEED DITTO
030465,000146: 22,3315 03267 TC V82GOFLP # RECYCLE RECOMPUTE STATE VECT + DISPLAY
030466,000147:
030467,000148: 22,3316 01014 OPTIONVN VN 412
030468,000149: 22,3317 04054 V16N44 VN 1644
030469,000150: 22,3320 02140 TFFBANK ECADR TFF
030470,000151:
030471,000152: 22,3321 06042 V82GOFF1 TC INTPRET
030472,000153: 22,3322 77634 RTB
030473,000154: 22,3323 21574 LOADTIME
030474,000155: 22,3324 00041 STORE TDEC1 # TIME FOR STATE VECTOR UPDATE.
030475,000156: 22,3325 02205 STORE TSTART82 # TIME FOR INTERNAL USE.
030476,000157: 22,3326 77776 EXIT
030477,000158: 22,3327 41051 CS OPTIONX +1 # 1 FOR THIS VEHICLE, NOT 1 FOR OTHER.
030478,000159: 22,3330 64753 AD ONE
030479,000160: 22,3331 00006 EXTEND
030480,000161: 22,3332 13356 BZF THISSHIP
030481,000162: 22,3333 06042 OTHSHIP TC INTPRET
030482,000163: 22,3334 77624 CALL # CALL STATE VECTOR UPDATE FOR OTHER SHIP.
030483,000164: 22,3335 27042 OTHPREC
030484,000165: 22,3336 77775 BOTHSHIP VLOAD # MOVE RESULTS INTO TFFCONIC STORAGE AREAS
030485,000166: 22,3337 00001 RATT # TO BE CALLED BY SR30.1.
030486,000167: 22,3340 26207 STOVL RONE # RATT AT (-29)M FOR EARTH OR MOON
030487,000168: 22,3341 00007 VATT
030488,000169: 22,3342 02215 STORE VONE # VATT AT (-7)M/CS FOR EARTH OR MOON
030489,000170: 22,3343 77743 DLOAD*
030490,000171: 22,3344 73774 1/RTMUE,2 # X2 IS 0 FOR EARTH CENTERED STATE VEC
030491,000172: 22,3345 00037 STORE TFF/RTMU # X2 IS 2 FOR MOON
030492,000173: 22,3346 77743 DLOAD* # AS LEFT BY THISPREC OR OTHPREC.
030493,000174: 22,3347 72411 MINPERE,2
030494,000175: 22,3350 02201 STORE HPERMIN # TFFRTMU, HPERMIN AND RPADTEM ARE ALL
030495,000176: 22,3351 46135 SLOAD BHIZ # EARTH/MOON PARAMETERS AS SET HERE.
030496,000177: 22,3352 00050 X2
030497,000178: 22,3353 45367 EARTHPAD
030498,000179: 22,3354 77650 GOTO
030499,000180: 22,3355 45373 MOONPAD
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Page 717
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030501,000182: 22,3356 06042 THISSHIP TC INTPRET
030502,000183: 22,3357 77624 CALL # CALL STATE VECTOR UPDATE FOR THIS SHIP.
030503,000184: 22,3360 27056 THISPREC
030504,000185: 22,3361 77650 GOTO
030505,000186: 22,3362 45336 BOTHSHIP
030506,000187:
030507,000188: # THE FOLLOWING CONSTANTS ARE PAIRWISE INDEXED. DO NOT SEPARATE PAIRS.
030508,000189:
030509,000190: 22,3363 00001 11530 MINPERM 2DEC 10668 B-27 # 35 KFT MIN PERIGEE HEIGHT FOR MOON(-27)M
030510,000191: 22,3365 00002 31230 MINPERE 2DEC 91440 B-29 # 300 KFT (-29)M FOR EARTH
030511,000192:
030512,000193: 22,3367 43145 EARTHPAD DLOAD CLRGO # PAD 37-B RADIUS. SCALED AT (-29)M.
030513,000194: 22,3370 06340 RPAD
030514,000195: 22,3371 03635 V82EMFLG # INDICATE EARTH SCALING FOR SR30.1
030515,000196: 22,3372 45377 BOTHPAD
030516,000197:
030517,000198: 22,3373 51575 MOONPAD VLOAD ABVAL # COMPUTE MOON PAD RADIUS FROM RLS VECTOR.
030518,000199: 22,3374 02023 RLS # SCALED AT (-27)M.
030519,000200: 22,3375 77614 SET
030520,000201: 22,3376 03475 V82EMFLG # INDICATE MOON SCALING FOR SR30.1
030521,000202: 22,3377 36203 BOTHPAD STCALL RPADTEM
030522,000203: 22,3400 45551 SR30.1 # CALCULATE ORBITAL PARAMETERS
030523,000204: 22,3401 45234 RTB DSU
030524,000205: 22,3402 21574 LOADTIME
030525,000206: 22,3403 02205 TSTART82 # PRESENT TIME - TIME V82GOFF1 BEGAN
030526,000207: 22,3404 02205 STORE TSTART82 # SAVE IT
030527,000208: 22,3405 53145 DLOAD BZE # SR30.1 SETS -TPER=0 IF HPER L/
030528,000209: 22,3406 02143 -TPER # HPERMIN (300 OR 35) KFT.
030529,000210: 22,3407 45420 TICKTIFF # (-TPER = 0)
030530,000211: 22,3410 43345 TICKTPER DLOAD DAD # (-TPER NON ZERO) TFF WAS NOT COMPUTED,
030531,000212: 22,3411 02143 -TPER # BUT WAS SET TO 59M59S. DONT TICK TFF, DO
030532,000213: 22,3412 02205 TSTART82 # TICK -TPER. DISPLAY BOTH.
030533,000214: 22,3413 02143 STORE -TPER # -TPER CORRECTED FOR TIME SINCE V82GOFF1
030534,000215: 22,3414 77776 EXIT # BEGAN.
030535,000216: 22,3415 34753 CAF BIT1
030536,000217: 22,3416 55537 TS V82FLAGS # INFORMS TICKTEST TO INCREMENT ONLY -TPER
030537,000218: 22,3417 05155 TC ENDOFJOB
030538,000219:
030539,000220: 22,3420 43345 TICKTIFF DLOAD DAD # (-TPER=0) TFF WAS COMPUTED. TICK TFF.
030540,000221: 22,3421 02141 TFF # DO NOT TICK -TPER. DISPLAY TFF, BUT NOT
030541,000222: 22,3422 02205 TSTART82 # -TPER.
030542,000223: 22,3423 02141 STORE TFF # TFF CORRECTED FOR TIME SINCE V82GOFF1
030543,000224: 22,3424 77776 EXIT # BEGAN.
030544,000225: 22,3425 34752 CAF BIT2
030545,000226: 22,3426 55537 TS V82FLAGS # INFORMS TICKTEST TO INCREMENT ONLY TFF.
030546,000227: 22,3427 05155 TC ENDOFJOB
030547,000228:
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Page 718
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030549,000230: 22,3430 34747 TICKTEST CAF BIT5 # THIS WAITLIST PROGRAM PERPETUATES ITSELF
030550,000231: 22,3431 71043 MASK EXTVBACT # ONCE A SEC UNTIL BIT 5 OF EXTVBACT =0.
030551,000232: 22,3432 10000 CCS A
030552,000233: 22,3433 03441 TC DOTICK
030553,000234: 22,3434 37716 CAF PRIO25
030554,000235: 22,3435 05072 TC NOVAC # TERMINATE V 82. CANT CALL ENDEXT IN RUPT.
030555,000236: 22,3436 1043 EBANK= EXTVBACT
030556,000237: 22,3436 05472 04062 2CADR ENDEXT
030557,000238:
030558,000239: 22,3440 05261 TC TASKOVER
030559,000240: 22,3441 34777 DOTICK CAF 1SEC # RE-REQUEST TICKTEST.
030560,000241: 22,3442 05203 TC WAITLIST
030561,000242: 22,3443 E4,1540 EBANK= TFF
030562,000243: 22,3443 03430 44064 2CADR TICKTEST
030563,000244:
030564,000245: 22,3445 36250 CAF THREE
030565,000246: 22,3446 71537 MASK V82FLAGS
030566,000247: 22,3447 50000 INDEX A
030567,000248: 22,3450 03451 TC +1
030568,000249: 22,3451 05261 TC TASKOVER # IF NO FLAGBITS SET DONT CHANGE TFF OR
030569,000250: # -TPER, BUT CONTINUE LOOP.
030570,000251: 22,3452 03460 TC TPERTICK # ONLY BIT 1 SET. INCR -TPER BY 1 SEC.
030571,000252: 22,3453 34777 TFFTICK CAF 1SEC # ONLY BIT 2 SET. INCR TFF BY 1 SEC.
030572,000253: 22,3454 54001 TS L
030573,000254: 22,3455 34755 CAF ZERO
030574,000255: 22,3456 21541 DAS TFF
030575,000256: 22,3457 05261 TC TASKOVER
030576,000257: 22,3460 34777 TPERTICK CAF 1SEC
030577,000258: 22,3461 54001 TS L
030578,000259: 22,3462 34755 CAF ZERO
030579,000260: 22,3463 21543 DAS -TPER
030580,000261: 22,3464 05261 TC TASKOVER
030581,000262:
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Page 719
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030583,000264: 22,3465 77776 V82GON EXIT # AVERAGE G ON. USE CURRENT STATE VECTOR
030584,000265: # FOR ORBITAL PARAMETER CALCULATIONS.
030585,000266: 22,3466 35021 CAF PRIO7 # LESS THAN LAMBERT
030586,000267: 22,3467 05105 TC FINDVAC # V82GON1 WILL PERFORM ORBIT CALCULATIONS
030587,000268: 22,3470 E4,1540 EBANK= TFF # ABOUT PROPER BODY APPROX ONCE PER SEC.
030588,000269: 22,3470 03503 44064 2CADR V82GON1
030589,000270:
030590,000271: 22,3472 00003 RELINT
030591,000272: 22,3473 10067 CCS NEWJOB # WITHOLD V16 N44 UNTIL FIRST ORBIT CALC
030592,000273: 22,3474 05122 TC CHANG1 # IS DONE. NOTE: V82GON1 (PRIO7, FINDVAC
030593,000274: # JOB) IS COMPLETED BEFORE V82GON (PRIO7,
030594,000275: # NOVAC JOB).
030595,000276: 22,3475 33317 V82REDSP CAF V16N44 # MONITOR HAPO, HPER, TFF
030596,000277: 22,3476 04616 TC BANKCALL
030597,000278: 22,3477 20334 CADR GOXDSPF
030598,000279: 22,3500 05563 TC B5OFF # TERM THIS TELLS V82GON1 TO KILL ITSELF.
030599,000280: 22,3501 05563 TC B5OFF # PROC DITTO.
030600,000281: 22,3502 03475 TC V82REDSP # RECYCLE
030601,000282:
030602,000283: 22,3503 06042 V82GON1 TC INTPRET # THIS EXEC PROGRAM PERPETUATES ITSELF
030603,000284: # ONCE A SEC UNTIL BIT 5 OF EXTVBACT =0.
030604,000285: 22,3504 52175 VLOAD GOTO # HOLDS OFF CCS NEWJOB BETWEEN RN AND
030605,000286: 22,3505 01220 RN # VN FETCH SO RN, VN ARE FROM SAME
030606,000287: 22,3506 45507 NEXTLINE # STATE VECTOR UPDATE.
030607,000288: 22,3507 26207 NEXTLINE STOVL RONE # RN AT (-29)M FOR EARTH OR MOON
030608,000289: 22,3510 01226 VN
030609,000290: 22,3511 02215 STORE VONE # VN AT (-7)M/CS FOR EARTH OR MOON
030610,000291: 22,3512 52014 BON GOTO
030611,000292: 22,3513 04304 MOONTHIS # FLAG INDICATES BODY ABOUT WHICH ORBITAL
030612,000293: 22,3514 45516 MOONGON # CALCULATIONS ARE TO BE PERFORMED.
030613,000294: 22,3515 45527 EARTHGON # IF SET - MOON , IF RESET - EARTH.
030614,000295:
030615,000296: 22,3516 71214 MOONGON SET DLOAD
030616,000297: 22,3517 03475 V82EMFLG # INDICATE MOON SCALING FOR SR30.1
030617,000298: 22,3520 04001 1/RTMUM # LUNAR PARAMETERS LOADED HERE FOR SR30.1
030618,000299: 22,3521 14037 STODL TFF/RTMU
030619,000300: 22,3522 05364 MINPERM
030620,000301: 22,3523 26201 STOVL HPERMIN
030621,000302: 22,3524 02023 RLS # SCALED AT (-27)M.
030622,000303: 22,3525 52046 ABVAL GOTO
030623,000304: 22,3526 45536 V82GON2
030624,000305: 22,3527 71214 EARTHGON CLEAR DLOAD
030625,000306: 22,3530 03675 V82EMFLG # INDICATE EARTH SCALING FOR SR30.1
030626,000307: 22,3531 04003 1/RTMUE # EARTH PARAMETERS LOADED HERE FOR SR30.1
030627,000308: 22,3532 14037 STODL TFF/RTMU
030628,000309: 22,3533 05366 MINPERE
030629,000310: 22,3534 16201 STODL HPERMIN
030630,000311: 22,3535 06340 RPAD
030631,000312: 22,3536 36203 V82GON2 STCALL RPADTEM # COMMON CODE FOR EARTH & MOON.
030632,000313: 22,3537 45551 SR30.1
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Page 720
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030634,000315: 22,3540 77776 EXIT
030635,000316: 22,3541 34747 V82GON3 CAF BIT5
030636,000317: 22,3542 71043 MASK EXTVBACT # SEE IF ASTRONAUT HAS SIGNALLED TERMINATE
030637,000318: 22,3543 00006 EXTEND
030638,000319: 22,3544 15472 BZF ENDEXT # YES, TERMINATE VB 82 LOOP
030639,000320: 22,3545 34777 CAF 1SEC
030640,000321: 22,3546 04616 TC BANKCALL # WAIT ONE SECOND BEFORE REPEATING
030641,000322: 22,3547 01736 CADR DELAYJOB # ORBITAL PARAMETER COMPUTATION.
030642,000323: 22,3550 03503 TC V82GON1
030643,000324:
030644,000325: 22,3551 22,3541 SPLRET = V82GON3
030645,000326:
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Page 721
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030647,000328: # SUBROUTINE NAME: SR30.1
030648,000329: # MOD NO: 0 DATE: 16 FEB 67
030649,000330: # MOD BY: RR BAIRNSFATHER LOG SECTION: R32
030650,000331: # MOD NO: 1 MOD BY: RR BAIRNSFATHER DATE: 11 APR 67 SR30.1 CHANGED TO ALLOW MONITOR OPERN
030651,000332: # MOD NO: 2 MOD BY: RR BAIRNSFATHER DATE: 14 APR 67 ADD OVFL CK FOR RAPO
030652,000333: # MOD NO: 3 MOD BY ALONSO DATE: 11 DEC 67 SUBROUTINE REWRITTEN
030653,000334: # MOD NO: 4 MOD BY ALONSO DATE: 26 MAR 68 PROG MOD TO HANDLE DIF EARTH/MOON SCALE
030654,000335: # MOD NO: 5 MOD BY: RR BAIRNSFATHER DATE: 6 AUG 68 OVFL CK FOR HAPO & HPER. VOIDS MOD #2.
030655,000336:
030656,000337: # NEW FUNCTIONAL DESCRIPTION: ORBITAL PARAMETERS DISPLAY FOR NOUNS 32 AND 44.
030657,000338: # SR30.1 CALLS TFFCONMU AND TFFRP/RA TO CALCULATE RPER (PERIGEE RADIUS),
030658,000339: # RAPO (APOGEE RADIUS), HPER (PERIGEE HEIGHT ABOVE LAUNCH PAD OR LUNAR
030659,000340: # LANDING SITE), HAPO (APOGEE HEIGHT AS ABOVE), TPER (TIME TO PERIGEE),
030660,000341: # TFF (TIME TO INTERSECT 300 KFT ABOVE PAD OR 35KFT ABOVE LANDING SITE).
030661,000342: # IF HPER IS GREATER THAN OR EQUAL TO HPERMIN, CALCULATES TPER AND STORES
030662,000343: # NEGATIVE IN -TPER. OTHERWISE STORES +0 IN -TPER. WHENEVER TPER IS
030663,000344: # CALCULATED, TFF IS NOT COMPUTABLE AND DEFAULTS TO -59MIN 59SEC. IF HAPO
030664,000345: # WOULD EXCEED 9999.9 NM, IT IS LIMITED TO THAT VALUE FOR DISPLAY.
030665,000346:
030666,000347: # ADDENDUM: HAPO AND HPER SHOULD BE CHANGED TO READ HAPOX AND HPERX IN THE
030667,000348: # ABOVE REMARKS.
030668,000349:
030669,000350: # CALLING SEQUENCE: CALL
030670,000351: # SR30.1
030671,000352:
030672,000353: # SUBROUTINES CALLED: TFFCONMU, TFFRP/RA, CALCTPER, CALCTFF
030673,000354:
030674,000355: # NORMAL EXIT MODE: CALLING LINE +1 (STILL IN INTERPRETIVE MODE)
030675,000356:
030676,000357: # ALARMS: NONE
030677,000358:
030678,000359: # OUTPUT: RAPO (-29) M EARTH APOGEE RADIUS EARTH CENTERED COORD.
030679,000360: # (-27) M MOON MOON CENTERED COORD.
030680,000361: # RPER (-29) M EARTH PERIGEE RADIUS EARTH CENTERED COORD.
030681,000362: # (-27) M MOON MOON CENTERED COORD.
030682,000363: # HAPOX (-29) M APOGEE ALTITUDE ABOVE PAD OR LAND. SITE MAX VALUE LIMITED TO 9999.9 NM.
030683,000364: # HPERX (-29) M PERIGEE ALT. ABOVE PAD OR LAND. SITE MAX VALUE LIMITED TO 9999.9 NM.
030684,000365: # TFF (-28) CS TIME TO 300KFT OR 35KFT ALTITUDE
030685,000366: # -TPER (-28) CS TIME TO PERIGEE
030686,000367:
030687,000368: # ERASABLE INITIALIZATION REQUIRED-
030688,000369: # TFF/RTMU (+17) EARTH RECIPROCAL OF PROPER GRAV CONSTANT FOR
030689,000370: # (+14) MOON EARTH OR MOON = 1/SQRT(MU).
030690,000371: # RONE (-29) M STATE VECTOR
030691,000372: # VONE (-7) M/CS STATE VECTOR
030692,000373: # RPADTEM (-29) M EARTH RADIUS OF LAUNCH PAD OR LUNAR LANDING
030693,000374: # (-27) M MOON SITE.
030694,000375: # HPERMIN (-29) M EARTH (300 OR 35) KFT MINIMUM PERIGEE ALTITUDE
030695,000376: # (-27) M MOON ABOVE LAUNCH PAD OR LUNAR LANDING SITE.
030696,000377: # V82EMFLG (INT SW BIT) RESET FOR EARTH, SET FOR MOON.
030697,000378:
030698,000379: # DEBRIS: QPRET, PDL, S2
030699,000380:
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Page 722
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030701,000382: 22,3551 COUNT* $$/SR30S
030702,000383:
030703,000384: 22,3551 44001 SR30.1 SETPD STQ # INITIALIZE PUSHDOWN LIST.
030704,000385: 22,3552 00001 0
030705,000386: 22,3553 00051 S2
030706,000387: # SR30.1 INPUT: RONE AT (-29)M EARTH/MOON
030707,000388: # VONE AT (-7)M/CS
030708,000389: # TFFCONMU, TFFRP/RA, CALCTPER AND CALCTFF
030709,000390: # CALLS REQUIRE:
030710,000391: # EARTH CENTERED (NO RESCALING REQUIRED)
030711,000392: # RONE SCALED TO B-29 M
030712,000393: # VONE SCALED TO B-7 M/CS
030713,000394: # MOON CENTERED (RESCALING REQUIRED)
030714,000395: # RONE SCALED TO B-27 M
030715,000396: # VONE SCALED TO B-5 M/CS
030716,000397: 22,3554 77214 BOFF VLOAD
030717,000398: 22,3555 03755 V82EMFLG # OFF FOR EARTH, ON FOR MOON.
030718,000399: 22,3556 45565 TFFCALLS
030719,000400: 22,3557 02207 RONE
030720,000401: 22,3560 77752 VSL2
030721,000402: 22,3561 26207 STOVL RONE
030722,000403: 22,3562 02215 VONE
030723,000404: 22,3563 77752 VSL2
030724,000405: 22,3564 02215 STORE VONE
030725,000406: 22,3565 77624 TFFCALLS CALL
030726,000407: 22,3566 57362 TFFCONMU
030727,000408: 22,3567 77624 CALL # TFFRP/RA COMPUTES RAPO,RPER.
030728,000409: 22,3570 57430 TFFRP/RA
030729,000410: # RETURNS WITH RAPO IN D(MPAC).
030730,000411: 22,3571 77625 DSU
030731,000412: 22,3572 02203 RPADTEM
030732,000413: 22,3573 64414 BOFF SR2R # NEED HAPO AT (-29)M FOR DISPLAY.
030733,000414: # IF MOON CENTERED, RESCALE FROM (-27)M.
030734,000415: # IF EARTH CENTERED ALREADY AT (-29)M.
030735,000416: 22,3574 03755 V82EMFLG # OFF FOR EARTH , ON FOR MOON.
030736,000417: 22,3575 45576 +1
030737,000418: 22,3576 77624 CALL # IF HAPO > MAXNM, SET HAPO =9999.9 NM.
030738,000419: 22,3577 45636 MAXCHK # OTHERWISE STORE (RAPO-RPADTEM) IN HAPO.
030739,000420: 22,3600 16120 STORHAPO STODL HAPOX
030740,000421: 22,3601 00017 RPER
030741,000422: 22,3602 77625 DSU
030742,000423: 22,3603 02203 RPADTEM # GIVES HPER AT (-29)M EARTH, (-27)M MOON.
030743,000424: 22,3604 00161 STORE MPAC +4 # SAVE THIS FOR COMPARISON TO HPERMIN.
030744,000425: 22,3605 64414 BOFF SR2R # NEED HPER AT (-29)M FOR DISPLAY.
030745,000426: # IF MOON CENTERED, RESCALE FROM (-27)M.
030746,000427: # IF EARTH CENTERED ALREADY AT (-29)M.
030747,000428: 22,3606 03755 V82EMFLG # OFF FOR EARTH, ON FOR MOON.
030748,000429: 22,3607 45610 +1
030749,000430: 22,3610 77624 CALL # IF HPER > MAXNM, SET HPER = 9999.9 NM.
030750,000431: 22,3611 45636 MAXCHK
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Page 723
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030752,000433: 22,3612 16122 STORHPER STODL HPERX # STORE (RPER - RPADTEM) INTO HPERX.
030753,000434: 22,3613 00161 MPAC +4
030754,000435: 22,3614 51025 DSU BPL # HPERMIN AT (-29)M FOR EARTH, (-27)M MOON
030755,000436: 22,3615 02201 HPERMIN # IF HPER L/ HPERMIN (300 OR 35) KFT,
030756,000437: 22,3616 45622 DOTPER # THEN ZERO INTO -TPER.
030757,000438: 22,3617 52145 DLOAD GOTO # OTHERWISE CALCULATE TPER.
030758,000439: 22,3620 06524 HI6ZEROS
030759,000440: 22,3621 45626 SKIPTPER
030760,000441: 22,3622 45145 DOTPER DLOAD CALL
030761,000442: 22,3623 00017 RPER
030762,000443: 22,3624 57466 CALCTPER
030763,000444: 22,3625 77676 DCOMP # TPER IS PUT NEG INTO -TPER.
030764,000445: 22,3626 16143 SKIPTPER STODL -TPER
030765,000446: 22,3627 02201 HPERMIN # HPERMIN AT (-29)M FOR EARTH, (-27)M MOON
030766,000447: 22,3630 45015 DAD CALL
030767,000448: 22,3631 02203 RPADTEM # RPADTEM AT (-29)M FOR EARTH, (-27)M MOON
030768,000449: 22,3632 57471 CALCTFF # GIVES 59M59S FOR TFF IF RPER G/
030769,000450: 22,3633 77676 DCOMP # HPERMIN + RPADTEM. (TPER WAS NON ZERO)
030770,000451: 22,3634 36141 STCALL TFF # OTHERWISE COMPUTES TFF. (GOTO)
030771,000452: 22,3635 00051 S2
030772,000453:
030773,000454: 22,3636 51025 MAXCHK DSU BPL # IF C(MPAC) > 9999.9 NM, MPAC = 9999.9 NM
030774,000455: 22,3637 05646 MAXNM
030775,000456: 22,3640 45643 +3 # OTHERWISE C(MPAC) = B(MPAC).
030776,000457: 22,3641 43415 DAD RVQ
030777,000458: 22,3642 05646 MAXNM
030778,000459: 22,3643 43545 +3 DLOAD RVQ # (USED BY P30 - P37 ALSO)
030779,000460: 22,3644 05646 MAXNM
030780,000461:
030781,000462: 22,3645 01065 05603 MAXNM 2OCT 0106505603
030782,000463:
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Page 724
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030785,000466:
End of include-file R30.agc. Parent file is MAIN.agc