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Fixed typos

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This commit is contained in:
Andrew Murray
2016-07-08 20:45:31 +10:00
committed by oldmud0
parent f0075c9e0c
commit 6088e4655e
52 changed files with 88 additions and 88 deletions
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2
Luminary099/AOTMARK.s
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@ -243,7 +243,7 @@ OANB SETPD STQ
GOTO
GCTR
# Page 250
# SURFSTAR COMPUTES A STAR VECTOR IN SM COORDINAGES FOR LUNAR
# SURFSTAR COMPUTES A STAR VECTOR IN SM COORDINATES FOR LUNAR
# SURFACE ALIGNMENT AND EXITS TO AVEIT TO AVERAGE STAR VECTORS.
#
# GIVEN X-MARK PLANE 1/4 VEC IN NB AT 18D OF LOCAL VAC

2
Luminary099/BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s
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@ -890,7 +890,7 @@ REP40ALM CAF V05N09 # (14)
TCF +2 # PROCEED CHECK FOR P42
TCF REP40ALM # V32E REDISPLAY ALARM
INDEX WHICH # FOR P42, ALLOW CREW TO PRECEED EVEN
INDEX WHICH # FOR P42, ALLOW CREW TO PROCEED EVEN
TCF 14 # THOUGH VEHICLE IS UNSTAGED.
# ********************************

4
Luminary099/DOWN_TELEMETRY_PROGRAM.s
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@ -115,7 +115,7 @@
# SAME AS ECADR, BUT USED WHEN THE WORD ADDRESSED IS THE LEFT
# HALF OF A DOUBLE-PRECISION WORD FOR DOWN TELEMETRY.
# B. 2DNADR - 6DNADR N-WORD DOWNLIST ADDRESS, N = 2 - 6.
# SAME AS 1DNADR, BUT WTIH THE 4 UNUSED BITS OF THE ECADR FORMAT
# SAME AS 1DNADR, BUT WITH THE 4 UNUSED BITS OF THE ECADR FORMAT
# FILLED IN WITH 0001-0101. USED TO POINT TO A LIST OF N DOUBLE-
# PRECISION WORDS, STORED CONSECUTIVELY, FOR DOWN TELEMETRY.
# C. DNCHAN DOWNLIST CHANNEL ADDRESS.
@ -339,7 +339,7 @@ SUBLIST EQUALS DNQ
# AFTER KEYING IN V74E THE CURRENT DOWNLIST WILL BE IMMEDIATELY TERMINATED AND THE DOWNLINK ERASABLE DUMP
# WILL BEGIN.
#
# ONCE INITITIATED THE DOWNLINK ERASABLE DUMP CAN BE TERMINATED (AND INTERRUPTED DOWNLIST REINSTATED) ONLY
# ONCE INITIATED THE DOWNLINK ERASABLE DUMP CAN BE TERMINATED (AND INTERRUPTED DOWNLIST REINSTATED) ONLY
# BY THE FOLLOWING:
#
# 1. A FRESH START

2
Luminary099/FINDCDUW--GUIDAP_INTERFACE.s
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@ -289,7 +289,7 @@ DELGMBLP TS TEM2
TS CPHI # OUTPUTS TO NOUN22
EXTEND
INDEX TEM2
MSU CDUXD # NO MATTER THAT THESE SLIGHLTY DIFFERENT
MSU CDUXD # NO MATTER THAT THESE SLIGHTLY DIFFERENT
COM # FROM WHEN WE INITIALLY FETCHED THEM
INDEX TEM2
TS -DELGMB # -UNLIMITED GIMBAL ANGLE CHGS, 1'S, PI

2
Luminary099/IMU_PERFORMANCE_TESTS_4.s
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@ -32,7 +32,7 @@
# BY -- GEORGE SCHMIDT IL7-146 EXT 1126
# MOD NO-ZERO
#
# FUNCITONAL DESCRIPTION
# FUNCTIONAL DESCRIPTION
#
# THIS SECTION CONSISTS OF THE FILTER FOR THE GYRO DRIFT TESTS. NO COMPASS
# IS DONE IN LEM. FOR A DESCRIPTION OF THE FILTER SEE E-1973. THIS

8
Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s
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@ -415,7 +415,7 @@ REDES1 DLOAD DSU
# VELOCITY RELATIVE TO THE SURFACE
# _______ _ _ __
# ANGTERM = V + R * WM
# STATE IN GUIDANCE COORDINTES:
# STATE IN GUIDANCE COORDINATES:
# ___ * _ ____
# RGU = CG (R - LAND)
# ___ * _ __ _
@ -1257,11 +1257,11 @@ DESCBITS MASK BIT7 # COME HERE FROM MARKRUPT CODING WITH BIT
#
# PRECAUTION: ROOTPSRS MAKES NO CHECKS FOR OVERFLOW OR FOR IMPROPER USAGE. IMPROPER USAGE COULD
# PRECLUDE CONVERGENCE OR REQUIRE EXCESSIVE ITERATIONS. AS A SPECIFIC EXAMPLE, ROOTPSRS FORMS A DERIVATIVE
# COEFFICIENT TABLE BY MULTIPLYINE EACH A(I) BY I, WHERE I RANGES FROM 1 TO N. IF AN ELEMENT OF THE DERIVATIVE
# COEFFICIENT TABLE = 1 OR >1 IN MAGNITUDE, ONLY THE EXCESS IS RETAINED. ROOTPSRS MAY CONVERGE ON THE COREECT
# COEFFICIENT TABLE BY MULTIPLYING EACH A(I) BY I, WHERE I RANGES FROM 1 TO N. IF AN ELEMENT OF THE DERIVATIVE
# COEFFICIENT TABLE = 1 OR >1 IN MAGNITUDE, ONLY THE EXCESS IS RETAINED. ROOTPSRS MAY CONVERGE ON THE CORRECT
# ROOT NONETHELESS, BUT IT MAY TAKE AN EXCESSIVE NUMBER OF ITERATIONS. THEREFORE THE USER SHOULD RECOGNIZE:
# 1. USER'S RESPONSIBILITY TO ASSUR THAT I X A(I) < 1 IN MAGNITUDE FOR ALL I.
# 2. USER'S RESPONSIBILITY TO ASSURE OVERFLOW WILL NOT OCCUR IN EVALUTATING EITHER THE RESIDUAL OR THE DERIVATIVE
# 2. USER'S RESPONSIBILITY TO ASSURE OVERFLOW WILL NOT OCCUR IN EVALUATING EITHER THE RESIDUAL OR THE DERIVATIVE
# POWER SERIES. THIS OVERFLOW WOULD BE PRODUCED BY SUBROUTINE POWRSERS, CALLED BY ROOTPSRS, AND MIGHT NOT
# PRECLUDE EVENTUAL CONVERGENCE.
# 3. AT PRESENT, ERASABLE LOCATIONS ARE RESERVED ONLY FOR N UP TO 5. AN N IN EXCESS OF 5 WILL PRODUCE CHAOS.

2
Luminary099/P-AXIS_RCS_AUTOPILOT.s
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@ -964,7 +964,7 @@ HEADTJET CA ZERO
-FOURDEG DEC -.08888
# Page 1440
# JET POLICY CONTSTRUCTION SUBROUTINE
# JET POLICY CONSTRUCTION SUBROUTINE
#
# INPUT: ROTINDEX, NUMBERT
#

2
Luminary099/P30_P37.s
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@ -90,7 +90,7 @@ V06N33 VN 0633
V06N42 VN 0642
# Page 616
# PROGRAM DESCRPTION S30.1 DATE 9NOV66
# PROGRAM DESCRIPTION S30.1 DATE 9NOV66
# MOD NO 1 LOG SECTION P30,P37
# MOD BY RAMA AIYAWAR **
#

2
Luminary099/P32-P35_P72-P75.s
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@ -34,7 +34,7 @@
#
# PURPOSE
# (1) TO CALCULATE PARAMETERS ASSOCIATED WTIH THE TIME FOLLOWING
# (1) TO CALCULATE PARAMETERS ASSOCIATED WITH THE TIME FOLLOWING
# CONCENTRIC FLIGHT PLAN MANEUVERS -- THE CO-ELLIPTIC SEQUENCE
# INITIATION (CSI) MANEUVER AND THE CONSTANT DELTA ALTITUDE
# (CDH) MANEUVER.

2
Luminary099/P70-P71.s
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@ -236,7 +236,7 @@ GOABORT TC INTPRET
TC DOWNFLAG
ADRES IDLEFLAG
TC UPFLAG # INSURE 4-JET TRANSLATION CAPABILIITY.
TC UPFLAG # INSURE 4-JET TRANSLATION CAPABILITY.
ADRES ACC4-2FL
TC CHECKMM

6
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 INERFACE ERROR
AD DELQEROR # KALCMANU INTERFACE 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 INERFACE ERROR
AD DELREROR # KALCMANU INTERFACE ERROR
AD E
XCH RERROR # SAVE R-ERROR FOR EIGHT-BALL DISPLAY.
TC Q
@ -538,7 +538,7 @@ TJLAW CA TJLAWADR
CADR SPSRCS # DETERMINE RCS CONTROL
RELINT
CAF FOUR # ALWAYS CALL FOR 2-JET CONTROL ABOUT U,V.
TS NUMBERT # FALL THROUGH TO JET SLECTION, ETC.
TS NUMBERT # FALL THROUGH TO JET SELECTION, ETC.
# Q,R-JET-SELECTION-LOGIC
#

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 UNCORRECT AND IN MSU.
INDEX A # OVERFLOW INCORRECT AND IN MSU.
CAF LIMITS
ADS MPAC
TC Q

2
Luminary099/SERVICER.s
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@ -1067,7 +1067,7 @@ MUNRVG VLOAD VXSC
R1S
VXV VSL2
WM
STODL DELVS # LUNAR ROTATION CORRECTON TERM*2(5) M/CS.
STODL DELVS # LUNAR ROTATION CORRECTION TERM*2(5) M/CS.
36D
DSU
/LAND/

2
Luminary099/THE_LUNAR_LANDING.s
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@ -126,7 +126,7 @@ IGNALOOP DLOAD
# 10
# 2 (VGU - 16 VGU KIGNX/B4)
# 2 0
# Page 787 new page is actually one line earlier but this would put the indices on a seperate line
# Page 787 new page is actually one line earlier but this would put the indices on a separate line
# disconnected from their respective variables
# THE NUMERATOR IS SCALED IN METERS AT 2(28). THE DENOMINATOR IS A VELOCITY IN UNITS OF 2(10) M/CS.
# THE QUOTIENT IS THUS A TIME IN UNITS OF 2(18) CENTISECONDS. THE FINAL SHIFT RESCALES TO UNITS OF 2(28) CS.

2
Luminary099/THROTTLE_CONTROL_ROUTINES.s
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@ -131,7 +131,7 @@ DOIT CA PIF
CA TIME1
TS TTHROT
# SINCE /AF/ IS NOT AN INSTANTANEOUS ACELERATION, BUT RATHER AN "AVERAGE" OF THE ACCELERATION LEVELS DURING
# SINCE /AF/ IS NOT AN INSTANTANEOUS ACCELERATION, BUT RATHER AN "AVERAGE" OF THE ACCELERATION LEVELS DURING
# 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
#

2
Luminary099/TJET_LAW.s
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@ -31,7 +31,7 @@
# Page 1460
# PROGRAM DESCRIPTION
# DESIGNED BY: R. D. GOSS AND P. S. WEISSMAN
# CODED BY: P. S. WEISSMAN, 28 FEBRURARY 1968
# CODED BY: P. S. WEISSMAN, 28 FEBRUARY 1968
#
# TJETLAW IS CALLED AS A SUBROUTINE WHEN THE LEM IS NOT DOCKED AND THE AUTOPILOT IS IN THE AUTOMATIC OR
# ATTITUDE-HOLD MODE TO CALCULATE THE JET-FIRING-TIME (TJET) REQUIRED FOR THE AXIS INDICATED BY AXISCTR:

2
Luminary099/TRIM_GIMBAL_CNTROL_SYSTEM.s
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@ -603,7 +603,7 @@ GMBLBITB OCTAL 06000 # INDEXED WRT GMBLBITA DO NOT MOVE *******
# SUBROUTINE ROOTCYCL: BY CRAIG WORK, 3 APRIL 68
#
# ROOTCYCL IS A SUBROUTINE WHICH EXECUTS ONE NEWTON SQUARE ALGORITHM ITERATION. THE INITIAL GUESS AT THE
# ROOTCYCL IS A SUBROUTINE WHICH EXECUTES ONE NEWTON SQUARE ALGORITHM ITERATION. THE INITIAL GUESS AT THE
# SQUARE ROOT IS PRESUMED TO BE IN THE A REGISTER AND ONE-HALF THE SQUARE IS TAKEN FROM HALFARG. THE NEW APPROXIMATION
# TO THE SQUARE ROOT IS RETURNED IN THE A REGISTER. DEBRIS: A, L, SR, SCRATCH. ROOTCYCL IS CALLED FROM
# LOCATION (LOC) BY A TC ROOTCYCL, AND RETURNS (TC Q) TO LOC +1.