2016-07-07 08:47:26 +00:00
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# Copyright: Public domain.
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# Filename: AOSTASK_AND_AOSJOB.agc
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# Purpose: Part of the source code for Luminary 1A build 099.
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# It is part of the source code for the Lunar Module's (LM)
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# Apollo Guidance Computer (AGC), for Apollo 11.
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# Assembler: yaYUL
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# Contact: Ron Burkey <info@sandroid.org>.
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# Website: www.ibiblio.org/apollo.
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# Pages: 1485-1506
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# Mod history: 2009-05-27 RSB Adapted from the corresponding
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# Luminary131 file, using page
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# images from Luminary 1A.
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# 2009-06-05 RSB Corrected a memory-bank error type.
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# 2009-06-07 RSB Corrected a typo.
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#
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# This source code has been transcribed or otherwise adapted from
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# digitized images of a hardcopy from the MIT Museum. The digitization
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# was performed by Paul Fjeld, and arranged for by Deborah Douglas of
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# the Museum. Many thanks to both. The images (with suitable reduction
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# in storage size and consequent reduction in image quality as well) are
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# available online at www.ibiblio.org/apollo. If for some reason you
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# find that the images are illegible, contact me at info@sandroid.org
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# about getting access to the (much) higher-quality images which Paul
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# actually created.
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#
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# Notations on the hardcopy document read, in part:
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#
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# Assemble revision 001 of AGC program LMY99 by NASA 2021112-61
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# 16:27 JULY 14, 1969
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# Page 1485
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# PROGRAM NAME: 1/ACCS
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# PROGRAM WRITTEN BY: BOB COVELLI AND MIKE HOUSTON
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# LAST MODIFICATION: FEB. 14, 1969 BY G. KALAN
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#
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# PROGRAM DESCRIPTION:
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# 1/ACCS PROVIDES THE INTERFACE BETWEEN THE GUIDANCE PROGRAMS AND THE DIGITAL AUTOPILOT. WHENEVER THERE IS A
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# CHANGE IN THE MASS OF THE VEHICLE, IN THE DEADBAND SELECTED, IN THE VEHICLE CONFIGURATION (ASCENT-DESCENT-
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# DOCKED), AND DURING A FRESH START OR A RESTART, 1/ACCS IS CALLED TO COMMUNICATE THE DATA CHANGES TO THE DAP.
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#
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# THE INPUTS TO 1/ACCS ARE MASS, ACCELERATION (ABDELV), DEADBAND (DB), OFFSET ACCELERATIONS (AOSQ AND AOSR),
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# STAGE VERIFY BIT (CHAN30, BIT2), DOCKED BIT (DAPBOOLS, BIT13), DRIFT BIT (DAPBOOLS, BIT8), USEQRJTS (DAPBOOLS,
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# BIT14), AND SURFACE FLAG (FLAGWRDB, BIT8), AND CH5MASK.
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#
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# 1/ACCS COMPUTES THE JET ACCELERATIONS (1JACC, 1JACCQ, 1JACCR) AS FUNCTIONS OF MASS. 1JACCU AND 1JACCV ARE
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# FORMED BY RESOLVING 1JACCQ AND 1JACCR. IN THE DESCENT CASE, THE DESCENT ENGINE MOMENT ARM (L, PVT-CG) IS ALSO
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# COMPUTED AS A FUNCTION OF MASS. THE RATE OF CHANGE OF ACCELERATION DUE TO ROTATION OF THE GIMBAL (ACCDOTQ,
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# ACCDOTR) IS ALSO COMPUTED IN THE DESCENT CASE.
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#
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# AFTER THE ABOVE COMPUTATIONS, THE PROGRAM 1/ACCONT COMPUTES THE RECIPROCAL NET ACCELERATIONS ABOUT THE P, U,
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# AND V AXES (2 JETS FOR P-AXIS, BOTH 1 AND 2 JETS FOR U AND V AXES), AND THE RECIPROCAL COAST ACCELERATIONS ABOUT
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# THE P, U, AND V AXES. THE ACCELERATION FUNCTIONS (ACCFCTZ1 AND ACCFCTZ5) ARE ALSO COMPUTED FOR THESE AXES. THE
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# FIRE AND COAST DEADBANDS AND AXISDIST ARE COMPUTED FOR EACH AXIS. FLAT AND ZONE3LIM, THE WIDTH AND HEIGHT OF THE
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# MINIMUM IMPULSE ZONE, ARE COMPUTED. 1/ACCONT ALSO SETS ACCSWU AND ACCSWV, WHICH INDICATE WHEN 1 JET ACCELERATION
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# IS NOT SUFFICIENT TO PRODUCE MINIMUM ACCELERATION. AT THE COMPLETION OF 1/ACCS, THE ACCSOKAY BIT IS SET.
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#
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# SUBROUTINES CALLED:
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# TIMEGMBL
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# MAKECADR
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# ROT45DEG
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#
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# CALLING SEQUENCE:
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# TC BANKCALL # (1/ACCS MUST BE CALLED BY BANKCALL)
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# CADR 1/ACCS
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#
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# NORMAL EXIT: VIA BANKJUMP
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#
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# ALARM AND EXIT MODES: NONE
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#
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# INPUT/OUTPUT: SEE PROGRAM DESCRIPTION.
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#
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# DEBRIS:
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# ALL OF THE EXECUTIVE TEMPORARY REGISTERS, EXCEPT FIXLOC AND OVFIND, AND THE CORE SET AREA FROM MPAC TO BANKSET.
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#
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# RESTRICTIONS:
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# 1/ACCS MUST BE CALLED BY BANKCALL
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# EBANK IS SET TO 6, BUT NOT RESTORED.
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# Page 1486
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BANK 20
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SETLOC DAPS3
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BANK
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COUNT* $$/DAPAO
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EBANK= AOSQ
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# ENTRY IS THROUGH 1/ACCJOB OR 1/ACCSIT WHEN 1/ACCS IS TO BE DONE AS A SEPARATE NOVAC JOB.
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# IT IS POSSIBLE FOR MORE THAN ONE OF THESE JOBS TO BE SET UP CONCURRENTLY. HOWEVER, SINCE THERE IS NO CHECK OF
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# NEWJOB, A SECOND MANIFESTATION CANNOT BE STARTED UNTIL THE FIRST IS COMPLETED.
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1/ACCSET CAF ZERO # ENTRY FROM FRESH START/RESTART CODING.
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TS AOSQ # NULL THE OFFSET ESTIMATES FOR 1/ACCS.
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TS AOSR
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TS ALPHAQ # NULL THE OFFSET ESTIMATES FOR DOWNLIST
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TS ALPHAR
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1/ACCJOB TC BANKCALL # 1/ACCS ASSUMES ENTRY VIA BANKCALL.
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CADR 1/ACCS +2 # SKIP EBANK SETTING.
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TC ENDOFJOB
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1/ACCS CA EBANK6 # ***** EBANK SET BUT NOT RESTORED *****
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TS EBANK
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TC MAKECADR # SAVE RETURN SO THAT BUF2 MAY BE USED
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TS ACCRETRN
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# DETERMINE MASS OF THE LEM.
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CA DAPBOOLS # IS THE CSM DOCKED
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MASK CSMDOCKD
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TS DOCKTEMP # STORE RECORD OF STATE IN TEMP (MPAC +3).
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CCS A
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CS CSMMASS # DOCKED: LEMMAS = MASS - CSMMASS
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AD MASS # LEM ALONE: LEMMASS = MASS
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TS LEMMASS
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# ON THE BASIS OF APSFLAG:
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# SET THE P-AXIS RATE COMMAND LIMIT FOR 2-JET/2-JET CONTROL
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# SET MPAC, WHICH INDICATES THE PROPER SET OF COEFFICIENTS FOR THE LEM-ALONE F(MASS) CALCULATIONS
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# ENSURE THAT THE LEM MASS VALUE IS WITHIN THE ACCEPTABLE RANGE
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INHINT
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CAE FLGWRD10 # DETERMINE WHETHER STAGED.
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MASK APSFLBIT
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EXTEND
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BZF DPSFLITE
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# Page 1487
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CS POSMAX # ASCENT (OR ON LUNAR SURFACE)
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TS -2JETLIM # ALWAYS 2 JETS FOR P-AXIS RATE COMMAND
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CAF OCT14 # INITIALIZE INDEX AT 12.
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TS MPAC
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CS LEMMASS # CHECK IF MASS TOO HIGH. CATCH STAGING.
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AD HIASCENT
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EXTEND
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BZMF MASSFIX
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CS LEMMASS # CHECK IF MASS TOO LOW. THIS LIMITS THE
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AD LOASCENT # DECREMENTING BY MASSMON.
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EXTEND
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BZMF F(MASS)
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MASSFIX ADS LEMMASS # STORE THE VIOLATED LIMIT AS LEMMASS.
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ZL # ALSO CORRECT TOTAL MASS, ZEROING THE
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CCS DOCKTEMP # LOW-ORDER WORD.
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CAE CSMMASS # DOCKED: MASS = LEMMASS + CSMMASS
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AD LEMMASS # LEM ALONE: MASS = LEMMASS
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DXCH MASS
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TCF F(MASS)
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DPSFLITE CS BIT10 # FOUR JETS FOR P-AXIS RATE COMMAND ERRORS
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TS -2JETLIM # EXCEEDING 1.4 DEG/SEC (SCALED AT 45)
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CAF SIX # INITIALIZE INDEX AT 6.
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TS MPAC
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CS LEMMASS # CHECK IF MASS TOO HIGH. SHOULD NEVER
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AD HIDESCNT # OCCUR EXCEPT PERHAPS BEFORE THE PAD
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EXTEND # LOAD IS DONE.
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BZMF MASSFIX
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CS LEMMASS # CHECK IF MASS TOO LOW. THIS LIMITS THE
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AD LODESCNT # DECREMENTING BY MASSMON.
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AD HIASCENT
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EXTEND
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BZMF F(MASS)
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TCF MASSFIX
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# COMPUTATION OF FUNCTIONS OF MASS
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F(MASS) RELINT
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CCS DOCKTEMP
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TCF DOCKED # DOCKED: USE SEPARATE COMPUTATION.
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CA TWO
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STCTR TS MPAC +1 # J=2,1,0 FOR 1JACCR,1JACCQ,1JACC
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CS TWO
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ADS MPAC # JX=10,8,6 OR 4,2,0 TO INDEX COEFS.
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STCTR1 CAE LEMMASS
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INDEX MPAC
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AD INERCONC
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TS MPAC +2 # MASS + C
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# Page 1488
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EXTEND
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INDEX MPAC
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DCA INERCONA
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EXTEND
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DV MPAC +2
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INDEX MPAC
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AD INERCONB
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INDEX MPAC +1 # 1JACC(J)=A(JX)/(MASS+C(JX) + B(JX)
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TS 1JACC # 1JACC(-1)=L,PVT-CG SCALED AT 8 FEET
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CCS MPAC +1
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TCF STCTR
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TCF COMMEQS
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TCF LRESC
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# COEFFQ AND COEFFR ARE COMPUTED IN THIS SECTION. THEY ARE USED TO RESOLVE Q-R COMPONENTS INTO NON-ORTHOGONAL
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# U AND V COMPONENTS (SEE ROT-TOUV SECTION).
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COMMEQS CS 1JACCR
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AD 1JACCQ
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EXTEND
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BZMF BIGIQ
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EXTEND # EPSILON IS A MEASURE OF COUPLING AND IS
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DV 1JACCQ # DEFINED=1-IQ/IR FOR IR GREATER THAN IQ.
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TS EPSILON # THE COMPUTED EXPRESSION IS EQUIVALENT
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AD -EPSMAX
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EXTEND
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BZMF GOODEPS1
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CS -EPSMAX
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TS EPSILON # EPSILON IS LIMITED TO A MAX. OF .42265
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GOODEPS1 CA EPSILON
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EXTEND
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MP 0.35356
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AD .7071
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TS COEFFR # IN THIS CASE WHERE IR IS GREATER THAN
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CS POSMAX # IQ, COEFFQ=-.707(1+.5EPSILON)(1-EPSILON)
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AD EPSILON # AND COEFFR=.707(1+.5EPSILON)
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EXTEND
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MP COEFFR
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TS COEFFQ
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TCF JACCUV
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BIGIQ EXTEND # EPSILON IS DEFINED AS 1-IR/IQ FOR IQ
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DV 1JACCR # GREATER THAN IR. -EPSILON IS COMPUTED
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TS -EPSILON # RATHER THAN EPSILON FOR CONVENIENCE
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CS -EPSILON
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AD -EPSMAX
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EXTEND
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BZMF GOODEPS2
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CA -EPSMAX
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TS -EPSILON # EPSILON IS LIMITED TO A MAX. OF .42265
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# Page 1489
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GOODEPS2 CA -EPSILON
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EXTEND
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MP 0.35356
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AD -.7071
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TS COEFFQ # IN THIS CASE WHERE IQ IS GREATER THAN
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CS -EPSILON # IR, COEFFQ=-.707(1+.5EPSILON) AND
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AD NEGMAX # COEFFR=.707(1+.5EPSILON)(1-EPSILON)
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EXTEND
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MP COEFFQ
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TS COEFFR
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JACCUV CS COEFFQ
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EXTEND
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MP 1JACCQ # 1JACCQ IS SCALED AT PI/4
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TS 1JACCU # 1JACCU USED AS TEMPORARY STORAGE
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CA COEFFR
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EXTEND
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MP 1JACCR
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AD 1JACCU
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EXTEND
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MP BIT14 # SCALING CHANGED FROM PI/4 TO PI/2
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TS 1JACCU
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TS 1JACCV # SCALED AT PI/2 RADIANS/SEC(2)
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CCS MPAC # COMPUTE L,PVT-CG IF IN DESCENT
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CAF ZERO # ZERO SWITCHES AND GO TO 1/ACCONT IN
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TS ALLOWGTS # ASCENT
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TCF 1/ACCONT -1
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CS TWO
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TS MPAC
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CS ONE
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TS MPAC +1
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TCF STCTR1
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# THIS SECTION COMPUTES THE RATE OF CHANGE OF ACCELERATION DUE TO THE ROTATION OF THE GIMBALS. THE EQUATION
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2016-07-10 18:56:18 +00:00
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# IMPLEMENTED IN BOTH THE Y-X PLANE AND THE Z-X PLANE IS -- D(ALPHA)/DT = TL/I*D(DELTA)/DT, WHERE
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2016-07-07 08:47:26 +00:00
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# T = ENGINE THRUST FORCE
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2016-07-10 19:08:21 +00:00
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# L = PIVOT TO CG DISTANCE OF ENGINE
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2016-07-07 08:47:26 +00:00
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# I = MOMENT OF INERTIA
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LRESC CAE ABDELV # SCALED AT 2(13) CM/SEC(2)
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EXTEND
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MP MASS # SCALED AT B+16 KGS
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TC DVOVSUB # GET QUOTIENT WITH OVERFLOW PROTECTION
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ADRES GFACTM
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# MASS IS DIVIDED BY ACCELERATION OF GRAVITY IN ORDER TO MATCH THE UNITS OF IXX,IYY,IZZ, WHICH ARE SLUG-FT(2).
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# THE RATIO OF ACCELERATION FROM PIPAS TO ACCELERATION OF GRAVITY IS THE SAME IN METRIC OR ENGINEERING UNITS, SO
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# THAT IS UNCONVERTED. 2.20462 CONVERTS KG. TO LB. NOW T IN IN A SCALED AT 2(14).
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EXTEND
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MP L,PVT-CG # SCALED AT 8 FEET.
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# Page 1490
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INHINT
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TS MPAC
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EXTEND
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MP 1JACCR
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TC DVOVSUB # GET QUOTIENT WITH OVERFLOW PROTECTION
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ADRES TORKJET1
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TS ACCDOTR # SCALED AT PI/2(7)
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CA MPAC
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EXTEND
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MP 1JACCQ
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TC DVOVSUB # GET QUOTIENT WITH OVERFLOW PROTECTION
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ADRES TORKJET1
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SPSCONT TS ACCDOTQ # SCALED AT PI/2(7)
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EXTEND
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MP DGBF # .3ACCDOTQ SCALED AT PI/2(8)
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TS KQ
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CAE ACCDOTR # .3ACCDOTR AT PI/2(8)
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EXTEND
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MP DGBF
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TS KRDAP
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EXTEND # NOW COMPUTE QACCDOT, RACCDOT, THE SIGNED
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READ CHAN12 # JERK TERMS. STORE CHANNEL 12. WITH GIMBAL
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TS MPAC +1 # DRIVE BITS 9 THROUGH 12 SET LOOP
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CAF BIT2 # INDEX TO COMPUTE RACCDOT, THEN QACCDOT.
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TCF LOOP3
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CAF ZERO # ACCDOTQ AND ACCDOTR ARE NOT NEGATIVE,
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LOOP3 TS MPAC # BECAUSE THEY ARE MAGNITUDES
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CA MPAC +1
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INDEX MPAC # MASK CHANNEL IMAGE FOR ANY GIMBAL MOTION
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MASK GIMBLBTS
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EXTEND
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BZF ZACCDOT # IF NONE, Q(R)ACCDOT IS ZERO.
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CA MPAC +1
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INDEX MPAC # GIMBAL IS MOVING. IS ROTATION POSITIVE.
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MASK GIMBLBTS +1
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EXTEND
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BZF FRSTZERO # IF NOT POSITIVE, BRANCH
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INDEX MPAC # POSITIVE ROTATION, NEGATIVE Q(R)ACCDOT.
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CS ACCDOTQ
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TCF STACCDOT
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FRSTZERO INDEX MPAC # NEGATIVE ROTATION, POSITIVE Q(R)ACCDOT.
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CA ACCDOTQ
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TCF STACCDOT
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ZACCDOT CAF ZERO
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STACCDOT INDEX MPAC
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TS QACCDOT # STORE Q(R)ACCDOT.
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CCS MPAC
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TCF LOOP3 -1 # NOW DO QACCDOT.
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# Page 1491
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CS DAPBOOLS # IS GIMBAL USABLE?
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MASK USEQRJTS
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EXTEND
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BZF DOWNGTS # NO. BE SURE THE GIMBAL SWITCHES ARE DOWN
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CS T5ADR # YES. IS THE DAP RUNNINT?
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AD PAXISADR
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EXTEND
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BZF +2
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TCF DOWNGTS # NO. BE SURE THE GIMBAL SWITCHES ARE DOWN
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CCS INGTS # YES. IS GTS IN CONTROL?
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TCF DOCKTEST # YES. PROCEED WITH 1/ACCS.
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TC IBNKCALL # NO. NULL OFFSET AND FIND ALLOWGTS
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CADR TIMEGMBL
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DOCKTEST CCS DOCKTEMP # BYPASS 1/ACCONT WHEN DOCKED.
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TCF 1/ACCRET
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TCF 1/ACCONT
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# Page 1492
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# SUBROUTINE: DVOVSUB
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# AUTHOR: C. WORK, MOD 0, 12 JUNE 68
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# PURPOSE: THIS SUBROUTINE PROVIDES A SINGLE-PRECISION MACHINE LANGUAGE DIVISION OPERATION WHICH RETURNS
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# (1) THE QUOTIENT, IF THE DIVISION WAS NORMAL.
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# (2) NEGMAX, IF THE QUOTIENT WAS IMPROPER AND NEGATIVE.
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# (3) POSMAX, IF THE QUOTIENT WAS IMPROPER AND POSITIVE OR IF THERE WAS A ZERO DIVISOR.
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# THE CALLING PROGRAM IS PRESUMED TO BE A JOB IN THE F BANK WHICH CONTAINS DVOVSUB. E BANK MUST BE 6.
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# THE DIVISOR FOR THIS ROUTINE MAY BE IN EITHER FIXED OR ERASABLE STORAGE. SIGN AGREEMENT IS
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# ASSUMED BETWEEN THE TWO HALVES OF THE DIVIDEND. (THIS IS CERTAIN IF THE A AND L REGISTERS ARE THE
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# RESULT OF A MULTIPLICATION OPERATION.)
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# CALL SEQUENCE: L TC DVOVSUB
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# L +1 ADRES (DIVISOR)
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# L +2 RETURN HERE, WITH RESULT IN A,L
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# INPUT: DIVIDEND IN A,L (SIGN AGREEMENT ASSUMED), DIVISOR IN LOCATION DESIGNATED BY "ADRES".
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# DIVISOR MAY BE IN THE DVOVSUB FBANK,FIXED-FIXED FBANK,EBANK 6, OR UNSWITCHED ERASABLE.
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# OUTPUT: QUOTIENT AND REMAINDER, OR POSMAX (NEGMAX), WHICHEVER IS APPROPRIATE.
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# DEBRIS: SCRATCHX,SCRATCHY,SCRATCHZ,A,L (NOTE: SCRATCHX,Y,Z ARE EQUATED TO MPAC +4,+5, AND +6.)
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# ABORTS OR ALARMS: NONE
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# EXITS: TO THE CALL POINT +2.
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# SUBROUTINES CALLED: NONE.
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DVOVSUB TS SCRATCHY # SAVE UPPER HALF OF DIVIDEND
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TS SCRATCHX
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INDEX Q # OBTAIN ADDRESS OF DIVISOR.
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CA 0
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INCR Q # STEP Q FOR PROPER RETURN SEQUENCE.
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INDEX A
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CA 0 # PICK UP THE DIVISOR.
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EXTEND # RETURN POSMAX FOR A ZERO DIVISOR.
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BZF MAXPLUS
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TS SCRATCHZ # STORE DIVISOR.
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CCS A # GET ABS(DIVISOR) IN THE A REGISTER.
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AD BIT1
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TCF ZEROPLUS
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AD BIT1
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|
|
ZEROPLUS XCH SCRATCHY # STORE ABS(DIVISOR). PICK UP TOP HALF OF
|
2016-07-11 12:35:15 +00:00
|
|
|
EXTEND # DIVIDEND.
|
2016-07-07 08:47:26 +00:00
|
|
|
BZMF GOODNEG # GET -ABS(DIVIDEND)
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# Page 1493
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CS A
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GOODNEG AD SCRATCHY # ABS(DIVISOR) - ABS(DIVIDEND)
|
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EXTEND
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|
|
BZMF MAKEMAX # BRANCH IF DIVISION IS NOT PROPER.
|
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|
|
CA SCRATCHX # RE-ESTABLISH THE DIVIDEND
|
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EXTEND
|
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|
DV SCRATCHZ # QUOTIENT IN THE A, REMAINDER IN L.
|
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|
|
TC Q # RETURN TO CALLER.
|
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|
MAKEMAX CCS SCRATCHX # DETERMINE THE SIGN OF THE QUOTIENT.
|
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|
|
CCS SCRATCHZ # SCRATCHX AND SCRATCHZ ARE NON-ZERO.
|
|
|
|
|
TCF MAXPLUS
|
|
|
|
|
CCS SCRATCHZ
|
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|
|
|
CAF NEGMAX # +,- OR -,+
|
|
|
|
|
TC Q
|
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|
|
MAXPLUS CAF POSMAX # -,- OR +,+
|
|
|
|
|
TC Q
|
|
|
|
|
|
|
|
|
|
# COEFFICIENTS FOR THE JET ACCELERATION CURVE FITS
|
|
|
|
|
# THE CURVE FITS ARE OF THE FORM --
|
|
|
|
|
#
|
|
|
|
|
# 1JACC = A/(MASS + C) + B
|
|
|
|
|
#
|
|
|
|
|
# A IS SCALED AT PI/4 RAD/SEC**2 B+16KG, B IS SCALED AT PI/4 RAD/SEC**2, AND C IS SCALED AT B +16 KG.
|
|
|
|
|
#
|
|
|
|
|
# THE CURVE FIT FOR L,PVT-CG IS OF THE SAME FORM, EXCEPT THAT A IS SCALED AT 8 FT B+16 KG, B IS SCALED AT 8 FT,
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|
|
# AND C IS SCALED AT B+16 KG.
|
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|
2DEC +.0410511917 # L A DESCENT
|
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|
|
INERCONA 2DEC +.0059347674 # 1JACCP A DESCENT
|
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|
2DEC +.0014979264 # 1JACCQ A DESCENT
|
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|
2DEC +.0010451889 # 1JACCR A DESCENT
|
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|
2DEC +.0065443852 # 1JACCP A ASCENT
|
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|
2DEC +.0035784354 # 1JACCQ A ASCENT
|
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2DEC +.0056946631 # 1JACCR A ASCENT
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DEC +.155044 # L B DESCENT
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|
DEC -.025233 # L C DESCENT
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# Page 1494
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INERCONB DEC +.002989 # 1JACCP B DESCENT
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INERCONC DEC +.008721 # 1JACCP C DESCENT
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DEC +.018791 # 1JACCQ B DESCENT
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DEC -.068163 # 1JACCQ C DESCENT
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DEC +.021345 # 1JACCR B DESCENT
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DEC -.066027 # 1JACCR C DESCENT
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DEC +.000032 # 1JACCP B ASCENT
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|
DEC -.006923 # 1JACCP C ASCENT
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|
DEC +.162862 # 1JACCQ B ASCENT
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DEC +.002588 # 1JACCQ C ASCENT
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|
|
DEC +.009312 # 1JACCR B ASCENT
|
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|
DEC -.023608 # 1JACCR C ASCENT
|
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|
|
GIMBLBTS OCTAL 01400
|
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|
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OCTAL 01000
|
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|
OCTAL 06000
|
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OCTAL 04000
|
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|
|
DGBF DEC 0.6 # .3 SCALED AT 1/2
|
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|
0.35356 DEC 0.35356 # .70711 SCALED AT 2
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|
GFACTM OCT 337 # 979.24/2.20462 AT B+15
|
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|
.7071 DEC .70711
|
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-.7071 DEC -.70711
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-EPSMAX DEC -.42265
|
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# CSM-DOCKED INERTIA COMPUTATIONS
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DOCKED CA ONE # COEFTR = 1 FOR INERTIA COEFFICIENTS
|
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SPSLOOP1 TS COEFCTR # = 7 FOR CG COEFFICIENTS
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CA ONE # MASSCTR = 1 FOR CSM
|
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TS MASSCTR # = 0 FOR LEM
|
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INDEX COEFCTR
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CA COEFF -1 # COEFF -1 = C
|
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EXTEND
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MP LEMMASS
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EXTEND
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MP CSMMASS # LET X = CSMMASS AND Y = LEMMASS
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INDEX COEFCTR
|
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|
AD COEFF # COEFF = F
|
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|
TS MPAC # MPAC = C X Y + F
|
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TCF +4
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SPSLOOP2 TS MASSCTR # LOOP TWICE THROUGH HERE TO OBTAIN
|
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EXTEND # MPAC = MPAC + (A X +D)X + (B Y +E)Y
|
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DIM COEFCTR # LOOP #1 LOOP #2
|
|
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INDEX COEFCTR
|
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CA COEFF +2 # COEFF +2 = A OR B
|
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EXTEND
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# Page 1495
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INDEX MASSCTR
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MP LEMMASS
|
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INDEX COEFCTR
|
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AD COEFF +4 # COEFF +4 = E OR D
|
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EXTEND
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INDEX MASSCTR
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MP LEMMASS
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ADS MPAC
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CCS MASSCTR
|
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TCF SPSLOOP2
|
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CCS COEFCTR # IF COEFCTR IS POS, EXIT FROM LOOP WITH
|
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TCF +7 # CG X DELDOT = MPAC X 4 PI RAD-CM/SEC
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TORQCONS 2DEC 0.51443 B-14 # CORRESPONDS TO 500 LB-FT
|
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CA MPAC
|
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TS MPAC +1 # INERTIA = (MPAC +1) X 2(38) KG-CM(2)
|
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CA SEVEN
|
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TCF SPSLOOP1
|
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CA 1JACCCON # 1JACC=1JACCCON/MASS
|
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|
ZL
|
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TC DVOVSUB
|
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ADRES MASS
|
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|
TS 1JACC # SCALED AT PI/4
|
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CA POSMAX # SET INVERSE JET ACCELERATIONS TO POSMAX,
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|
TS 1/ANETP # WHICH CORRESPONDS TO ACCEL. OF 1.4 D/SS.
|
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|
TS 1/ANET2 +1
|
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|
TS 1/ANET2 +2
|
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|
TS 1/ANET2 +17D
|
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|
TS 1/ANET2 +18D
|
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|
EXTEND
|
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|
DCA TORQCONS
|
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EXTEND
|
|
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|
DV MPAC +1
|
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|
INHINT
|
|
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|
|
TS 1JACCQ # SCALED AT PI/4
|
|
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|
|
TS 1JACCR
|
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|
|
|
|
|
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|
CA -.7071
|
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|
|
TS COEFFQ # COEFFQ AND COEFFR ARE CHOSEN TO MAKE U-
|
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|
CA .7071 # AND V-AXES ORTHOGONAL FOR DOCKED CASE
|
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TS COEFFR
|
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|
CA MASS # SCALED AT 2(16) KG
|
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EXTEND
|
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|
MP MPAC # SCALED AT 4 PI RAD-CM/SEC
|
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EXTEND
|
|
|
|
|
MP ABDELV # SCALED AT 2(13) CM/SEC(2)
|
|
|
|
|
TC DVOVSUB # GET QUOTIENT WITH OVERFLOW PROTECTION
|
|
|
|
|
# Page 1496
|
|
|
|
|
ADRES MPAC +1
|
|
|
|
|
|
|
|
|
|
TS ACCDOTR
|
|
|
|
|
TCF SPSCONT # CONTINUE K, KSQ CALCULATIONS
|
|
|
|
|
|
|
|
|
|
1JACCCON OCT 00167 # SCALED AT PI/4X2(16) RAD/SEC(2)-KG
|
|
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|
# 2 2
|
|
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|
|
# COEFFICIENTS FOR CURVE FIT OF THE FORM Z = A X +B Y +C X Y +D X +E Y +F
|
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|
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|
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|
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|
COEFF DEC .19518 # C COEFFICIENT OF INERTIA
|
|
|
|
|
DEC -.00529 # F "
|
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|
|
DEC -.17670 # B "
|
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|
|
DEC -.03709 # A "
|
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|
DEC .06974 # E "
|
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|
DEC .02569 # D "
|
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|
DEC .20096 # C COEFFICIENT OF CG
|
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|
DEC .13564 # F "
|
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|
DEC .75704 # B "
|
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|
|
DEC -.37142 # A "
|
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|
|
DEC -.63117 # E "
|
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|
DEC .41179 # D "
|
|
|
|
|
|
|
|
|
|
# ASSIGNMENT OF TEMPORARIES FOR 1/ACCS (EXCLUDING 1/ACCONT)
|
|
|
|
|
# MPAC, MPAC +1, MPAC +2 USED EXPLICITLY
|
|
|
|
|
COEFCTR EQUALS MPAC +4
|
|
|
|
|
MASSCTR EQUALS MPAC +5
|
|
|
|
|
SCRATCHX EQUALS MPAC +4 # SCRATCH AREA FOR DVOVSUB ROUTINE.
|
|
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|
|
SCRATCHY EQUALS SCRATCHX +1
|
|
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|
|
SCRATCHZ EQUALS SCRATCHX +2
|
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|
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|
|
DOCKTEMP EQUALS MPAC +3 # RECORD OF CSMDOCKED BIT OF DAPBOOLS
|
|
|
|
|
EPSILON EQUALS MPAC +1
|
|
|
|
|
-EPSILON EQUALS EPSILON
|
|
|
|
|
-.1875 DEC -.18750
|
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# Page 1497
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BANK 20
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SETLOC DAPS3
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BANK
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EBANK= AOSQ
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COUNT* $$/DAPAO
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-1 TS INGTS # ZERO INGTS IN ASCENT
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1/ACCONT CA DB # INITIALIZE DBVAL1,2,3
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EXTEND
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MP BIT13
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TS L # 0.25 DB
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AD A
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TS DBVAL3 # 0.50 DB
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CS DBVAL1
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AD L
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TS DBVAL2 # -.75 DB
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GETAOSUV INHINT
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CAE AOSR # COMPUTE ASOU AND AOSV BY ROTATING
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TS L # AOSQ AND AOSR.
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CAE AOSQ
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TC IBNKCALL
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CADR ROT-TOUV
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DXCH AOSU
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RELINT
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CA DAPBOOLS
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MASK DRIFTBIT # ZERO DURING ULLAGE AND POWERED FLIGHT.
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CCS A # IF DRIFTING LIGHT,
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CA ONE # SET DRIFTER TO 1
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TS DRIFTER # SAVE TO TEST FOR DRIFTING FLIGHT LATER
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AD ALLOWGTS # NON-ZERO IF DRIFT OR GTS NEAR
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CCS A
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CA FLATVAL # DRIFTING FLIGHT, STORE .8 IN FLAT
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TS FLATEMP # IN POWERED FLIGHT, STORE ZERO IN FLAT
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EXTEND
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BZF DOPAXIS # IF POWERED AND NO GTS, START P AXIS,
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CCS DRIFTER # OTHERWISE SET ZONE3LIM
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CA ZONE3MAX # 17.5 MS, SCALED AT 4 SECONDS.
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TS Z3TEM
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DOPAXIS CA 1JACC # 1JACC AT PI/4 = 2JACC AT PI/2 =
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# ANET AT PI/2 = ANET/ACOAST AT 2(6).
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AD BIT9 # 1 + ANET/ACOAST AT 2(6)
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TS FUNTEM
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CA 1JACC
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# Page 1498
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TC INVERT
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INHINT # P AXIS DATA MUST BE CONSISTENT
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TS 1/ANETP # SCALED AT 2(7)/PI.
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TS 1/ANETP +1
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CS BIT9 # -1 AT 2(6)
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EXTEND
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MP 1/ANETP # -1/ANET AT 2(13)/PI
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EXTEND
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DV FUNTEM # -1/(ANET + ANET**2/ACOAST) AT 2(7)/PI
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TS PACCFUN
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TS PACCFUN +1
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CA 1/.03 # NO AOS FOR P AXIS, ACOAST = AMIN
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TS 1/ACOSTP
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TS 1/ACOSTP +1
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RELINT
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ZL
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CCS DRIFTER
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DXCH AOSU # ZERO AOSU,V IF IN DRIFT, JUST TO BE SURE
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UAXIS CA ZERO # DO U AXIS COMPUTATIONS
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TS UV # ZERO FOR U AXIS, ONE FOR V AXIS.
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BOTHAXES TS SIGNAOS # CODING COMMON TO U,V AXES
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INDEX UV
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CCS AOSU # PICK UP ABS(AOSU OR AOSV)
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AD ONE # RESTORE TO PROPER VALUE
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TCF +3 # AND LEAVE SIGNAOS AT ZERO
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AD ONE # NEGATIVE, RESTORE TO PROPER VALUE
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INCR SIGNAOS # AND SET SIGNAOS TO ONE TO SHOW AOS NEG
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TS ABSAOS # SAVE ABS(AOS)
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CS SIGNAOS
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TS -SIGNAOS # USED AS AN INDEX
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CA DBVAL1 # SET DB1, DB2 TO DBVAL1 (= DB)
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TS DBB1
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TS DBB2
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CA ABSAOS # TEST MAGNITUDE OF ABS(AOS)
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AD -.03R/S2
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EXTEND
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BZMF NOTMUCH # ABS(AOS) LESS THAN AMIN
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BIGAOS CCS FLATEMP # AGS(AOS) GREATER THAN AMIN
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TCF SKIPDB1 # I DRIFT OR GTS, DO NOT COMPUTE DB
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CA DBVAL1
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INDEX -SIGNAOS
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# Page 1499
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ADS DBB2 # DB2(1) = 2 DB
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INDEX SIGNAOS
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TS DBB4 # DB4(3) = 1 DB
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CA -.1875 # -.1875 PI/2 RAD/SEC(2) SCALED AT PI/2
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AD ABSAOS # ABSAOS IS SCALED AT PI/2
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EXTEND
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BZMF +3
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CS DBVAL3 # -.5 DB
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TCF DBONE
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CS ABSAOS
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DOUBLE
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DOUBLE
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AD BIT14
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DOUBLE # 1-8 ABSAOS. (8 IS 16/PI SCALED AT 2/PI)
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EXTEND
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MP DB
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DBONE INDEX SIGNAOS # DB1(2)=(1-8 ABSAOS) DB. IF ABSAOS IS
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TS DBB1 # GREATER THAN .1875 THEN DB1(2) = -.5 DB
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CA DBVAL2
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INDEX -SIGNAOS
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TS DBB3 # DB3(4) = -.75 DB
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SKIPDB1 CA ABSAOS # ABS(AOS) GREATER THAN AMIN, SO IT IS
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EXTEND
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MP BIT12
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AD ABSAOS # (9/8) ABSAOS.
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TC INVERT # ALL RIGHT TO DIVIDE
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INDEX -SIGNAOS
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TS 1/ACOSTT +1 # 1/ACOASTPOS(NET) = 1/ABS(AOS)
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CA 1/.03
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INDEX SIGNAOS
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TS 1/ACOSTT # 1/ACOASTNEG(POS) = 1/AIN
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CA ABSAOS
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AD 1JACCU
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AD 1JACCU # 2 JACC + ABS(AOS)
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AD BIT9 # MAXIMUM VALUE IN COMPUTATIONS
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TS A # TEST FOR OVERFLOW
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TCF SKIPDB2 # NO OVERFLOW, DO NORMAL COMPUTATION
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CA ABSAOS # RESCALE TO PI TO PREVENT OVERFLOW
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EXTEND
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MP BIT14
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AD 1JACCU # 1 JACC AT PI/2 = 2JACC AT PI
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TS ANET # ANETPOS(NEG) MAX SCALED AT PI =
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# ANETPOS(NEG) MAX/ACOASTNEG(POS) AT 2(7)
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AD BIT8 # 1 + ANETPOS/ACOASTNEG AT 2(7)
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XCH ANET # SAVE IN ANET, WHILE PICKING UP ANET
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TC INVERT
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EXTEND
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# Page 1500
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MP BIT14 # SCALE 1/ANET AT 2(7)/PI
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TS 1/ANET
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CA ACCHERE # SET UP RETURN FROM COMPUTATION ROUTINE
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TS ARET
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CS BIT8 # -1 AT 2(7)
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TCF DOACCFUN # FINISH ACCFUN COMPUTATION
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ACCHERE TCF ACCTHERE
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NOTMUCH TS L # ABS(AOS) LESS THAN AMIN, SAVE IN L
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CA 1/.03 # ACOASTPOS,NEG = AMIN
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TS 1/ACOSTT
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TS 1/ACOSTT +1
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CCS FLATEMP
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TCF SKIPDB2 # DO NOT COMPUTE DB IF DRIFT OR GTS
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CA .0125RS # AMIN/2
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AD L # L HAS ABS(AOS) - AMIN
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EXTEND # RESULT IS ABS(AOS)- AMIN/2
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BZMF NOAOS # ABS(AOS) LESS THAN AMIN/2
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SOMEAOS CA DBVAL3 # AMIN/2 LT ABS(AOS) LT AMIN
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INDEX -SIGNAOS
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TS DBB3 # DB3(4) = DB/2
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AD A
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INDEX SIGNAOS
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TS DBB4 # DB4(3) = DB
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TCF SKIPDB2
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NOAOS CA DBVAL1
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TS DBB3 # DB3,4 = DB
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TS DBB4
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SKIPDB2 CA ABSAOS # ANETPOS(NEG) MAX = 2 JACC + ABS(AOS)
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AD 1JACCU
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AD 1JACCU
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TS ANET # CANNOT OVERFLOW HERE
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CL1/NET+ TC DO1/NET+ # COMPUTE 1/ANET, ACCFUN
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ACCTHERE INDEX -SIGNAOS
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TS Z5TEM +2 # STORE ACCFUN IN TEMPORARY BUFFER
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CA 1/ANET
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INDEX -SIGNAOS
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TS 1/ATEM2 +2 # STORE 1/ANET IN TEMPORARY BUFFER
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CA ABSAOS # SEE IF OVERFLOW IN MIN CASE
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AD 1JACCU
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# Page 1501
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AD BIT9 # MAXIMUM POSSIBLE VALUE
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TS A # OVERFLOW POSSIBLE BUT REMOTE
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TCF +2
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CA POSMAX # IF OVERFLOW, TRUNCATE TO PI/2
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AD -.03R/S2 # RESTORE TO CORRECT VALUE
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TS ANET
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TC DO1/NET+ # COMPUTE 1/ANET, ACCFUN
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INDEX -SIGNAOS # STORE MIN VALUES JUST AS MAX VALUES
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TS Z5TEM
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CA 1/ANET
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INDEX -SIGNAOS
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TS 1/ATEM2
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CS ABSAOS # NOW DO NEG(POS) CASES
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AD 1JACCU
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AD 1JACCU # ANETNEG(POS) MAX
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TC 1/ANET- # COMPUTE 1/ANET, ACCFUN, AND ACCSW
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INDEX SIGNAOS # STORE NEG(POS) VALUES JUST AS POS(NEG)
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TS Z1TEM +2
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TS L # SAVE IN L FOR POSSIBLE FUTURE USE
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CA 1/ANET
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INDEX SIGNAOS
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TS 1/ATEM1 +2
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CS ABSAOS
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AD 1JACCU # 1/ANETNEG(POS) MIN
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TS ANET
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AD -.03R/S2 # TEST FOR AMIN
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EXTEND # IF ANET LESS THAN AMIN, STORE MAX JET
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BZMF FIXMIN # VALUES FOR MIN JETS AND SET ACCSW
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TC 1/NETMIN # OTHERWISE DO MIN JET COMPUTATIONS
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STMIN- INDEX SIGNAOS # STORE VALUES
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TS Z1TEM
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CA 1/ANET
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INDEX SIGNAOS
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TS 1/ATEM1
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INDEX UV
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CA +UMASK
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MASK CH5MASK # TEST FOR +U (+V) JET FAILURES
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EXTEND
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BZF FAIL-
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CA 1/ATEM2 # REPLACE FUNCTION VALUES DEPENDING ON THE
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TS 1/ATEM2 +2 # FAILED JET PAIR WITH CORRESPONDING ONE-
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CA Z5TEM # JET (OR AMIN) FUNCTION VALUES
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TS Z5TEM +2
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FAIL- INDEX UV
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# Page 1502
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CA -UMASK
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MASK CH5MASK # TEST FOR -U (-V) JET FAILURES
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EXTEND
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BZF DBFUN
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CA 1/ATEM1 # REPLACE FUNCTION VALUES DEPENDING ON THE
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TS 1/ATEM1 +2 # FAILED JET PAIR WITH CORRESPONDING ONE-
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CA Z1TEM # JET (OR AMIN) FUNCTION VALUES
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TS Z1TEM +2
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DBFUN CS DBB3 # COMPUTE AXISDIST
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AD DBB1
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AD FLATEMP
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TS AXDSTEM
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CS DBB4
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AD DBB2
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AD FLATEMP
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TS AXDSTEM +1
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INHINT
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CCS UV # TEST FOR U OR V AXIS
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TCF STORV # V AXIS STORE V VALUES
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CA ACCSW # U AXIS STORE U VALUES
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TS ACCSWU
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CA NINE # TRANSFER 10 WORDS VIA GENTRAN
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TC GENTRAN +1
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ADRES 1/ATEM1 # TEMPORARY BUFFER
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ADRES 1/ANET1 # THE REAL PLACE
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RELINT
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DXCH DBB1 # SAVE U DBS FOR LATER STORING
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DXCH UDB1
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DXCH DBB4
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DXCH UDB4
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DXCH AXDSTEM
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DXCH UAXDIST
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CA ONE # NOW DO V AXIS
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TS UV
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CA ZERO
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TCF BOTHAXES # AND DO IT AGAIN
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STORV CA ACCSW # STORE V AXIS VALUES
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TS ACCSWV
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CA NINE
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TC GENTRAN +1
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# Page 1503
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ADRES 1/ATEM1 # TEMPORARY BUFFER
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ADRES 1/ANET1 +16D # THE REAL PLACE
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# NOW STORE DEADBANDS FOR ALL AXES
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DXCH FLATEMP # FLAT AND ZONE3LIM
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DXCH FLAT
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CA DBVAL1 # COMPUTE P AXIS DEADBANDS
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TS PDB1
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TS PDB2
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AD FLAT
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TS PDB3
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TS PDB4
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CA ZERO
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TS PAXDIST
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TS PAXDIST +1
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CCS FLAT
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TCF DRFDB # DRIFT OR GTS -- COMPUTE DBS
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DXCH UDB1 # STORE U DEADBANDS
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DXCH FIREDB # CANNOT USE GENTRAN BECAUSE OF RELINT
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DXCH UDB4
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DXCH COASTDB
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DXCH UAXDIST
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DXCH AXISDIST
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DXCH DBB1 # STORE V AXIS DEADBANDS
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DXCH FIREDB +16D # COULD USE GENTRAN IF DESIRED
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DXCH DBB4
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DXCH COASTDB +16D
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DXCH AXDSTEM
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DXCH AXISDIST +16D
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TCF 1/ACCRET +1 # ALL DONE
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DRFDB CA DBVAL1 # DRIFT DEADBANDS
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TS FIREDB
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TS FIREDB +1
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TS FIREDB +16D
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TS FIREDB +17D
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AD FLAT
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TS COASTDB
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TS COASTDB +1
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TS COASTDB +16D
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TS COASTDB +17D
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CA ZERO
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TS AXISDIST
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TS AXISDIST +1
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TS AXISDIST +16D
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TS AXISDIST +17D
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# Page 1504
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1/ACCRET INHINT
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CS DAPBOOLS # SET BIT TO INDICATE DATA GOOD.
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MASK ACCSOKAY
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ADS DAPBOOLS
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RELINT
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CA ACCRETRN
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TC BANKJUMP # RETURN TO CALLER
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INVERT TS HOLD # ROUTINE TO INVERT -INPUT AT PI/2
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CA BIT9 # 1 AT 2(6)
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ZL # ZERO L FOR ACCURACY AND TO PREVENT OVFLO
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EXTEND
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DV HOLD
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TC Q # RESULT AT 2(7)/PI
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DOWNGTS CAF ZERO # ZERO SWITCHES WHEN USEQRJTS BIT IS UP
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TS ALLOWGTS # OR DAP IS OFF
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TS INGTS
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TCF DOCKTEST
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1/ANET- ZL
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LXCH ACCSW # ZERO ACCSW
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TS ANET # SAVE ANET
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AD -.03R/S2 # TEST FOR MIN VALUE
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EXTEND
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BZMF NETNEG # ANET LESS THAN AMIN, SO FAKE IT
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1/NETMIN CA ANET
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EXTEND
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INDEX -SIGNAOS
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MP 1/ACOSTT +1 # ANETNEG(POS)/ACOASTPOS(NEG) AT 2(6)
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# THE FOLLOWING CODING IS VALID FOR BOTH POS OR NEG
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# VALUES OF AOS
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DO1/NET+ AD BIT9 # 1 + ANET/ACOAST AT 2(6)
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XCH ANET # SAVE AND PICK UP ANET
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EXTEND
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QXCH ARET # SAVE RETURN
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TC INVERT
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|
TS 1/ANET # 1/ANET AT 2(7)/PI
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CS BIT9 # -1 AT 2(6)
|
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|
DOACCFUN EXTEND
|
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|
MP 1/ANET # -1/ANET AT 2(13)/PI
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|
EXTEND
|
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|
DV ANET # ACCFUN AT 2(7)/PI
|
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|
TC ARET # RETURN
|
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|
NETNEG CS -.03R/S2 # ANET LESS THAN AMIN -- SET EQUAL TO AMIN
|
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|
TS ANET
|
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|
# Page 1505
|
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|
|
TCF 1/NETMIN +1 # CONTINUE AS IF NOTHING HAPPENED.
|
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|
|
|
|
|
FIXMIN CCS SIGNAOS
|
|
|
|
|
CA TWO # IF AOS NEG, ACCSW = +1
|
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|
|
AD NEGONE # IF AOS POS, ACCSW = -1
|
|
|
|
|
TS ACCSW
|
|
|
|
|
AD UV # IF ACCSW = +1, TEST FOR +U (+V) JET FAIL
|
|
|
|
|
INDEX A # IF ACCSW = -1, TEST FOR -U (-V) JET FAIL
|
|
|
|
|
CA -UMASK +1
|
|
|
|
|
MASK CH5MASK
|
|
|
|
|
EXTEND
|
|
|
|
|
BZF +4
|
|
|
|
|
CS -.03R/S2 # JET FAILURE -- CANNOT USE 2-JET VALUES
|
|
|
|
|
TS ANET # ANET = AMIN
|
|
|
|
|
TCF STMIN- -1 # CALCULATE FUNCTIONS USING AMIN
|
|
|
|
|
CA L # L HAS ACCFUN
|
|
|
|
|
TCF STMIN- # STORE MAX VALUES FOR MIN JETS
|
|
|
|
|
|
|
|
|
|
# ERASABLE ASSIGNMENTS FOR 1/ACCONT
|
|
|
|
|
|
|
|
|
|
1/ANETP EQUALS BLOCKTOP +2
|
|
|
|
|
1/ACOSTP EQUALS BLOCKTOP +4
|
|
|
|
|
PACCFUN EQUALS BLOCKTOP +8D
|
|
|
|
|
PDB1 EQUALS BLOCKTOP +10D
|
|
|
|
|
PDB2 EQUALS BLOCKTOP +11D
|
|
|
|
|
PDB4 EQUALS BLOCKTOP +12D
|
|
|
|
|
PDB3 EQUALS BLOCKTOP +13D
|
|
|
|
|
PAXDIST EQUALS BLOCKTOP +14D
|
|
|
|
|
|
|
|
|
|
ACCSW EQUALS VBUF # EXECUTIVE TEMPORARIES
|
|
|
|
|
# CANNOT DO CCS NEWJOB DURING 1/ACCS
|
|
|
|
|
1/ATEM1 EQUALS ACCSW +1 # TEMP BUFFER FOR U AND V AXES
|
|
|
|
|
1/ATEM2 EQUALS 1/ATEM1 +1
|
|
|
|
|
1/ACOSTT EQUALS 1/ATEM1 +4
|
|
|
|
|
Z1TEM EQUALS 1/ATEM1 +6
|
|
|
|
|
Z5TEM EQUALS 1/ATEM1 +7
|
|
|
|
|
|
|
|
|
|
UDB1 EQUALS 1/ATEM1 +10D # UAXIS DEADBAND BUFFER
|
|
|
|
|
UDB2 EQUALS 1/ATEM1 +11D
|
|
|
|
|
UDB4 EQUALS 1/ATEM1 +12D
|
|
|
|
|
UDB3 EQUALS 1/ATEM1 +13D
|
|
|
|
|
UAXDIST EQUALS 1/ATEM1 +14D
|
|
|
|
|
|
|
|
|
|
DBB1 EQUALS 1/ATEM1 +16D # TEMP DEADBAND BUFFER, ALSO V AXIS
|
|
|
|
|
DBB2 EQUALS 1/ATEM1 +17D
|
|
|
|
|
DBB4 EQUALS 1/ATEM1 +18D
|
|
|
|
|
DBB3 EQUALS 1/ATEM1 +19D
|
|
|
|
|
AXDSTEM EQUALS 1/ATEM1 +20D
|
|
|
|
|
|
|
|
|
|
# Page 1506
|
|
|
|
|
FLATEMP EQUALS 1/ATEM1 +22D
|
|
|
|
|
Z3TEM EQUALS 1/ATEM1 +23D # MUST FOLLOW FLATEMP
|
|
|
|
|
|
|
|
|
|
DBVAL1 EQUALS DB
|
|
|
|
|
DBVAL2 EQUALS INTB15+
|
|
|
|
|
DBVAL3 EQUALS INTB15+ +1
|
|
|
|
|
|
|
|
|
|
DRIFTER EQUALS INTB15+ +2
|
|
|
|
|
|
|
|
|
|
UV EQUALS MPAC
|
|
|
|
|
ANET EQUALS MPAC +3
|
|
|
|
|
FUNTEM EQUALS MPAC +3
|
|
|
|
|
1/ANET EQUALS MPAC +4
|
|
|
|
|
ARET EQUALS MPAC +5
|
|
|
|
|
ABSAOS EQUALS MPAC +6
|
|
|
|
|
SIGNAOS EQUALS MPAC +7
|
|
|
|
|
-SIGNAOS EQUALS MPAC +8D
|
|
|
|
|
HOLD EQUALS MPAC +9D
|
|
|
|
|
ACCRETRN EQUALS FIXLOC -1
|
|
|
|
|
|
|
|
|
|
ZONE3MAX DEC .004375 # 17.5 MS (35 MS FOR 1 JET) AT 4 SECONDS
|
|
|
|
|
FLATVAL DEC .01778 # .8 AT PI/4 RAD
|
|
|
|
|
-.03R/S2 OCT 77377 # -PI/2(7) AT PI/2
|
|
|
|
|
|
|
|
|
|
.0125RS EQUALS BIT8 # PI/2(+8) AT PI/2
|
|
|
|
|
1/.03 EQUALS POSMAX # 2(7)/PI AT 2(7)/PI
|
|
|
|
|
|
|
|
|
|
PAXISADR GENADR PAXIS
|
|
|
|
|
|
|
|
|
|
# THE FOLLOWING 4 CONSTANTS ARE JET
|
|
|
|
|
# FAILURE MASKS AND ARE INDEXED
|
|
|
|
|
-UMASK OCT 00110 # -U
|
|
|
|
|
OCT 00022 # -V
|
|
|
|
|
+UMASK OCT 00204 # +U
|
|
|
|
|
OCT 00041 # +V
|
|
|
|
|
|
