SevenOfAces/Apollo-Guidance-Computer
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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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12
Luminary099/AOSTASK_AND_AOSJOB.agc
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@ -31,7 +31,7 @@
# Page 1485
# PROGRAM NAME: 1/ACCS
# 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:
# 1/ACCS PROVIDES THE INTERFACE BETWEEN THE GUIDANCE PROGRAMS AND THE DIGITAL AUTOPILOT. WHENEVER THERE IS A
@ -40,7 +40,7 @@
#
# 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,
# 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
# FORMED BY RESOLVING 1JACCQ AND 1JACCR. IN THE DESCENT CASE, THE DESCENT ENGINE MOMENT ARM (L, PVT-CG) IS ALSO
@ -65,9 +65,9 @@
#
# 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:
# 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.
CA DAPBOOLS # IS THE CSM DOCKED
CA DAPBOOLS # IS CSM DOCKED
MASK CSMDOCKD
TS DOCKTEMP # STORE RECORD OF STATE IN TEMP (MPAC +3).
CCS A
@ -117,7 +117,7 @@
TS LEMMASS
# 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
# ENSURE THAT THE LEM MASS VALUE IS WITHIN THE ACCEPTABLE RANGE