From 2f62a05a56e5481306c5f0b89cb11e9e77de0bc8 Mon Sep 17 00:00:00 2001 From: James Harris Date: Tue, 12 Jul 2016 18:52:11 -0500 Subject: [PATCH] Readd some typos based on the original scans --- Comanche055/CSM_GEOMETRY.s | 2 +- Comanche055/ERASABLE_ASSIGNMENTS.s | 4 ++-- Comanche055/EXTENDED_VERBS.s | 2 +- Comanche055/FRESH_START_AND_RESTART.s | 4 ++-- Comanche055/IMU_CALIBRATION_AND_ALIGNMENT.s | 2 +- Comanche055/INTERPRETER.s | 8 ++++---- Comanche055/JET_SELECTION_LOGIC.s | 2 +- Comanche055/KEYRUPT_UPRUPT.s | 2 +- Comanche055/MEASUREMENT_INCORPORATION.s | 2 +- Comanche055/ORBITAL_INTEGRATION.s | 4 ++-- Comanche055/P20-P25.s | 12 ++++++------ Comanche055/P32-P33_P72-P73.s | 2 +- Comanche055/P51-P53.s | 4 ++-- Comanche055/P61-P67.s | 1 - Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s | 2 +- Comanche055/R30.s | 6 +++--- Comanche055/RCS-CSM_DIGITAL_AUTOPILOT.s | 4 ++-- Comanche055/RT8_OP_CODES.s | 2 +- Comanche055/T4RUPT_PROGRAM.s | 2 +- Comanche055/TIME_OF_FREE_FALL.s | 2 +- Comanche055/TVCROLLDAP.s | 2 +- Comanche055/WAITLIST.s | 4 ++-- Luminary099/ASCENT_GUIDANCE.s | 2 +- .../BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s | 2 +- Luminary099/DAPIDLER_PROGRAM.s | 2 +- Luminary099/FLAGWORD_ASSIGNMENTS.s | 2 +- Luminary099/INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.s | 2 +- Luminary099/LAMBERT_AIMPOINT_GUIDANCE.s | 2 +- Luminary099/LEM_GEOMETRY.s | 2 +- Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s | 2 +- Luminary099/P-AXIS_RCS_AUTOPILOT.s | 2 +- Luminary099/P12.s | 2 +- Luminary099/P32-P35_P72-P75.s | 4 ++-- Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s | 4 ++-- Luminary099/RADAR_LEADIN_ROUTINES.s | 2 +- Luminary099/RTB_OP_CODES.s | 2 +- Luminary099/THROTTLE_CONTROL_ROUTINES.s | 2 +- 37 files changed, 54 insertions(+), 55 deletions(-) diff --git a/Comanche055/CSM_GEOMETRY.s b/Comanche055/CSM_GEOMETRY.s index 41ee100..8a77811 100644 --- a/Comanche055/CSM_GEOMETRY.s +++ b/Comanche055/CSM_GEOMETRY.s @@ -111,7 +111,7 @@ CALCSXA ITA VLOAD # PUSHDOWN 00-26D, 28D, 30D, 32D-36D # SIGHT LIES ALONG THE STAR VECTOR. # # THE INPUTS ARE: 1) THE STAR VECTOR REFERRED TO ANY COORDINATE SYSTEM STORED AT STAR. 2) THE NAVIGATION BASE -# COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB,AND +# COORDINATES REFERRED TO THE SAME COORDINATE SYSTEM. THESE THREE HALF-UNIT VECTORS ARE STORED AT XNB, YNB, AND # ZNB. # # THE OUTPUTS ARE THE SEXTANT SHAFT AND TRUNNION ANGLES STORED DP AT SAC AND PAC RESPECTIVELY. (LOW ORDER PART diff --git a/Comanche055/ERASABLE_ASSIGNMENTS.s b/Comanche055/ERASABLE_ASSIGNMENTS.s index 64cf49c..c2b3cc1 100644 --- a/Comanche055/ERASABLE_ASSIGNMENTS.s +++ b/Comanche055/ERASABLE_ASSIGNMENTS.s @@ -546,8 +546,8 @@ TRM03FLG = 026D # REQUEST TO NO REQUEST TO TRM03BIT = BIT4 # BIT 3 FLAG 1 -SLOPESW = 027D # ITERATE WITH BIAS ITERATE WITH REGULAR - # METHOD IN ITERATOR FALSE METHOD IN +SLOPESW = 027D # ITERATE WITH BIAS ITERATE WITH REGULA + # METHOD IN ITERATOR FALSI METHOD IN # ITERATOR SLOPEBIT = BIT3 diff --git a/Comanche055/EXTENDED_VERBS.s b/Comanche055/EXTENDED_VERBS.s index b82eff7..a503699 100644 --- a/Comanche055/EXTENDED_VERBS.s +++ b/Comanche055/EXTENDED_VERBS.s @@ -76,7 +76,7 @@ LST2FAN TC VBZERO # VB40 ZERO (USED WITH NOUN 20 ONLY) TC V62 # VB62 SELECT MODE II, ERROR WRT N22 TC V63 # VB63 SELECT MODE III, ERROR WRT N17 TC VB64 # VB64 CALCULATE, DISPLAY S-BAND ANT ANGLES - TC CKOPTVB # V 65 E OPTICAL VERIFICATION FOR PRELAUNCH + TC CKOPTVB # V 65 E OPTICAL VERIFICATION FOR PRELAUNC TC ATTACHED # VB66 ATTACHED. MOVE THIS TO OTHER STATE TC V67 # VB67 W MATRIX MONITOR TC STROKON # VB68 CSM STROKE TEST ON. diff --git a/Comanche055/FRESH_START_AND_RESTART.s b/Comanche055/FRESH_START_AND_RESTART.s index ca56a99..8c89614 100644 --- a/Comanche055/FRESH_START_AND_RESTART.s +++ b/Comanche055/FRESH_START_AND_RESTART.s @@ -932,7 +932,7 @@ DUMMYAD EXIT # Page 200 TC BANKCALL - CADR UPACTOFF # TURN OFF UPLINK ACTIVE LIGHT + CADR UPACTOFF # TURN OFF UPLINK ACTIV LIGHT TC DOWNFLAG ADRES VHFRFLAG @@ -1000,7 +1000,7 @@ RENDN00 CS MMNUMBER EXTEND BZF KILL20 - CA FLAGWRD0 # IS RENDEZVOUS FLAG SET + CA FLAGWRD0 # IS RENDEZVOO FLAG SET MASK RNDVZBIT CCS A TCF STATQUO diff --git a/Comanche055/IMU_CALIBRATION_AND_ALIGNMENT.s b/Comanche055/IMU_CALIBRATION_AND_ALIGNMENT.s index 9cd552a..d184781 100644 --- a/Comanche055/IMU_CALIBRATION_AND_ALIGNMENT.s +++ b/Comanche055/IMU_CALIBRATION_AND_ALIGNMENT.s @@ -430,7 +430,7 @@ FINETIME INHINT # RETURNS WITH INTERRUPT INHIBITED # INTEGRATED TOGETHER TO SAVE WORDS. COMPASS IS COMPLETELY RESTART # PROOFED EXCEPT FOR THE FIRST 30 SECONDS OR SO. PERFORMANCE TESTS OF # THE IRIGS IS RESTART PROOFED ENOUGH TO GIVE 75 PERCENT CONFIDENCE THAT -# IF A RESTART OCCURS THE DATA WILL STILL BE GOOD. GOOD PRACTICE TO RECYCLE +# IF A RESTART OCCURS THE DATA WILL STILL BE GOOD. GOOD PRACTICE TO RECYCL # WHEN A RESTART OCCURS UNLESS IT HAPPENS NEAR THE END OF A TEST -- THEN WAIT # FOR THE DATA TO FLASH. # diff --git a/Comanche055/INTERPRETER.s b/Comanche055/INTERPRETER.s index daf91ab..0a2e426 100644 --- a/Comanche055/INTERPRETER.s +++ b/Comanche055/INTERPRETER.s @@ -97,7 +97,7 @@ LOW7 OCT 177 MASK LOW7 # WHERE CCS EDOP WILL HONOR IT NEXT. OPJUMP TS CYR # LOWWD ENTERS HERE IF A RIGHT-HAND OP - CCS CYR # CODE IS TO BE PROCESSED. TEST PREFIXES. + CCS CYR # CODE IS TO BE PROCESSED. TEST PREFICES. TCF OPJUMP2 # TEST SECOND PREFIX BIT. TCF EXIT # +0 OP CODE IS EXIT @@ -401,7 +401,7 @@ STADR CA BANKSET # THE STADR CODE (PUSHUP UP ON STORE INCR LOC ITR1 INDEX LOC # THE STORECODE WAS STORED COMPLEMENTED TO CS 0 # MAKE IT LOOK LIKE AN OPCODE PAIR. - AD NEGONE # (YUL CAN'T REMOVE 1 BECAUSE OF EARLY CCS) + AD NEGONE # (YUL CANT REMOVE 1 BECAUSE OF EARLY CCS) DOSTORE TS ADDRWD MASK LOW11 # ENTRY FROM DISPATCHER. SAVE THE ERASABLE @@ -1336,8 +1336,8 @@ UPPOS XCH L # SAVE DECREMENTED UPPER PART. AD HALF TS A # SKIPS ON OVERFLOW TCF +2 - INCR L # RESTORE UPPER TO ORIGINAL VALUE - XCH L # SWAP A + L BANK. + INCR L # RESTORE UPPER TO ROIGINAL VALUE + XCH L # SWAP A + L BACK. TC Q UPNEG XCH L # SAVE COMPLEMENTED + DECREMENTED UPPER PT diff --git a/Comanche055/JET_SELECTION_LOGIC.s b/Comanche055/JET_SELECTION_LOGIC.s index 7eed1a9..b1a14f0 100644 --- a/Comanche055/JET_SELECTION_LOGIC.s +++ b/Comanche055/JET_SELECTION_LOGIC.s @@ -278,7 +278,7 @@ BDZCHECK CA ZNDX BZF TAUCHECK ACRBDZ CA T5TEMP # Z-TRANSLATION ACCEPTED EVEN THO WE MAY - TS RWORD1 # HAVE INTRODUCED AN UNDESIRABLE ROLL + TS RWORD1 # HAVE INTRODUCED AN UNDESIREABLE ROLL TCF ROLLTIME # BRANCH TO JET ON-TIME CALCULATIONS TAUCHECK CCS TAU diff --git a/Comanche055/KEYRUPT_UPRUPT.s b/Comanche055/KEYRUPT_UPRUPT.s index f3c1985..19493c2 100644 --- a/Comanche055/KEYRUPT_UPRUPT.s +++ b/Comanche055/KEYRUPT_UPRUPT.s @@ -127,7 +127,7 @@ ELRCODE OCT 22 # THE RECEPTION OF A BAD CODE (I.E., CCC FAILURE) LOCKS OUT FURTHER UPLINK ACTIVITY BY SETTING BIT4 OF FLAGWRD7 = 1. # THIS INDICATION WILL BE TRANSFERRED TO THE GROUND BY THE DOWNLINK WHICH DOWNLINKS ALL FLAGWORDS. # WHEN UPLINK ACTIVITY IS LOCKED OUT, IT CAN BE ALLOWED WHEN THE GROUND UPLINKS AND `ERROR RESET' CODE. -# (IT IS RECOMMENDED THAT THE `ERROR LIGHT RESET' CODE IS PRECEDED BY 16 BITS THE FIRST OF WHICH IS 1 FOLLOWED +# (IT IS RECOMMENDED THAT THE `ERROR LIGHT RESET' CODE IS PRECEEDED BY 16 BITS THE FIRST OF WHICH IS 1 FOLLOWED # BY 15 ZEROS. THIS WILL ELIMINATE EXTRANEOUS BITS FROM INLINK WHICH MAY HAVE BEEN LEFT OVER FROM THE ORIGINAL # FAILURE). # diff --git a/Comanche055/MEASUREMENT_INCORPORATION.s b/Comanche055/MEASUREMENT_INCORPORATION.s index 6ecdee5..7468155 100644 --- a/Comanche055/MEASUREMENT_INCORPORATION.s +++ b/Comanche055/MEASUREMENT_INCORPORATION.s @@ -362,7 +362,7 @@ FAZC CALL GRP2PC # Page 1259 VLOAD VAD # START 3RD PHASE OF INCORP2 - X789 # 7TH, 8TH, 9TH COMPONENTS OF STATE VECTOR + X789 # 7TH,8TH,9TH,COMPONENT OF STATE VECTOR DELTAX +12D # INCORPORATION FOR X789 STORE TX789 BON RTB diff --git a/Comanche055/ORBITAL_INTEGRATION.s b/Comanche055/ORBITAL_INTEGRATION.s index f5b6c2d..836472e 100644 --- a/Comanche055/ORBITAL_INTEGRATION.s +++ b/Comanche055/ORBITAL_INTEGRATION.s @@ -227,9 +227,9 @@ GAMCOMP VLOAD VSR1 # Page 1339 36D STORE BETAM - NORM BDDV # FORM NORMALIZE QUOTIENT ALPHAM/BETAM + NORM BDDV # FORM NORMALIZED QUOTIENT ALPHAM/BETAM 33D - SR1R PUSH # C(PDL+2) = ALMOST NORMALIZE RHO. + SR1R PUSH # C(PDL+2) = ALMOST NORMALIZED RHO. DLOAD* ASCALE,1 STORE S1 diff --git a/Comanche055/P20-P25.s b/Comanche055/P20-P25.s index 9d1da62..01d7cde 100644 --- a/Comanche055/P20-P25.s +++ b/Comanche055/P20-P25.s @@ -420,7 +420,7 @@ DE-GR-50 TC 2PHSCHNG # # ABORT MODES: P23 ABORT IF MARKING SYSTEM OR EXTENDED VERB ACTIVE # -# INPUT: NONE REQUIRES, NORMALLY CALLED BY P23 +# INPUT: NONE REQUIRED, NORMALLY CALLED BY P23 # # OUTPUT: TRUNNION BIAS ANGLE: ANGLE DETERMINED WHEN SHAFT LINE OF SIGHT # (SLOS) AND LANDMARK LINE OF SIGHT (LLOS) ARE SUPERIMPOSED. THIS ANGLE @@ -714,15 +714,15 @@ DECRM61 TS R61CNTR # # INPUT # -# UM, 1/2 UNIT VECTOR ALONG THE CSM-LM LINE-OF-SIGHT (BASIC REF. SYSTEM) +# UM,1/2 UNIT VECTOR ALONG THE CSM-LM LINE-OF-SIGHT (BASIC REF. SYSTEM) # -# USTAR, FICTITIOUS STAR DIRECTION (1/2 UNIT VECTOR) +# USTAR,FICTITIOUS STAR DIRECTION (1/2 UNIT VECTOR) # -# RCLP, RELATIVE CSM TO LM POSITION VECTOR +# RCLP,RELATIVE CSM TO LM POSITION VECTOR # # OUTPUT # -# USTAR, MODIFIED FICTITIOUS STAR DIRECTION (1/2 UNIT VECTOR) +# USTAR,MODIFIED FICTITIOUS STAR DIRECTION (1/2 UNIT VECTOR) # # BVECTOR = 9 DIMENSIONAL BVECTOR (1/2 UNIT VEC.) # @@ -2707,7 +2707,7 @@ DP1MIN 2DEC 6000 V89CALL TC BANKCALL # IMU STATUS CHECK. RETURNS IF ORIENTATION CADR R02BOTH # KNOWN. ALARMS IF NOT. CAF THREE # ALLOW ASTRONAUT TO SELECT DESIRED - TS OPTION1 # TRACKING ATTITUDE AXIS + TS OPTION1 # TRACKING ATTITUDE AXIS. CAF ONE TS OPTION1 +1 CAF VB04N06 # V 04 N 06 diff --git a/Comanche055/P32-P33_P72-P73.s b/Comanche055/P32-P33_P72-P73.s index 35a4fe4..528bf87 100644 --- a/Comanche055/P32-P33_P72-P73.s +++ b/Comanche055/P32-P33_P72-P73.s @@ -39,7 +39,7 @@ # 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 # (1) TO CALCULATE PARAMETERS ASSOCIATED WITH THE FOLLOWING diff --git a/Comanche055/P51-P53.s b/Comanche055/P51-P53.s index ae4cc8a..cf7fe50 100644 --- a/Comanche055/P51-P53.s +++ b/Comanche055/P51-P53.s @@ -317,8 +317,8 @@ V06N89* VN 0689 # # FUNCTION -- TO DISPLAY THE LANDING SITE LATITUDE, # LONGITUDE AND ALTITUDE. TO ACCEPT NEW DATA VIA -# THE KEYBOARD. TO COMPUT THE LANDING SITE -# ORIENTATION FOR P52 OR P54. +# THE KEYBOARD. TO COMPUTE THE LANDING SITE +# ORIENTATION FOR P52 OR P54 # # LET: # RLS = LANDING SITE VECTOR IN REF COORDINATES diff --git a/Comanche055/P61-P67.s b/Comanche055/P61-P67.s index b854b16..ff586d6 100644 --- a/Comanche055/P61-P67.s +++ b/Comanche055/P61-P67.s @@ -516,7 +516,6 @@ SERVCAD2 = SERVCAD1 # MOD NO: 0 DATE: 21 FEB 67 # MOD BY: RR BAIRNSFATHER LOG SECTION: P61-P67 # MOD NO: 1 MOD BY: RR BAIRNSFATHER DATE: 22 JUN 67 RESTARTS. -# # FUNCTIONAL DESCRIPTION: CALLED BY BOTH P61 AND P62 # FIRST, TEST TO SEE IF AVERAGEG IS ON. IF NOT, UPDATE THE STATE VECTOR TO PRESENT TIME + TOLERANCE # AND TURN ON AVERAGEG AT THAT TIME, AND CONTINUE. OTHERWISE CONTINUE: SEE IF IMU Y AXIS IS diff --git a/Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s b/Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s index 3bac890..2da9bfe 100644 --- a/Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s +++ b/Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s @@ -2967,7 +2967,7 @@ ENDRELDS EQUALS # NVMONOPT IS AN ENTRY SIMILAR TO NVSUB, BUT REQUIRING AN ADDITIONAL # Page 370 # PARAMETER IN L. IT SHOULD BE USED ONLY WITH A MONITOR VERB-NOUN CODE IN -# A. AFTER EACH MONITOR DISPLAY A *PLEASE* VERB WILL BE PASSED INT THE VERB +# A. AFTER EACH MONITOR DISPLAY A *PLEASE* VERB WILL BE PASTED IN THE VERB # LIGHTS OR DATA WILL BE BLANKED (OR BOTH) ACCORDING TO THE OPTIONS # SPECIFIED IN L. IF BITS 8-14 OF L ARE OTHER THAN ZERO, THEN THEY WILL # BE INTERPRETED AS A VERB CODE AND PASTED IN THE VERB LIGHTS. (THIS VERB diff --git a/Comanche055/R30.s b/Comanche055/R30.s index ddb5eb5..d16ec10 100644 --- a/Comanche055/R30.s +++ b/Comanche055/R30.s @@ -259,7 +259,7 @@ DOTICK CAF 1SEC # RE-REQUEST TICKTEST. MASK V82FLAGS INDEX A TC +1 - TC TASKOVER # IF NO FLAGBITS SET DON'T CHANGE TFF OR + TC TASKOVER # IF NO FLAGBITS SET DONT CHANGE TFF OR # -TPER, BUT CONTINUE LOOP. TC TPERTICK # ONLY BIT 1 SET. INCR -TPER BY 1 SEC. TFFTICK CAF 1SEC # ONLY BIT 2 SET. INCR TFF BY 1 SEC. @@ -281,7 +281,7 @@ V82GON EXIT # AVERAGE G ON. USE CURRENT STATE VECTOR 2CADR V82GON1 RELINT - CCS NEWJOB # WITHHOLD V16 N44 UNTIL FIRST ORBIT CALC + CCS NEWJOB # WITHOLD V16 N44 UNTIL FIRST ORBIT CALC TC CHANG1 # IS DONE. NOTE: V82GON1 (PRIO7, FINDVAC # JOB) IS COMPLETED BEFORE V82GON (PRIO7, # NOVAC JOB). @@ -340,7 +340,7 @@ SPLRET EXIT EXTEND BZF SPLRET1 V82GON3 CAF BIT5 - MASK EXTVBACT # SEE IF ASTRONAUT HAS SIGNALED TERMINATE + MASK EXTVBACT # SEE IF ASTRONAUT HAS SIGNALLED TERMINATE EXTEND BZF ENDEXT # YES, TERMINATE VB 82 LOOP CAF 1SEC diff --git a/Comanche055/RCS-CSM_DIGITAL_AUTOPILOT.s b/Comanche055/RCS-CSM_DIGITAL_AUTOPILOT.s index 9a5ca3a..4116427 100644 --- a/Comanche055/RCS-CSM_DIGITAL_AUTOPILOT.s +++ b/Comanche055/RCS-CSM_DIGITAL_AUTOPILOT.s @@ -295,7 +295,7 @@ TENTHSEK TS ATTSEC # ALSO IGNORE AUTOMATIC STEERING # SET = + BY # 1) INITIALIZATION PHASE OF AUTOPILOT -# 2) OCCURRENCE OF RHC COMMANDS +# 2) OCCURANCE OF RHC COMMANDS # 3) FREE MODE # 4) SWITCH OVER TO ATTITUDE HOLD FROM AUTO # WHILE DOING AUTOMATIC STEERING (IN THIS CASE @@ -397,7 +397,7 @@ KRESUME1 TCF RESUME # END PHASE 1 # MASK BIT3 # ADS RCSFLAGS # -# THEREAFTER, THE ATTITUDE ERRORS GENERATED BY THE USER SHOULD BE TRANSFERRED TO THE FOLLOWING LOCATIONS IN EBANK6: +# THEREAFTER, THE ATTITUDE ERRORS GENERATED BY THE USER SHOULD BE TRANSFERED TO THE FOLLOWING LOCATIONS IN EBANK6: # # AK SCALED 180 DEGREES NOTE: THESE LOCATIONS ARE SUBJECT # AK1 SCALED 180 DEGREES TO CHANGE diff --git a/Comanche055/RT8_OP_CODES.s b/Comanche055/RT8_OP_CODES.s index 1bf169a..a4e348c 100644 --- a/Comanche055/RT8_OP_CODES.s +++ b/Comanche055/RT8_OP_CODES.s @@ -136,7 +136,7 @@ TPMODE CAF ONE # MODE IS TP. # Page 1510 TC Q - INDEX A # OVERFLOW INCORRECT AND IN MSU. + INDEX A # OVERFLOW UNCORRECT AND IN MSU. CAF LIMITS ADS MPAC TC Q diff --git a/Comanche055/T4RUPT_PROGRAM.s b/Comanche055/T4RUPT_PROGRAM.s index af8594d..cdc0b8e 100644 --- a/Comanche055/T4RUPT_PROGRAM.s +++ b/Comanche055/T4RUPT_PROGRAM.s @@ -1240,7 +1240,7 @@ ENDZOPT TC ZEROPCDU # ZERO OCDU COUNTERS ZEROPCDU CAF ZERO TS CDUS # ZERO IN CDUS, -20 IN CDUT - TS ZONE # INITIALIZE SHAFT MONITOR ZONE. + TS ZONE # INITIALIZE SHAFT MONITOR ZONE CS 20DEGS TS CDUT TC Q diff --git a/Comanche055/TIME_OF_FREE_FALL.s b/Comanche055/TIME_OF_FREE_FALL.s index 8846c10..435a83f 100644 --- a/Comanche055/TIME_OF_FREE_FALL.s +++ b/Comanche055/TIME_OF_FREE_FALL.s @@ -139,7 +139,7 @@ TFFTEM = 36D # TEMPORARY # TFFNP E:(-38+2NR) M LCP, SEMI LATUS RECTUM, WEIGHTED BY NR. FOR VGAMCALC. # M:(-36+2NR) # TFF/RTMU E:(17) M:(14) 1/SQRT(MU) -# TFFVSQ E:(20) M:(18) 1/M -(V SQ/MU): PRESENT VELOCITY, NORMALIZED. FOR VGAMCALC +# TFFVSQ E:(20) M:(18) 1/M -(V SQ/MU): PRESENT VELOCITY,NORMLIZED. FOR VGAMCALC # TFFALFA E:(26-NR) 1/M ALFA, WEIGHTED BY NR # M:(24-NR) # TFFRTALF E:(10+NA) SQRT(ALFA), NORMALIZED diff --git a/Comanche055/TVCROLLDAP.s b/Comanche055/TVCROLLDAP.s index 952efec..1411e69 100644 --- a/Comanche055/TVCROLLDAP.s +++ b/Comanche055/TVCROLLDAP.s @@ -136,7 +136,7 @@ # PARABOLA WHICH PASSES THROUGH THE OPERATING POINT. FOR REGION 3 # DESIRED OGARATE IS SIMPLY +-MAXLIM. FOR REGIONS 1 OR 6 THE SOLUTION # TO A QUADRATIC IS REQUIRED (THE PENETRATION IS ALONG THE STRAIGHT -# LINE OR MINLIM BOUNDARY SWITCH LINES). AN APPROXIMATION IS MADE +# LINE OR MINLIM BOUNDRY SWITCH LINES). AN APPROXIMATION IS MADE # INSTEAD. CONSIDER AN OPERATING POINT IN REGION 6'. PASS A TANGENT TO # THE CONTROL PARABOLA THROUGH THE OPERATING POINT, AND FIND ITS # INTERSECTION WITH THE STRAIGHT LINE SECTION OF THE SWITCH CURVE... diff --git a/Comanche055/WAITLIST.s b/Comanche055/WAITLIST.s index 8433ca4..fe6d1f7 100644 --- a/Comanche055/WAITLIST.s +++ b/Comanche055/WAITLIST.s @@ -472,7 +472,7 @@ NOQBRSM DXCH ARUPT # LONGEXIT AND LONGEXIT+1 # LONGTIME AND LONGTIME+1 # -# *** THE FOLLOWING IS TO BE IN FIXED-FIXED AND UNSWITCHED ERASABLE ** +# *** THE FOLLOWING IS TO BE IN FIXED-FIXED AND UNSWITCHED ERRASIBLE *** BLOCK 02 EBANK= LST1 @@ -503,7 +503,7 @@ LNGCALL2 LXCH LONGEXIT +1 # SAVE THE CORRECT BB FOR RETURN # *** WAITLIST TASK LONGCYCL *** -LONGCYCL EXTEND # CAN WE SUCCESSFULLY TAKE ABOUT 1.25 +LONGCYCL EXTEND # CAN WE SUCCESFULLY TAKE ABOUT 1.25 DCS DPBIT14 # MINUTES OFF OF LONGTIME DAS LONGTIME diff --git a/Luminary099/ASCENT_GUIDANCE.s b/Luminary099/ASCENT_GUIDANCE.s index 70e654b..2463453 100644 --- a/Luminary099/ASCENT_GUIDANCE.s +++ b/Luminary099/ASCENT_GUIDANCE.s @@ -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 diff --git a/Luminary099/BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s b/Luminary099/BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s index b88a489..b3872b1 100644 --- a/Luminary099/BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s +++ b/Luminary099/BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s @@ -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, diff --git a/Luminary099/DAPIDLER_PROGRAM.s b/Luminary099/DAPIDLER_PROGRAM.s index 164f84a..fb42a73 100644 --- a/Luminary099/DAPIDLER_PROGRAM.s +++ b/Luminary099/DAPIDLER_PROGRAM.s @@ -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 diff --git a/Luminary099/FLAGWORD_ASSIGNMENTS.s b/Luminary099/FLAGWORD_ASSIGNMENTS.s index ee51fef..a0904b4 100644 --- a/Luminary099/FLAGWORD_ASSIGNMENTS.s +++ b/Luminary099/FLAGWORD_ASSIGNMENTS.s @@ -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) diff --git a/Luminary099/INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.s b/Luminary099/INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.s index 3d71a44..d945853 100644 --- a/Luminary099/INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.s +++ b/Luminary099/INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.s @@ -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 diff --git a/Luminary099/LAMBERT_AIMPOINT_GUIDANCE.s b/Luminary099/LAMBERT_AIMPOINT_GUIDANCE.s index fd09189..cd367f4 100644 --- a/Luminary099/LAMBERT_AIMPOINT_GUIDANCE.s +++ b/Luminary099/LAMBERT_AIMPOINT_GUIDANCE.s @@ -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. diff --git a/Luminary099/LEM_GEOMETRY.s b/Luminary099/LEM_GEOMETRY.s index 9eca786..33af2e7 100644 --- a/Luminary099/LEM_GEOMETRY.s +++ b/Luminary099/LEM_GEOMETRY.s @@ -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 diff --git a/Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s b/Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s index 6207887..79cc344 100644 --- a/Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s +++ b/Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s @@ -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: diff --git a/Luminary099/P-AXIS_RCS_AUTOPILOT.s b/Luminary099/P-AXIS_RCS_AUTOPILOT.s index 851f2a7..8a11483 100644 --- a/Luminary099/P-AXIS_RCS_AUTOPILOT.s +++ b/Luminary099/P-AXIS_RCS_AUTOPILOT.s @@ -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 diff --git a/Luminary099/P12.s b/Luminary099/P12.s index b298382..569efd0 100644 --- a/Luminary099/P12.s +++ b/Luminary099/P12.s @@ -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 diff --git a/Luminary099/P32-P35_P72-P75.s b/Luminary099/P32-P35_P72-P75.s index 8be357c..061c7fd 100644 --- a/Luminary099/P32-P35_P72-P75.s +++ b/Luminary099/P32-P35_P72-P75.s @@ -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. # diff --git a/Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s b/Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s index 3de826f..0724045 100644 --- a/Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s +++ b/Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s @@ -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 diff --git a/Luminary099/RADAR_LEADIN_ROUTINES.s b/Luminary099/RADAR_LEADIN_ROUTINES.s index 266f861..bd331d8 100644 --- a/Luminary099/RADAR_LEADIN_ROUTINES.s +++ b/Luminary099/RADAR_LEADIN_ROUTINES.s @@ -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. diff --git a/Luminary099/RTB_OP_CODES.s b/Luminary099/RTB_OP_CODES.s index b1f0e4b..aa6cce0 100644 --- a/Luminary099/RTB_OP_CODES.s +++ b/Luminary099/RTB_OP_CODES.s @@ -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 diff --git a/Luminary099/THROTTLE_CONTROL_ROUTINES.s b/Luminary099/THROTTLE_CONTROL_ROUTINES.s index 49c2289..bb24381 100644 --- a/Luminary099/THROTTLE_CONTROL_ROUTINES.s +++ b/Luminary099/THROTTLE_CONTROL_ROUTINES.s @@ -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/