Readd some typos based on the original scans
This commit is contained in:
James Harris
oldmud0
parent
afa13e7364
commit
2f62a05a56
@ -111,7 +111,7 @@ CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D
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# SIGHT LIES ALONG THE STAR VECTOR.
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#
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# THE INPUTS ARE: 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE
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# COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB,AND
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# COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB, AND
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# ZNB.
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#
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# THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART
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@ -546,8 +546,8 @@ TRM03FLG = 026D # REQUEST TO NO REQUEST TO
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TRM03BIT = BIT4
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# BIT 3 FLAG 1
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SLOPESW = 027D # ITERATE WITH BIAS ITERATE WITH REGULAR
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# METHOD IN ITERATOR FALSE METHOD IN
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SLOPESW = 027D # ITERATE WITH BIAS ITERATE WITH REGULA
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# METHOD IN ITERATOR FALSI METHOD IN
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# ITERATOR
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SLOPEBIT = BIT3
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@ -76,7 +76,7 @@ LST2FAN TC VBZERO # VB40 ZERO (USED WITH NOUN 20 ONLY)
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TC V62 # VB62 SELECT MODE II, ERROR WRT N22
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TC V63 # VB63 SELECT MODE III, ERROR WRT N17
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TC VB64 # VB64 CALCULATE, DISPLAY S-BAND ANT ANGLES
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TC CKOPTVB # V 65 E OPTICAL VERIFICATION FOR PRELAUNCH
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TC CKOPTVB # V 65 E OPTICAL VERIFICATION FOR PRELAUNC
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TC ATTACHED # VB66 ATTACHED. MOVE THIS TO OTHER STATE
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TC V67 # VB67 W MATRIX MONITOR
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TC STROKON # VB68 CSM STROKE TEST ON.
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@ -932,7 +932,7 @@ DUMMYAD EXIT
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# Page 200
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TC BANKCALL
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CADR UPACTOFF # TURN OFF UPLINK ACTIVE LIGHT
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CADR UPACTOFF # TURN OFF UPLINK ACTIV LIGHT
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TC DOWNFLAG
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ADRES VHFRFLAG
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@ -1000,7 +1000,7 @@ RENDN00 CS MMNUMBER
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EXTEND
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BZF KILL20
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CA FLAGWRD0 # IS RENDEZVOUS FLAG SET
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CA FLAGWRD0 # IS RENDEZVOO FLAG SET
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MASK RNDVZBIT
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CCS A
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TCF STATQUO
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@ -430,7 +430,7 @@ FINETIME INHINT # RETURNS WITH INTERRUPT INHIBITED
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# INTEGRATED TOGETHER TO SAVE WORDS. COMPASS IS COMPLETELY RESTART
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# PROOFED EXCEPT FOR THE FIRST 30 SECONDS OR SO. PERFORMANCE TESTS OF
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# THE IRIGS IS RESTART PROOFED ENOUGH TO GIVE 75 PERCENT CONFIDENCE THAT
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# IF A RESTART OCCURS THE DATA WILL STILL BE GOOD. GOOD PRACTICE TO RECYCLE
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# IF A RESTART OCCURS THE DATA WILL STILL BE GOOD. GOOD PRACTICE TO RECYCL
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# WHEN A RESTART OCCURS UNLESS IT HAPPENS NEAR THE END OF A TEST -- THEN WAIT
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# FOR THE DATA TO FLASH.
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#
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@ -97,7 +97,7 @@ LOW7 OCT 177
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MASK LOW7 # WHERE CCS EDOP WILL HONOR IT NEXT.
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OPJUMP TS CYR # LOWWD ENTERS HERE IF A RIGHT-HAND OP
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CCS CYR # CODE IS TO BE PROCESSED. TEST PREFIXES.
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CCS CYR # CODE IS TO BE PROCESSED. TEST PREFICES.
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TCF OPJUMP2 # TEST SECOND PREFIX BIT.
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TCF EXIT # +0 OP CODE IS EXIT
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@ -401,7 +401,7 @@ STADR CA BANKSET # THE STADR CODE (PUSHUP UP ON STORE
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INCR LOC
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ITR1 INDEX LOC # THE STORECODE WAS STORED COMPLEMENTED TO
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CS 0 # MAKE IT LOOK LIKE AN OPCODE PAIR.
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AD NEGONE # (YUL CAN'T REMOVE 1 BECAUSE OF EARLY CCS)
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AD NEGONE # (YUL CANT REMOVE 1 BECAUSE OF EARLY CCS)
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DOSTORE TS ADDRWD
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MASK LOW11 # ENTRY FROM DISPATCHER. SAVE THE ERASABLE
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@ -1336,8 +1336,8 @@ UPPOS XCH L # SAVE DECREMENTED UPPER PART.
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AD HALF
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TS A # SKIPS ON OVERFLOW
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TCF +2
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INCR L # RESTORE UPPER TO ORIGINAL VALUE
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XCH L # SWAP A + L BANK.
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INCR L # RESTORE UPPER TO ROIGINAL VALUE
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XCH L # SWAP A + L BACK.
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TC Q
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UPNEG XCH L # SAVE COMPLEMENTED + DECREMENTED UPPER PT
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@ -278,7 +278,7 @@ BDZCHECK CA ZNDX
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BZF TAUCHECK
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ACRBDZ CA T5TEMP # Z-TRANSLATION ACCEPTED EVEN THO WE MAY
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TS RWORD1 # HAVE INTRODUCED AN UNDESIRABLE ROLL
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TS RWORD1 # HAVE INTRODUCED AN UNDESIREABLE ROLL
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TCF ROLLTIME # BRANCH TO JET ON-TIME CALCULATIONS
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TAUCHECK CCS TAU
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@ -127,7 +127,7 @@ ELRCODE OCT 22
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# THE RECEPTION OF A BAD CODE (I.E., CCC FAILURE) LOCKS OUT FURTHER UPLINK ACTIVITY BY SETTING BIT4 OF FLAGWRD7 = 1.
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# THIS INDICATION WILL BE TRANSFERRED TO THE GROUND BY THE DOWNLINK WHICH DOWNLINKS ALL FLAGWORDS.
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# WHEN UPLINK ACTIVITY IS LOCKED OUT, IT CAN BE ALLOWED WHEN THE GROUND UPLINKS AND `ERROR RESET' CODE.
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# (IT IS RECOMMENDED THAT THE `ERROR LIGHT RESET' CODE IS PRECEDED BY 16 BITS THE FIRST OF WHICH IS 1 FOLLOWED
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# (IT IS RECOMMENDED THAT THE `ERROR LIGHT RESET' CODE IS PRECEEDED BY 16 BITS THE FIRST OF WHICH IS 1 FOLLOWED
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# BY 15 ZEROS. THIS WILL ELIMINATE EXTRANEOUS BITS FROM INLINK WHICH MAY HAVE BEEN LEFT OVER FROM THE ORIGINAL
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# FAILURE).
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#
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@ -362,7 +362,7 @@ FAZC CALL
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GRP2PC
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# Page 1259
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VLOAD VAD # START 3RD PHASE OF INCORP2
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X789 # 7TH, 8TH, 9TH COMPONENTS OF STATE VECTOR
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X789 # 7TH,8TH,9TH,COMPONENT OF STATE VECTOR
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DELTAX +12D # INCORPORATION FOR X789
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STORE TX789
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BON RTB
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@ -227,9 +227,9 @@ GAMCOMP VLOAD VSR1
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# Page 1339
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36D
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STORE BETAM
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NORM BDDV # FORM NORMALIZE QUOTIENT ALPHAM/BETAM
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NORM BDDV # FORM NORMALIZED QUOTIENT ALPHAM/BETAM
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33D
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SR1R PUSH # C(PDL+2) = ALMOST NORMALIZE RHO.
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SR1R PUSH # C(PDL+2) = ALMOST NORMALIZED RHO.
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DLOAD*
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ASCALE,1
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STORE S1
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@ -420,7 +420,7 @@ DE-GR-50 TC 2PHSCHNG
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#
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# ABORT MODES: P23 ABORT IF MARKING SYSTEM OR EXTENDED VERB ACTIVE
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#
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# INPUT: NONE REQUIRES, NORMALLY CALLED BY P23
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# INPUT: NONE REQUIRED, NORMALLY CALLED BY P23
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#
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# OUTPUT: TRUNNION BIAS ANGLE: ANGLE DETERMINED WHEN SHAFT LINE OF SIGHT
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# (SLOS) AND LANDMARK LINE OF SIGHT (LLOS) ARE SUPERIMPOSED. THIS ANGLE
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@ -714,15 +714,15 @@ DECRM61 TS R61CNTR
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#
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# INPUT
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#
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# UM, 1/2 UNIT VECTOR ALONG THE CSM-LM LINE-OF-SIGHT (BASIC REF. SYSTEM)
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# UM,1/2 UNIT VECTOR ALONG THE CSM-LM LINE-OF-SIGHT (BASIC REF. SYSTEM)
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#
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# USTAR, FICTITIOUS STAR DIRECTION (1/2 UNIT VECTOR)
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# USTAR,FICTITIOUS STAR DIRECTION (1/2 UNIT VECTOR)
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#
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# RCLP, RELATIVE CSM TO LM POSITION VECTOR
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# RCLP,RELATIVE CSM TO LM POSITION VECTOR
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#
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# OUTPUT
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#
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# USTAR, MODIFIED FICTITIOUS STAR DIRECTION (1/2 UNIT VECTOR)
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# USTAR,MODIFIED FICTITIOUS STAR DIRECTION (1/2 UNIT VECTOR)
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#
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# BVECTOR = 9 DIMENSIONAL BVECTOR (1/2 UNIT VEC.)
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#
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@ -2707,7 +2707,7 @@ DP1MIN 2DEC 6000
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V89CALL TC BANKCALL # IMU STATUS CHECK. RETURNS IF ORIENTATION
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CADR R02BOTH # KNOWN. ALARMS IF NOT.
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CAF THREE # ALLOW ASTRONAUT TO SELECT DESIRED
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TS OPTION1 # TRACKING ATTITUDE AXIS
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TS OPTION1 # TRACKING ATTITUDE AXIS.
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CAF ONE
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TS OPTION1 +1
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CAF VB04N06 # V 04 N 06
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@ -39,7 +39,7 @@
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# COELLIPTIC SEQUENCE INITIATION (CSI) PROGRAMS (P32 AND P72)
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#
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# MOD NO -1 LOG SECTION -- P32-P35, P72-P75
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# MOD BY WHITE, P. DATE 1 JUNE 67
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# MOD BY WHITE. P DATE 1JUNE67
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#
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# PURPOSE
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# (1) TO CALCULATE PARAMETERS ASSOCIATED WITH THE FOLLOWING
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@ -317,8 +317,8 @@ V06N89* VN 0689
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#
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# FUNCTION -- TO DISPLAY THE LANDING SITE LATITUDE,
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# LONGITUDE AND ALTITUDE. TO ACCEPT NEW DATA VIA
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# THE KEYBOARD. TO COMPUT THE LANDING SITE
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# ORIENTATION FOR P52 OR P54.
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# THE KEYBOARD. TO COMPUTE THE LANDING SITE
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# ORIENTATION FOR P52 OR P54
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#
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# LET:
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# RLS = LANDING SITE VECTOR IN REF COORDINATES
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@ -516,7 +516,6 @@ SERVCAD2 = SERVCAD1
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# MOD NO: 0 DATE: 21 FEB 67
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# MOD BY: RR BAIRNSFATHER LOG SECTION: P61-P67
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# MOD NO: 1 MOD BY: RR BAIRNSFATHER DATE: 22 JUN 67 RESTARTS.
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#
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# FUNCTIONAL DESCRIPTION: CALLED BY BOTH P61 AND P62
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# FIRST, TEST TO SEE IF AVERAGEG IS ON. IF NOT, UPDATE THE STATE VECTOR TO PRESENT TIME + TOLERANCE
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# AND TURN ON AVERAGEG AT THAT TIME, AND CONTINUE. OTHERWISE CONTINUE: SEE IF IMU Y AXIS IS
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@ -2967,7 +2967,7 @@ ENDRELDS EQUALS
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# NVMONOPT IS AN ENTRY SIMILAR TO NVSUB, BUT REQUIRING AN ADDITIONAL
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# Page 370
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# PARAMETER IN L. IT SHOULD BE USED ONLY WITH A MONITOR VERB-NOUN CODE IN
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# A. AFTER EACH MONITOR DISPLAY A *PLEASE* VERB WILL BE PASSED INT THE VERB
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# A. AFTER EACH MONITOR DISPLAY A *PLEASE* VERB WILL BE PASTED IN THE VERB
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# LIGHTS OR DATA WILL BE BLANKED (OR BOTH) ACCORDING TO THE OPTIONS
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# SPECIFIED IN L. IF BITS 8-14 OF L ARE OTHER THAN ZERO, THEN THEY WILL
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# BE INTERPRETED AS A VERB CODE AND PASTED IN THE VERB LIGHTS. (THIS VERB
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@ -259,7 +259,7 @@ DOTICK CAF 1SEC # RE-REQUEST TICKTEST.
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MASK V82FLAGS
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INDEX A
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TC +1
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TC TASKOVER # IF NO FLAGBITS SET DON'T CHANGE TFF OR
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TC TASKOVER # IF NO FLAGBITS SET DONT CHANGE TFF OR
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# -TPER, BUT CONTINUE LOOP.
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TC TPERTICK # ONLY BIT 1 SET. INCR -TPER BY 1 SEC.
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TFFTICK CAF 1SEC # ONLY BIT 2 SET. INCR TFF BY 1 SEC.
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@ -281,7 +281,7 @@ V82GON EXIT # AVERAGE G ON. USE CURRENT STATE VECTOR
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2CADR V82GON1
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RELINT
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CCS NEWJOB # WITHHOLD V16 N44 UNTIL FIRST ORBIT CALC
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CCS NEWJOB # WITHOLD V16 N44 UNTIL FIRST ORBIT CALC
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TC CHANG1 # IS DONE. NOTE: V82GON1 (PRIO7, FINDVAC
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# JOB) IS COMPLETED BEFORE V82GON (PRIO7,
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# NOVAC JOB).
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@ -340,7 +340,7 @@ SPLRET EXIT
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EXTEND
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BZF SPLRET1
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V82GON3 CAF BIT5
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MASK EXTVBACT # SEE IF ASTRONAUT HAS SIGNALED TERMINATE
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MASK EXTVBACT # SEE IF ASTRONAUT HAS SIGNALLED TERMINATE
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EXTEND
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BZF ENDEXT # YES, TERMINATE VB 82 LOOP
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CAF 1SEC
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@ -295,7 +295,7 @@ TENTHSEK TS ATTSEC
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# ALSO IGNORE AUTOMATIC STEERING
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# SET = + BY
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# 1) INITIALIZATION PHASE OF AUTOPILOT
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# 2) OCCURRENCE OF RHC COMMANDS
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# 2) OCCURANCE OF RHC COMMANDS
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# 3) FREE MODE
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# 4) SWITCH OVER TO ATTITUDE HOLD FROM AUTO
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# WHILE DOING AUTOMATIC STEERING (IN THIS CASE
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@ -397,7 +397,7 @@ KRESUME1 TCF RESUME # END PHASE 1
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# MASK BIT3
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# ADS RCSFLAGS
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#
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# THEREAFTER, THE ATTITUDE ERRORS GENERATED BY THE USER SHOULD BE TRANSFERRED TO THE FOLLOWING LOCATIONS IN EBANK6:
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# THEREAFTER, THE ATTITUDE ERRORS GENERATED BY THE USER SHOULD BE TRANSFERED TO THE FOLLOWING LOCATIONS IN EBANK6:
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#
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# AK SCALED 180 DEGREES NOTE: THESE LOCATIONS ARE SUBJECT
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# AK1 SCALED 180 DEGREES TO CHANGE
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@ -136,7 +136,7 @@ TPMODE CAF ONE # MODE IS TP.
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# Page 1510
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TC Q
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INDEX A # OVERFLOW INCORRECT AND IN MSU.
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INDEX A # OVERFLOW UNCORRECT AND IN MSU.
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CAF LIMITS
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ADS MPAC
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TC Q
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@ -1240,7 +1240,7 @@ ENDZOPT TC ZEROPCDU # ZERO OCDU COUNTERS
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ZEROPCDU CAF ZERO
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TS CDUS # ZERO IN CDUS, -20 IN CDUT
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TS ZONE # INITIALIZE SHAFT MONITOR ZONE.
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TS ZONE # INITIALIZE SHAFT MONITOR ZONE
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CS 20DEGS
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TS CDUT
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TC Q
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@ -139,7 +139,7 @@ TFFTEM = 36D # TEMPORARY
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# TFFNP E:(-38+2NR) M LCP, SEMI LATUS RECTUM, WEIGHTED BY NR. FOR VGAMCALC.
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# M:(-36+2NR)
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# TFF/RTMU E:(17) M:(14) 1/SQRT(MU)
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# TFFVSQ E:(20) M:(18) 1/M -(V SQ/MU): PRESENT VELOCITY, NORMALIZED. FOR VGAMCALC
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# TFFVSQ E:(20) M:(18) 1/M -(V SQ/MU): PRESENT VELOCITY,NORMLIZED. FOR VGAMCALC
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# TFFALFA E:(26-NR) 1/M ALFA, WEIGHTED BY NR
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# M:(24-NR)
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# TFFRTALF E:(10+NA) SQRT(ALFA), NORMALIZED
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@ -136,7 +136,7 @@
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# PARABOLA WHICH PASSES THROUGH THE OPERATING POINT. FOR REGION 3
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# DESIRED OGARATE IS SIMPLY +-MAXLIM. FOR REGIONS 1 OR 6 THE SOLUTION
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# TO A QUADRATIC IS REQUIRED (THE PENETRATION IS ALONG THE STRAIGHT
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# LINE OR MINLIM BOUNDARY SWITCH LINES). AN APPROXIMATION IS MADE
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# LINE OR MINLIM BOUNDRY SWITCH LINES). AN APPROXIMATION IS MADE
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# INSTEAD. CONSIDER AN OPERATING POINT IN REGION 6'. PASS A TANGENT TO
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# THE CONTROL PARABOLA THROUGH THE OPERATING POINT, AND FIND ITS
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# INTERSECTION WITH THE STRAIGHT LINE SECTION OF THE SWITCH CURVE...
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@ -472,7 +472,7 @@ NOQBRSM DXCH ARUPT
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# LONGEXIT AND LONGEXIT+1
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# LONGTIME AND LONGTIME+1
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#
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# *** THE FOLLOWING IS TO BE IN FIXED-FIXED AND UNSWITCHED ERASABLE **
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# *** THE FOLLOWING IS TO BE IN FIXED-FIXED AND UNSWITCHED ERRASIBLE ***
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BLOCK 02
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EBANK= LST1
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@ -503,7 +503,7 @@ LNGCALL2 LXCH LONGEXIT +1 # SAVE THE CORRECT BB FOR RETURN
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# *** WAITLIST TASK LONGCYCL ***
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LONGCYCL EXTEND # CAN WE SUCCESSFULLY TAKE ABOUT 1.25
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LONGCYCL EXTEND # CAN WE SUCCESFULLY TAKE ABOUT 1.25
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DCS DPBIT14 # MINUTES OFF OF LONGTIME
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DAS LONGTIME
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@ -357,7 +357,7 @@ ASCTERM EXIT
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CALL
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FINDCDUW -2
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ASCTERM1 EXIT
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+1 CA FLAGWRD9 # ENSURE THAT THE NOUN 63 DISPLAY IS
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+1 CA FLAGWRD9 # INSURE THAT THE NOUN 63 DISPLAY IS
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MASK FLRCSBIT # BYPASSED IF WE ARE IN THE RCS TRIMMING
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CCS A # MODE OF OPERATION
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TCF ASCTERM3
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@ -55,7 +55,7 @@
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# BETWEEN THE PRE-IGNITION TIME CHECK -- ARE WE WITHIN 45 SECONDS OF TIG? -- AND TIG + 26 SECONDS, WHEN DPS
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# PROGRAMS THROTTLE UP.
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#
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# VARIATIONS AMONG PROGRAMS ARE ACCOMMODATED BY MEANS OF TABLES CONTAINING CONSTANTS (FOR AVEGEXIT, FOR
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# VARIATIONS AMONG PROGRAMS ARE ACCOMODATED BY MEANS OF TABLES CONTAINING CONSTANTS (FOR AVEGEXIT, FOR
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# WAITLIST, FOR PINBALL) AND TCF INSTRUCTIONS. USERS PLACE THE ADRES OF THE HEAD OF THE APPROPRIATE TABLE
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# (OF P61TABLE FOR P61LM, FOR EXAMPLE) IN ERASABLE REGISTER `WHICH' (E4). THE IGNITION ROUTINE THEN INDEXES BY
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# WHICH TO OBTAIN OR EXECUTE THE PROPER TABLE ENTRY. THE IGNITION ROUTINE IS INITIATED BY A TCF BURNBABY,
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@ -154,7 +154,7 @@ CALLGMBL EQUALS BIT5 # RCSFLAGS INITIALIZATION.
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TS NEXTU
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TS NEXTV
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CS TEN
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TS DAPZRUPT # TASK NOT IN PROGRESS, INITIALIZE NEG.
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TS DAPZRUPT # JASK NOT IN PROGRESS, INITIALIZE NEG.
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CA TWO
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TS NPTRAPS
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TS NQTRAPS
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@ -365,7 +365,7 @@ TRACKBIT = BIT5
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# BIT 3 FLAG 1 (S)
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SLOPESW = 027D # ITERATE WITH BIAS ITERATE WITH REGULAR
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# METHOD IN ITERATOR FALSE METHOD IN
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# METHOD IN ITERATOR FALSI METHOD IN
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SLOPEBIT = BIT3 # ITERATOR
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# BIT 2 FLAG 1 (S)
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@ -72,7 +72,7 @@
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# CHANNEL 12 CHAN12: OUTPUT CHANNEL; BITS USED TO DRIVE NAVIGATION AND SPACECRAFT HARDWARE.
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#
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# BIT 1 ZERO RR CDU; CDU'S GIVE RADAR INFORMATION FOR LM
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# BIT 1 ZERO RR CDU; CDU'S GIVE RRADAR INFORMATION FOR LM
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# BIT 2 ENABLE CDU RADAR ERROR COUNTERS
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# BIT 3 NOT USED
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# BIT 4 COARSE ALIGN ENABLE OF IMU
|
||||
|
||||
@ -65,7 +65,7 @@
|
||||
|
||||
# DISPLAYS USED IN P-31LM **
|
||||
#
|
||||
# V06N33 DISPLAY STORED TIG (IN HRS. MINS. SECS.)
|
||||
# V06N33 DISPLAY SOTRED TIG (IN HRS. MINS. SECS.)
|
||||
# V06N42 DISPLAY APOGEE, PERIGEE, DELTAV.
|
||||
# V16N35 DISPLAY TIME FROM TIG.
|
||||
# V06N45 TIME FROM IGNITION AND MIDDLE GIMBAL ANGLE.
|
||||
|
||||
@ -189,7 +189,7 @@ RRNB1 PUSH COS # SHAFT ANGLE TO 2
|
||||
# THIS ENTRY TO RRNB REQUIRES THE TRUNNION AND SHAFT ANGLES IN MPAC AND MPAC +1 RESPECTIVELY
|
||||
|
||||
RRNBMPAC STODL 20D # SAVE SHAFT CDU IN 21.
|
||||
MPAC # SET MODE TO DP. (THE PRECEDING STORE
|
||||
MPAC # SET MODE TO DP. (THE PRECEEDING STORE
|
||||
# MAY BE DP, TP OR VECTOR.)
|
||||
RTB SETPD
|
||||
CDULOGIC
|
||||
|
||||
@ -412,7 +412,7 @@ REDES1 DLOAD DSU
|
||||
# *********************************************************************
|
||||
#
|
||||
# RGVGCALC COMPUTATIONS ARE AS FOLLOWS:--
|
||||
# VELOCITY RELATIVE TO THE SURFACE
|
||||
# VELOCITY RELATIVE TO THE SURFACE:
|
||||
# _______ _ _ __
|
||||
# ANGTERM = V + R * WM
|
||||
# STATE IN GUIDANCE COORDINATES:
|
||||
|
||||
@ -347,7 +347,7 @@ R-RATE INCR NRTRAPS
|
||||
TS OMEGAR
|
||||
|
||||
# END OF RATE DERIVATION
|
||||
# BEGIN OFFSET ESTIMATOR
|
||||
# BEGIN OFFSET ESTIMATER
|
||||
# IN POWERED FLIGHT, AOSTASK WILL BE CALLED EVERY 2 SECONDS.
|
||||
# AOS = AOS + K*SUMRATE
|
||||
|
||||
|
||||
@ -47,7 +47,7 @@ P12LM TC PHASCHNG
|
||||
TC UPFLAG # PREVENT R10 FROM ISSUING CROSS-POINTER
|
||||
ADRES R10FLAG # OUTPUTS.
|
||||
|
||||
TC CLRADMOD # INITIALIZE RADMODES FOR R29
|
||||
TC CLRADMOD # INITIALIZE RADMODES FOR R29.
|
||||
|
||||
TC DOWNFLAG # CLEAR RENDEZVOUS FLAG FOR P22
|
||||
ADRES RNDVZFLG
|
||||
|
||||
@ -30,7 +30,7 @@
|
||||
# COELLIPTIC SEQUENCE INITIATION (CSI) PROGRAMS (P32 AND P72)
|
||||
#
|
||||
# MOD NO -1 LOG SECTION -- P32-P35, P72-P75
|
||||
# MOD BY WHITE, P. DATE 1 JUNE 67
|
||||
# MOD BY WHITE.P DATE 1JUNE67
|
||||
#
|
||||
# PURPOSE
|
||||
|
||||
@ -107,7 +107,7 @@
|
||||
# CALCULATES THE MANEUVER PARAMETERS. SET AT THE START OF
|
||||
# EACH RENDEZVOUS PRE-THRUSTING PROGRAM.
|
||||
#
|
||||
# FINAL FLAG -- SELECTED FINAL PROGRAM DISPLAYS AFTER CREW HAS
|
||||
# FINAL FLAG -- SELECTS FINAL PROGRAM DISPLAYS AFTER CREW HAS
|
||||
# COMPLETED THE FINAL MANEUVER COMPUTATION AND DISPLAY
|
||||
# CYCLE.
|
||||
#
|
||||
|
||||
@ -476,7 +476,7 @@ QERRCALC CAE CDUY # Q-ERROR CALCULATION
|
||||
TS DAPTEMP2 # SAVE FOR RERRCALC
|
||||
EXTEND
|
||||
MP M22 # (CDUZ-CDUZD)*M22 SCALED AT PI RADIANS
|
||||
AD DELQEROR # KALCMANU INTERFACE ERROR
|
||||
AD DELQEROR # KALCMANU INERFACE ERROR
|
||||
AD E
|
||||
XCH QERROR # SAVE Q-ERROR FOR EIGHT-BALL DISPLAY.
|
||||
|
||||
@ -487,7 +487,7 @@ RERRCALC CAE DAPTEMP1 # R-ERROR CALCULATION:
|
||||
CAE DAPTEMP2 # SECOND TERM CALCULATION:
|
||||
EXTEND # CDU ANGLE -ANGLE DESIRED (Z-AXIS)
|
||||
MP M32 # (CDUZ-CDUZD)*M32 SCALED AT PI RADIANS
|
||||
AD DELREROR # KALCMANU INTERFACE ERROR
|
||||
AD DELREROR # KALCMANU INERFACE ERROR
|
||||
AD E
|
||||
XCH RERROR # SAVE R-ERROR FOR EIGHT-BALL DISPLAY.
|
||||
TC Q
|
||||
|
||||
@ -36,7 +36,7 @@
|
||||
# RADAR SAMPLING LOOP.
|
||||
|
||||
COUNT* $$/RLEAD
|
||||
RADSAMP CCS RSAMPDT # TIMES NORMAL ONCE PER SECOND SAMPLING
|
||||
RADSAMP CCS RSAMPDT # TIMES NORMAL ONCE-PER-SECOND SAMPLING
|
||||
TCF +2
|
||||
TCF TASKOVER # +0 INSERTED MANUALLY TERMINATES TEST.
|
||||
|
||||
|
||||
@ -113,7 +113,7 @@ TPMODE CAF ONE # MODE IS TP.
|
||||
TS MPAC # AND SKIP ON OVERFLOW.
|
||||
TC Q
|
||||
|
||||
INDEX A # OVERFLOW INCORRECT AND IN MSU.
|
||||
INDEX A # OVERFLOW UNCORRECT AND IN MSU.
|
||||
CAF LIMITS
|
||||
ADS MPAC
|
||||
TC Q
|
||||
|
||||
@ -132,7 +132,7 @@ DOIT CA PIF
|
||||
TS TTHROT
|
||||
|
||||
# SINCE /AF/ IS NOT AN INSTANTANEOUS ACCELERATION, BUT RATHER AN "AVERAGE" OF THE ACCELERATION LEVELS DURING
|
||||
# THE PRECEDING PIPA INTERVAL, AND SINCE FP IS COMPUTED DIRECTLY FROM /AF/, FP IN ORDER TO CORRESPOND TO THE
|
||||
# THE PRECEEDING PIPA INTERVAL, AND SINCE FP IS COMPUTED DIRECTLY FROM /AF/, FP IN ORDER TO CORRESPOND TO THE
|
||||
# ACTUAL THRUST LEVEL AT THE END OF THE INTERVAL MUST BE WEIGHTED BY
|
||||
#
|
||||
# PIF(PPROCESS + TL) PIF /PIF/
|
||||
|
||||
Loading…
Reference in New Issue
Block a user