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Readd some typos based on the original scans

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This commit is contained in:
James Harris
2016-07-12 18:52:11 -05:00
committed by oldmud0
parent afa13e7364
commit 2f62a05a56
37 changed files with 54 additions and 55 deletions
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2
Luminary099/ASCENT_GUIDANCE.s
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@ -357,7 +357,7 @@ ASCTERM EXIT
CALL
FINDCDUW -2
ASCTERM1 EXIT
+1 CA FLAGWRD9 # ENSURE THAT THE NOUN 63 DISPLAY IS
+1 CA FLAGWRD9 # INSURE THAT THE NOUN 63 DISPLAY IS
MASK FLRCSBIT # BYPASSED IF WE ARE IN THE RCS TRIMMING
CCS A # MODE OF OPERATION
TCF ASCTERM3

2
Luminary099/BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s
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@ -55,7 +55,7 @@
# BETWEEN THE PRE-IGNITION TIME CHECK -- ARE WE WITHIN 45 SECONDS OF TIG? -- AND TIG + 26 SECONDS, WHEN DPS
# PROGRAMS THROTTLE UP.
#
# VARIATIONS AMONG PROGRAMS ARE ACCOMMODATED BY MEANS OF TABLES CONTAINING CONSTANTS (FOR AVEGEXIT, FOR
# VARIATIONS AMONG PROGRAMS ARE ACCOMODATED BY MEANS OF TABLES CONTAINING CONSTANTS (FOR AVEGEXIT, FOR
# WAITLIST, FOR PINBALL) AND TCF INSTRUCTIONS. USERS PLACE THE ADRES OF THE HEAD OF THE APPROPRIATE TABLE
# (OF P61TABLE FOR P61LM, FOR EXAMPLE) IN ERASABLE REGISTER `WHICH' (E4). THE IGNITION ROUTINE THEN INDEXES BY
# WHICH TO OBTAIN OR EXECUTE THE PROPER TABLE ENTRY. THE IGNITION ROUTINE IS INITIATED BY A TCF BURNBABY,

2
Luminary099/DAPIDLER_PROGRAM.s
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@ -154,7 +154,7 @@ CALLGMBL EQUALS BIT5 # RCSFLAGS INITIALIZATION.
TS NEXTU
TS NEXTV
CS TEN
TS DAPZRUPT # TASK NOT IN PROGRESS, INITIALIZE NEG.
TS DAPZRUPT # JASK NOT IN PROGRESS, INITIALIZE NEG.
CA TWO
TS NPTRAPS
TS NQTRAPS

2
Luminary099/FLAGWORD_ASSIGNMENTS.s
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@ -365,7 +365,7 @@ TRACKBIT = BIT5
# BIT 3 FLAG 1 (S)
SLOPESW = 027D # ITERATE WITH BIAS ITERATE WITH REGULAR
# METHOD IN ITERATOR FALSE METHOD IN
# METHOD IN ITERATOR FALSI METHOD IN
SLOPEBIT = BIT3 # ITERATOR
# BIT 2 FLAG 1 (S)

2
Luminary099/INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.s
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@ -72,7 +72,7 @@
# CHANNEL 12 CHAN12: OUTPUT CHANNEL; BITS USED TO DRIVE NAVIGATION AND SPACECRAFT HARDWARE.
#
# BIT 1 ZERO RR CDU; CDU'S GIVE RADAR INFORMATION FOR LM
# BIT 1 ZERO RR CDU; CDU'S GIVE RRADAR INFORMATION FOR LM
# BIT 2 ENABLE CDU RADAR ERROR COUNTERS
# BIT 3 NOT USED
# BIT 4 COARSE ALIGN ENABLE OF IMU

2
Luminary099/LAMBERT_AIMPOINT_GUIDANCE.s
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@ -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.

2
Luminary099/LEM_GEOMETRY.s
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@ -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

2
Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s
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@ -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:

2
Luminary099/P-AXIS_RCS_AUTOPILOT.s
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@ -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

2
Luminary099/P12.s
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@ -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

4
Luminary099/P32-P35_P72-P75.s
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@ -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.
#

4
Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s
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@ -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

2
Luminary099/RADAR_LEADIN_ROUTINES.s
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@ -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.

2
Luminary099/RTB_OP_CODES.s
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@ -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

2
Luminary099/THROTTLE_CONTROL_ROUTINES.s
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@ -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/