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Fix all the typos! (and add some too)

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This commit is contained in:
oldmud0
2016-07-11 07:35:15 -05:00
parent 6088e4655e
commit afa13e7364
78 changed files with 150 additions and 150 deletions
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2
Luminary099/AOSTASK_AND_AOSJOB.s
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@ -391,7 +391,7 @@ DVOVSUB TS SCRATCHY # SAVE UPPER HALF OF DIVIDEND
AD BIT1
ZEROPLUS XCH SCRATCHY # STORE ABS(DIVISOR). PICK UP TOP HALF OF
EXTEND # DIVIDENT.
EXTEND # DIVIDEND.
BZMF GOODNEG # GET -ABS(DIVIDEND)
# Page 1493
CS A

2
Luminary099/AOTMARK.s
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@ -157,7 +157,7 @@ COASCODE INDEX FIXLOC
TC INTPRET # COMPUTE X AND Y PLANE VECTORS
# Page 248
# THE OPTAXIS SOBROUTINE COMPUTES THE X AND Y MARK PLANE VECS AND
# THE OPTAXIS SUBROUTINE COMPUTES THE X AND Y MARK PLANE VECS AND
# ROTATES THEM THRU THE APPARENT FIELD OF VIEW ROTATION UNIQUE TO AOT
# OPTAXIS USES OANB TO COMPUTE THE OPTIC AXIS
#

8
Luminary099/ASCENT_GUIDANCE.s
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@ -357,7 +357,7 @@ ASCTERM EXIT
CALL
FINDCDUW -2
ASCTERM1 EXIT
+1 CA FLAGWRD9 # INSURE THAT THE NOUN 63 DISPLAY IS
+1 CA FLAGWRD9 # ENSURE THAT THE NOUN 63 DISPLAY IS
MASK FLRCSBIT # BYPASSED IF WE ARE IN THE RCS TRIMMING
CCS A # MODE OF OPERATION
TCF ASCTERM3
@ -374,7 +374,7 @@ ASCTERM3 TCF ENDOFJOB
ASCTERM4 EXIT
INHINT
TC IBNKCALL # NO GUIDANCE THIS CYCLE -- HENCE ZERO
CADR ZATTEROR # THE DAP COMMANDED ERRORSss.
CADR ZATTEROR # THE DAP COMMANDED ERRORS.
TCF ASCTERM1 +1
CHECKALT DLOAD DSU
@ -425,7 +425,7 @@ OFFROT CLRGO
SETXFLAG = CHECKYAW
CHECKYAW SET
XOVINFLG # PROHIBIT X-AXIS OVERRRIDE
XOVINFLG # PROHIBIT X-AXIS OVERRIDE
DLOAD VXSC
ATY
LAXIS
@ -473,7 +473,7 @@ ENGOFF RTB
PIPTIME
TTOGO
DCOMP EXIT
TC TPAGREE # FORCH SIGN AGREEMENT ON MPAC, MPAC +1.
TC TPAGREE # FORCE SIGN AGREEMENT ON MPAC, MPAC +1.
CAF EBANK7
TS EBANK
EBANK= TGO

8
Luminary099/ATTITUDE_MANEUVER_ROUTINE.s
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@ -46,7 +46,7 @@
# WHEN POINTING A SPACECRAFT AXIS (I.E., X, Y, Z, THE AOT, THRUST AXIS, ETC.) THE SUBROUTINE VECPOINT MAY BE
# USED TO GENERATE THIS SET OF DESIRED CDU ANGLES (SEE DESCRIPTION IN R60).
#
# WITH THIS INFORMATION KALCMANU DETERMINES THE DIRECTION OF THE SINGLE EQUIVALEN ROTATION (COF ALSO U) AND THE
# WITH THIS INFORMATION KALCMANU DETERMINES THE DIRECTION OF THE SINGLE EQUIVALENT ROTATION (COF ALSO U) AND THE
# MAGNITUDE OF THE ROTATION (AM) TO BRING THE S/C FROM ITS INITIAL ORIENTATION TO ITS FINAL ORIENTATION.
# THIS DIRECTION REMAINS FIXED BOTH IN INERTIAL COORDINATES AND IN COMMANDED S/C AXES THROUGHOUT THE
# _
@ -86,7 +86,7 @@
# A) AM LESS THAN .25 DEGREES (MINANG)
# B) AM GREATER THAN 170 DEGREES (MAXANG)
#
# IF AM IS LESS THAN .25 DEGREES, NO COMPLICATED AUTOMATIC MANEUVERING IS NECESSARY. THREFORE, WE CAN SIMPLY
# IF AM IS LESS THAN .25 DEGREES, NO COMPLICATED AUTOMATIC MANEUVERING IS NECESSARY. THEREFORE, WE CAN SIMPLY
# SET CDU DESIRED EQUAL TO THE FINAL CDU DESIRED ANGLES AND TERMINATE THE JOB.
#
# IF AM IS GREATER THAN .25 DEGREES BUT LESS THAN 170 DEGREES THE AXES OF THE SINGLE EQUIVALENT ROTATION
@ -141,7 +141,7 @@
# RELINT
#
# THE USER'S PROGRAM MAY EITHER CONTINUE OR WAIT FOR THE TERMINATION OF THE MANEUVER. IF THE USER WISHES TO
# WAIT, HE MAY PUT HIS JOB TO SLEEP WTH THE FOLLOWING INSTRUCTIONS:
# WAIT, HE MAY PUT HIS JOB TO SLEEP WITH THE FOLLOWING INSTRUCTIONS:
#
# L TC BANKCALL
# L+1 CADR ATTSTALL
@ -260,7 +260,7 @@
# THIS ROUTINE EXTRACTS THE CDU ANGLES FROM A DIRECTION COSINE MATRIX (M SCALED BY 2) RELATING S/C AXIS TO
# *
# STABLE MEMBER AXES. X1 MUST CONTAIN THE COMPLEMENT OF THE STARTING ADDRESS FOR M. THE SUBROUTINE LEAVES THE
# CORRESPONDING GIMBAL ANGLES IN V(MPAC) AS DOUBLE PRECISION 1'S COMPLEMENT ANGLES ACALED BY 2PI. THE FORMULAS
# CORRESPONDING GIMBAL ANGLES IN V(MPAC) AS DOUBLE PRECISION 1'S COMPLEMENT ANGLES SCALED BY 2PI. THE FORMULAS
# FOR THIS CONVERSION ARE
#
# Z = ARCSIN (M )

4
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 ACCOMODATED BY MEANS OF TABLES CONTAINING CONSTANTS (FOR AVEGEXIT, FOR
# VARIATIONS AMONG PROGRAMS ARE ACCOMMODATED 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,
@ -594,7 +594,7 @@ ZOOM = P40ZOOMA
COMFAIL TC UPFLAG # (15)
ADRES IDLEFLAG
TC UPFLAG # SET FLAG TO SUPRESS CONFLICTING DISPLAY
TC UPFLAG # SET FLAG TO SUPPRESS CONFLICTING DISPLAY
ADRES FLUNDISP
CAF FOUR # RESET DVMON
TS DVCNTR

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 # JASK NOT IN PROGRESS, INITIALIZE NEG.
TS DAPZRUPT # TASK NOT IN PROGRESS, INITIALIZE NEG.
CA TWO
TS NPTRAPS
TS NQTRAPS

2
Luminary099/DOWN_TELEMETRY_PROGRAM.s
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@ -321,7 +321,7 @@ DNTMEXIT EXTEND # DOWN-TELEMETRY EXIT
CA L # RESPECTIVELY
TMEXITL EXTEND
WRITE DNTM2
TMRESUME TCF RESUME # EXIT TELEMTRY PROGRAM VIA RESUME.
TMRESUME TCF RESUME # EXIT TELEMETRY PROGRAM VIA RESUME.
MINB12 EQUALS -1/8
DNECADR EQUALS TMINDEX

2
Luminary099/FINDCDUW--GUIDAP_INTERFACE.s
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@ -45,7 +45,7 @@
# FINDCDUW PROVIDES THE INTERFACES BETWEEN THE VARIOUS POWERED FLITE GUIDANCE PROGRAMS
# AND THE DIGITAL AUTOPILOT. THE INPUTS TO FINDCDUW ARE THE THRUST COMMAND VECTOR
# AND THE WINDOW COMMAND VECTOR, AND THE OUTPUTS ARE THE GIMBAL ANGLE
# INCRMENTS, THE COMMANDED ATTITUDE ANGLE RATES, AND THE COMMANDED
# INCREMENTS, THE COMMANDED ATTITUDE ANGLE RATES, AND THE COMMANDED
# ATTITUDE LAG ANGLES (WHICH ACCOUNT FOR THE ANGLES BY WHICH THE BODY WILL
# LAG BEHIND A RAMP COMMAND IN ATTITUDE ANGLE DUE TO THE FINITE ANGULAR
# ACCELERATIONS AVAILABLE).

4
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 FALSI METHOD IN
# METHOD IN ITERATOR FALSE METHOD IN
SLOPEBIT = BIT3 # ITERATOR
# BIT 2 FLAG 1 (S)
@ -687,7 +687,7 @@ FLAGWRD6 = STATE +6 # (090-104)
# BIT 15 FLAG 6 (S)
S32.1F1 = 090D # DELTA V AT CSI TIME DVT1 LESS THAN MAX
S32BIT1 = BIT15 # ONE EXEEDS MAX
S32BIT1 = BIT15 # ONE EXCEEDS MAX
# BIT 14 FLAG 6 (S)
S32.1F2 = 091D # FIRST PASS OF REITERATION OF

4
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 RRADAR INFORMATION FOR LM
# BIT 1 ZERO RR CDU; CDU'S GIVE RADAR INFORMATION FOR LM
# BIT 2 ENABLE CDU RADAR ERROR COUNTERS
# BIT 3 NOT USED
# BIT 4 COARSE ALIGN ENABLE OF IMU
@ -158,7 +158,7 @@
# BIT 10 LM COMPUTER (NOT AGS) HAS CONTROL OF LM.
# BIT 11 IMU CAGE COMMAND TO DRIVE IMU GIMBAL ANGLES TO 0.
# BIT 12 IMU CDU FAIL (MALFUNCTION OF IMU CDU,S)
# BIT 13 IMU FAIL (MALFUCTION OF IMU STABILIZATION LOOPS)
# BIT 13 IMU FAIL (MALFUNCTION OF IMU STABILIZATION LOOPS)
# BIT 14 ISS TURN ON REQUESTED
# BIT 15 TEMPERATURE OF STABLE MEMBER WITHIN DESIGN LIMITS

2
Luminary099/LAMBERT_AIMPOINT_GUIDANCE.s
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@ -65,7 +65,7 @@
# DISPLAYS USED IN P-31LM **
#
# V06N33 DISPLAY SOTRED TIG (IN HRS. MINS. SECS.)
# V06N33 DISPLAY STORED 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/LANDING_ANALOG_DISPLAYS.s
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@ -17,7 +17,7 @@
# 2021112-061. July 14, 1969.
#
# Prepared by
# Massachussets Institute of Technology
# Massachusetts Institute of Technology
# 75 Cambridge Parkway
# Cambridge, Massachusetts
#

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 PRECEEDING STORE
MPAC # SET MODE TO DP. (THE PRECEDING STORE
# MAY BE DP, TP OR VECTOR.)
RTB SETPD
CDULOGIC

4
Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s
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@ -960,7 +960,7 @@ RODCOMP INHINT
XCH OLDPIPAZ
XCH RUPTREG3
EXTEND # SHAPSHOT TIME OF PIPA READING.
EXTEND # SNAPSHOT TIME OF PIPA READING.
DCA TIME2
# Page 817
DXCH THISTPIP
@ -1093,7 +1093,7 @@ AFCSPOT DLOAD # (2), (4), OR (6)
2D
STODL /AFC/ # (0)
ITRPNT2 EXIT
DXCH MPAC # MPAC = MEASURED ACCELARATION.
DXCH MPAC # MPAC = MEASURED ACCELERATION.
TC BANKCALL
CADR THROTTLE +3
TC INTPRET

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 ESTIMATER
# BEGIN OFFSET ESTIMATOR
# IN POWERED FLIGHT, AOSTASK WILL BE CALLED EVERY 2 SECONDS.
# AOS = AOS + K*SUMRATE

2
Luminary099/P12.s
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@ -49,7 +49,7 @@ P12LM TC PHASCHNG
TC CLRADMOD # INITIALIZE RADMODES FOR R29
TC DOWNFLAG # CLEAR RENDEVOUS FLAG FOR P22
TC DOWNFLAG # CLEAR RENDEZVOUS FLAG FOR P22
ADRES RNDVZFLG
CAF THRESH2 # INITIALIZE DVMON

8
Luminary099/P32-P35_P72-P75.s
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@ -44,14 +44,14 @@
# (3) TO DISPLAY TO THE ASTRONAUT AND THE GROUND DEPENDENT VARIABLES
# ASSOCIATED WITH THE CONCENTRIC FLIGHT PLAN MANEUVERS FOR
# APPROVAL BY THE ASTRRONAUT/GROUND.
# APPROVAL BY THE ASTRONAUT/GROUND.
# (4) TO STORE THE CSI TARGET PARAMETERS FOR USE BY THE DESIRED
# THRUSTING PROGRAM.
#
# ASSUMPTIONS
# (1) AT A SELECTED TPI TIME THE LINE OF SIGNT BETWEEN THE ACTIVE
# (1) AT A SELECTED TPI TIME THE LINE OF SIGHT BETWEEN THE ACTIVE
# AND PASSIVE VEHICLES IS SELECTED TO BE A PRESCRIBED ANGLE (E)
# FROM THE HORIZONTAL PLANE DEFINED BY THE ACTIVE VEHICLE
# POSITION.
@ -72,7 +72,7 @@
# IGNITION.
# (6) THE PERICENTER ALTITUDE OF THE ORBIT FOLLOWING CSI AND CDH
# MUST BE GREATER THAN 35,000 FT (LUNAR ORBIT) OR 85 NM (EARCH
# MUST BE GREATER THAN 35,000 FT (LUNAR ORBIT) OR 85 NM (EARTH
# ORBIT) FOR SUCCESSFUL COMPLETION OF THIS PROGRAM.
# (7) THE CSI AND CDH MANEUVERS ARE ORIGINALLY ASSUMED TO BE
@ -107,7 +107,7 @@
# CALCULATES THE MANEUVER PARAMETERS. SET AT THE START OF
# EACH RENDEZVOUS PRE-THRUSTING PROGRAM.
#
# FINAL FLAG -- SELECTES FINAL PROGRAM DISPLAYS AFTER CREW HAS
# FINAL FLAG -- SELECTED FINAL PROGRAM DISPLAYS AFTER CREW HAS
# COMPLETED THE FINAL MANEUVER COMPUTATION AND DISPLAY
# CYCLE.
#

2
Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s
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@ -45,7 +45,7 @@ CALLQERR CA BIT13 # CALCULATE Q,R ERRORS UNLESS THESE AXES
CS DAPBOOLS # IN MANUAL RATE COMMAND?
MASK OURRCBIT
EXTEND
BZF Q,RORGTS # IF SO BYPASS CALCULATION OF ERROS.
BZF Q,RORGTS # IF SO BYPASS CALCULATION OF ERRORS.
TC QERRCALC
Q,RORGTS CCS COTROLER # CHOOSE CONTROL SYSTEM FOR THIS DAP PASS:

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 SAMLING
RADSAMP CCS RSAMPDT # TIMES NORMAL ONCE PER SECOND SAMPLING
TCF +2
TCF TASKOVER # +0 INSERTED MANUALLY TERMINATES TEST.

4
Luminary099/RCS_FAILURE_MONITOR.s
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@ -34,7 +34,7 @@
# THIS ROUTINE IS ATTACHED TO T4RUPT, AND IS ENTERED EVERY 480 MS. ITS FUNCTION IS TO EXAMINE THE LOW 8 BITS
# OF CHANNEL 32 TO SEE IF ANY ISOLATION-VALVE CLOSURE BITS HAVE APPEARED OR DISAPPEARED (THE CREW IS WARNED OF JET
# FAILURES BY LAMPS LIT BY THE GRUMMAN FAILURE-DETECTION CIRCUITRY; THEY MAY RESPOND BY OPERATING SWITCHES WHICH
# ISOLATE PAIRS OF JETS FROM THE PROPELLANT TANKS AND SET BITS IN CHANNEL 32). iN THE EVENT THAT CHANNEL 32 BITS
# ISOLATE PAIRS OF JETS FROM THE PROPELLANT TANKS AND SET BITS IN CHANNEL 32). IN THE EVENT THAT CHANNEL 32 BITS
# DIFFER FROM `PVALVEST', THE RECORD OF ACTIONS TAKEN BY THIS ROUTINE, THE APPROPRIATE BITS IN `CH5MASK' &
# `CH6MASK', USED BY THE DAP JET-SELECTION LOGIC, ARE UPDATED, AS IS `PVALVEST'. TO SPEED UP & SHORTEN THE
# ROUTINE, NO MORE THAN ONE CHANGE IS ACCEPTED PER ENTRY. THE HIGHEST-NUMBERED BIT IN CHANNEL 32 WHICH REQUIRES
@ -47,7 +47,7 @@
# FORMER STATE. THE CONSEQUENCE OF THIS IS THAT THE NEXT ENTRY WOULD NOT SEE THE CHANGE INCOMPLETELY INCORP-
# ORATED BY THE LAST PASS (BECAUSE IT WENT AWAY AT JUST THE RIGHT TIME), BUT THE DAP MASK-WORDS WILL BE INCORRECT.
# THIS COMBINATION OF EVENTS SEEMS QUITE REMOTE, BUT NOT IMPOSSIBLE UNLESS THE CREW OPERATES THE SWITCHES AT HALF-
# SECOND INTERVALS OR LONGER. IN ANY EVENT, A DISAGREEMENT BETWEEN REALITY AND THE DAP MASKS WILL BE CUREED IF
# SECOND INTERVALS OR LONGER. IN ANY EVENT, A DISAGREEMENT BETWEEN REALITY AND THE DAP MASKS WILL BE CURED IF
# THE MISINTERPRETED SWITCH IS REVERSED AND THEN RESTORED TO ITS CORRECT POSITION (SLOWLY).
#
# CALLING SEQUENCE:

2
Luminary099/RTB_OP_CODES.s
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@ -119,7 +119,7 @@ TPMODE CAF ONE # MODE IS TP.
TC Q
# THE FOLLOWING ROUTINE INCREMENTS IN 2S COMPLEMENT THE REGISTER WHOSE ADDRESS IS IN BUF BY THE 1S COMPL.
# QUANTITY FOUND IN TEM2. THIS MAY BE USED TO INCRMENT DESIRED IMU AND OPTICS CDU ANGLES OR ANY OTHER 2S COMPL.
# QUANTITY FOUND IN TEM2. THIS MAY BE USED TO INCREMENT DESIRED IMU AND OPTICS CDU ANGLES OR ANY OTHER 2S COMPL.
# (+0 UNEQUAL TO -0) QUANTITY. MAY BE CALLED BY BANKCALL/SWCALL.
CDUINC TS TEM2 # 1S COMPL.QUANT. ARRIVES IN ACC. STORE IT

2
Luminary099/SERVICER.s
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@ -19,7 +19,7 @@
# 2021112-061. July 14, 1969.
#
# Prepared by
# Massachussets Institute of Technology
# Massachusetts Institute of Technology
# 75 Cambridge Parkway
# Cambridge, Massachusetts
#

2
Luminary099/SPS_BACK-UP_RCS_CONTROL.s
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@ -114,7 +114,7 @@ NEGCHECK INDEX AXISCTR # JETS FIRING NEGATIVELY
TCF +2
TCF +1 # JETS COMMANDED OFF. SET CTR AND RETURN
SETCTR INDEX AXISCTR # JET FIRING REVERSAL COMMANDED. SET CTR,
CA UTIME # SET JET TIME TO ZER, AND RETURN
CA UTIME # SET JET TIME TO ZERO, AND RETURN
# Page 1509
INDEX AXISCTR
TS UJETCTR

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 PRECEEDING PIPA INTERVAL, AND SINCE FP IS COMPUTED DIRECTLY FROM /AF/, FP IN ORDER TO CORRESPOND TO THE
# THE PRECEDING 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/

2
Luminary099/TJET_LAW.s
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@ -156,7 +156,7 @@ ERRTEST CCS E # DOES BIG ERROR (THREE DEG BEYOND THE
SU FIREDB
EXTEND
BZMF SENSTEST # IF NOT: ARE UNBALANCED JETS PREFERRED?
MAXJETS CAF TWO # IF YES: INCRMENT ADDRESS LOCATOR AND
MAXJETS CAF TWO # IF YES: INCREMENT ADDRESS LOCATOR AND
ADS ADRSDIF2 # SET SWITCH FOR JET SELECT LOGIC TO 4.
CAF FOUR # (ALWAYS DO THIS FOR P-AXIS)
TCF TJCALC