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fixed typos

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proof read page 1485 through 1488
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Adhiraj 2021-10-02 20:59:10 +05:30 committed by GitHub
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20
Luminary099/AOSTASK_AND_AOSJOB.agc
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@ -31,23 +31,23 @@
# Page 1485 # Page 1485
# PROGRAM NAME: 1/ACCS # PROGRAM NAME: 1/ACCS
# PROGRAM WRITTEN BY: BOB COVELLI AND MIKE HOUSTON # PROGRAM WRITTEN BY: BOB COVELLI AND MIKE HOUSTON
# LAST MODIFICATION: FEB. 14, 1969 BY G. KALAN # *LAST MODIFICATION: FEB. 14, 1969 BY G. KALAN
# #
# PROGRAM DESCRIPTION: # PROGRAM DESCRIPTION:
# 1/ACCS PROVIDES THE INTERFACE BETWEEN THE GUIDANCE PROGRAMS AND THE DIGITAL AUTOPILOT. WHENEVER THERE IS A # 1/ACCS PROVIDES THE INTERFACE BETWEEN THE GUIDANCE PROGRAMS AND THE DIGITAL AUTOPILOT. WHENEVER THERE IS A
# CHANGE IN THE MASS OF THE VEHICLE, IN THE DEADBAND SELECTED, IN THE VEHICLE CONFIGURATION (ASCENT-DESCENT- # CHANGE IN THE MASS OF THE VEHICLE, IN THE DEADBAND SELECTED, IN THE VEHICLE CONFIGURATION (ASCENT-DESCENT-
# DOCKED), AND DURING A FRESH START OR A RESTART, 1/ACCS IS CALLED TO COMMUNICATE THE DATA CHANGES TO THE DAP. # DOCKED), AND DURING A FRESH START OR A RESTART, 1/ACCS IS CALLED TO COMMUNICATE THE DATA CHANGES TO THE DAP.
# #
# THE INPUTS TO 1/ACCS ARE MASS, ACCELERATION (ABDELV), DEADBAND (DB), OFFSET ACCELERATIONS (AOSQ AND AOSR), # THE INPUTS TO 1/ACCS ARE MASS, ACCELERATION (ABDELV), DEADBAND (DB), OFFSET ACCELERATIONS (AOSQ AND AOSR),
# STAGE VERIFY BIT (CHAN30, BIT2), DOCKED BIT (DAPBOOLS, BIT13), DRIFT BIT (DAPBOOLS, BIT8), USEQRJTS (DAPBOOLS, # STAGE VERIFY BIT (CHAN30, BIT2), DOCKED BIT (DAPBOOLS, BIT13), DRIFT BIT (DAPBOOLS, BIT8), USEQRJTS (DAPBOOLS,
# BIT14), AND SURFACE FLAG (FLAGWRDB, BIT8), AND CH5MASK. # BIT14), AND SURFACE FLAG (FLAGWRD8, BIT8), AND CH5MASK.
# #
# 1/ACCS COMPUTES THE JET ACCELERATIONS (1JACC, 1JACCQ, 1JACCR) AS FUNCTIONS OF MASS. 1JACCU AND 1JACCV ARE # 1/ACCS COMPUTES THE JET ACCELERATIONS (1JACC, 1JACCQ, 1JACCR) AS FUNCTIONS OF MASS. 1JACCU AND 1JACCV ARE
# FORMED BY RESOLVING 1JACCQ AND 1JACCR. IN THE DESCENT CASE, THE DESCENT ENGINE MOMENT ARM (L, PVT-CG) IS ALSO # FORMED BY RESOLVING 1JACCQ AND 1JACCR. IN THE DESCENT CASE, THE DESCENT ENGINE MOMENT ARM (L, PVT-CG) IS ALSO
# COMPUTED AS A FUNCTION OF MASS. THE RATE OF CHANGE OF ACCELERATION DUE TO ROTATION OF THE GIMBAL (ACCDOTQ, # COMPUTED AS A FUNCTION OF MASS. THE RATE OF CHANGE OF ACCELERATION DUE TO ROTATION OF THE GIMBAL (ACCDOTQ,
# ACCDOTR) IS ALSO COMPUTED IN THE DESCENT CASE. # ACCDOTR) IS ALSO COMPUTED IN THE DESCENT CASE.
# #
# AFTER THE ABOVE COMPUTATIONS, THE PROGRAM 1/ACCONT COMPUTES THE RECIPROCAL NET ACCELERATIONS ABOUT THE P, U, # AFTER THE ABOVE COMPUTATIONS, THE PROGRAM 1/ACCONT COMPUTES THE RECIPROCAL NET ACCELERATIONS ABOUT THE P, U,
# AND V AXES (2 JETS FOR P-AXIS, BOTH 1 AND 2 JETS FOR U AND V AXES), AND THE RECIPROCAL COAST ACCELERATIONS ABOUT # AND V AXES (2 JETS FOR P-AXIS, BOTH 1 AND 2 JETS FOR U AND V AXES), AND THE RECIPROCAL COAST ACCELERATIONS ABOUT
# THE P, U, AND V AXES. THE ACCELERATION FUNCTIONS (ACCFCTZ1 AND ACCFCTZ5) ARE ALSO COMPUTED FOR THESE AXES. THE # THE P, U, AND V AXES. THE ACCELERATION FUNCTIONS (ACCFCTZ1 AND ACCFCTZ5) ARE ALSO COMPUTED FOR THESE AXES. THE
# FIRE AND COAST DEADBANDS AND AXISDIST ARE COMPUTED FOR EACH AXIS. FLAT AND ZONE3LIM, THE WIDTH AND HEIGHT OF THE # FIRE AND COAST DEADBANDS AND AXISDIST ARE COMPUTED FOR EACH AXIS. FLAT AND ZONE3LIM, THE WIDTH AND HEIGHT OF THE
@ -65,9 +65,9 @@
# #
# NORMAL EXIT: VIA BANKJUMP # NORMAL EXIT: VIA BANKJUMP
# #
# ALARM AND EXIT MODES: NONE # ALARM AND EXIT MODES: NONE.
# #
# INPUT/OUTPUT: SEE PROGRAM DESCRIPTION. # INPUT/OUTPUT: SEE PROGRAM DESCRIPTION
# #
# DEBRIS: # DEBRIS:
# ALL OF THE EXECUTIVE TEMPORARY REGISTERS, EXCEPT FIXLOC AND OVFIND, AND THE CORE SET AREA FROM MPAC TO BANKSET. # ALL OF THE EXECUTIVE TEMPORARY REGISTERS, EXCEPT FIXLOC AND OVFIND, AND THE CORE SET AREA FROM MPAC TO BANKSET.
@ -108,7 +108,7 @@
# DETERMINE MASS OF THE LEM. # DETERMINE MASS OF THE LEM.
CA DAPBOOLS # IS THE CSM DOCKED CA DAPBOOLS # IS CSM DOCKED
MASK CSMDOCKD MASK CSMDOCKD
TS DOCKTEMP # STORE RECORD OF STATE IN TEMP (MPAC +3). TS DOCKTEMP # STORE RECORD OF STATE IN TEMP (MPAC +3).
CCS A CCS A
@ -117,7 +117,7 @@
TS LEMMASS TS LEMMASS
# ON THE BASIS OF APSFLAG: # ON THE BASIS OF APSFLAG:
# SET THE P-AXIS RATE COMMAND LIMIT FOR 2-JET/2-JET CONTROL # SET THE P-AXIS RATE COMMAND LIMIT FOR 2-JET/4-JET CONTROL
# SET MPAC, WHICH INDICATES THE PROPER SET OF COEFFICIENTS FOR THE LEM-ALONE F(MASS) CALCULATIONS # SET MPAC, WHICH INDICATES THE PROPER SET OF COEFFICIENTS FOR THE LEM-ALONE F(MASS) CALCULATIONS
# ENSURE THAT THE LEM MASS VALUE IS WITHIN THE ACCEPTABLE RANGE # ENSURE THAT THE LEM MASS VALUE IS WITHIN THE ACCEPTABLE RANGE