From 6088e4655e45054f25c0cd848a2ad4eb4b6b2c04 Mon Sep 17 00:00:00 2001 From: Andrew Murray Date: Fri, 8 Jul 2016 20:45:31 +1000 Subject: [PATCH 1/3] Fixed typos --- Comanche055/AGC_BLOCK_TWO_SELF-CHECK.s | 2 +- Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.s | 4 ++-- Comanche055/AUTOMATIC_MANEUVERS.s | 2 +- Comanche055/CM_ENTRY_DIGITAL_AUTOPILOT.s | 6 +++--- Comanche055/CONIC_SUBROUTINES.s | 6 +++--- Comanche055/CSM_GEOMETRY.s | 2 +- Comanche055/DISPLAY_INTERFACE_ROUTINES.s | 4 ++-- Comanche055/DOWN-TELEMETRY_PROGRAM.s | 6 +++--- Comanche055/EXECUTIVE.s | 6 +++--- Comanche055/FRESH_START_AND_RESTART.s | 4 ++-- Comanche055/INTERPRETER.s | 2 +- Comanche055/JET_SELECTION_LOGIC.s | 4 ++-- Comanche055/KALCMANU_STEERING.s | 2 +- Comanche055/KEYRUPT_UPRUPT.s | 2 +- Comanche055/P20-P25.s | 6 +++--- Comanche055/P32-P33_P72-P73.s | 2 +- Comanche055/P34-35_P74-75.s | 2 +- Comanche055/P37_P70.s | 2 +- Comanche055/P51-P53.s | 6 +++--- Comanche055/P61-P67.s | 4 ++-- Comanche055/P76.s | 2 +- Comanche055/PHASE_TABLE_MAINTENANCE.s | 2 +- Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s | 14 +++++++------- Comanche055/PINBALL_NOUN_TABLES.s | 8 ++++---- Comanche055/R60_62.s | 2 +- Comanche055/RCS-CSM_DIGITAL_AUTOPILOT.s | 2 +- Comanche055/RT8_OP_CODES.s | 2 +- Comanche055/STABLE_ORBIT.s | 2 +- Comanche055/SXTMARK.s | 2 +- Comanche055/T4RUPT_PROGRAM.s | 4 ++-- Comanche055/TIME_OF_FREE_FALL.s | 6 +++--- Comanche055/TVCEXECUTIVE.s | 2 +- Comanche055/TVCRESTARTS.s | 2 +- Comanche055/TVCSTROKETEST.s | 4 ++-- Comanche055/UPDATE_PROGRAM.s | 2 +- Luminary099/AOTMARK.s | 2 +- .../BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s | 2 +- Luminary099/DOWN_TELEMETRY_PROGRAM.s | 4 ++-- Luminary099/FINDCDUW--GUIDAP_INTERFACE.s | 2 +- Luminary099/IMU_PERFORMANCE_TESTS_4.s | 2 +- Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s | 8 ++++---- Luminary099/P-AXIS_RCS_AUTOPILOT.s | 2 +- Luminary099/P30_P37.s | 2 +- Luminary099/P32-P35_P72-P75.s | 2 +- Luminary099/P70-P71.s | 2 +- Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s | 6 +++--- Luminary099/RTB_OP_CODES.s | 2 +- Luminary099/SERVICER.s | 2 +- Luminary099/THE_LUNAR_LANDING.s | 2 +- Luminary099/THROTTLE_CONTROL_ROUTINES.s | 2 +- Luminary099/TJET_LAW.s | 2 +- Luminary099/TRIM_GIMBAL_CNTROL_SYSTEM.s | 2 +- 52 files changed, 88 insertions(+), 88 deletions(-) diff --git a/Comanche055/AGC_BLOCK_TWO_SELF-CHECK.s b/Comanche055/AGC_BLOCK_TWO_SELF-CHECK.s index 283661b..e2af62f 100644 --- a/Comanche055/AGC_BLOCK_TWO_SELF-CHECK.s +++ b/Comanche055/AGC_BLOCK_TWO_SELF-CHECK.s @@ -82,7 +82,7 @@ # IN R2 THE BBCON OF SELF-CHECK, AND IN R3 THE TOTAL NUMBER OF ERRORS DETECTED BY SELF-CHECK SINCE THE LAST MAN # INITIATED FRESH START (SLAP1). # -# SHOW-BANKSUM STARTING WTIH BANK 0 DISPLAYS IN R1 THE BANK SUM (A +-NUMBER EQUAL TO THE BANK NUMBER), IN R2 +# SHOW-BANKSUM STARTING WITH BANK 0 DISPLAYS IN R1 THE BANK SUM (A +-NUMBER EQUAL TO THE BANK NUMBER), IN R2 # THE BANK NUMBER, AND IN R3 THE BUGGER WORD. # # ERASABLE INITIALIZATION REQUIRED diff --git a/Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.s b/Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.s index 410935d..62c2db8 100644 --- a/Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.s +++ b/Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.s @@ -250,7 +250,7 @@ # Page 8 # IN THE FOLLOWING NOUN LIST THE 'NO LOAD' RESTRICTION MEANS THE NOUN -# CONTAINS AT LEAST ONE COMONENT WHICH CANNOT BE LOADED, I.E. OF +# CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF # SCALE TYPE L (MIN/SEC) OR PP (2 INTEGERS). # IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22, OR 23 @@ -1033,7 +1033,7 @@ # 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY # 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY # 00007 SPECIFY PROPULSION SYSTEM 1=SPS 2=RCS P37 COLOSSUS -# 00010 SPECIFY ALIGNEMENT MODE 0=ANY TIME 1=REFSMMAT + G P57 LUMINARY +# 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT + G P57 LUMINARY # 2=TWO BODIES 3=ONE BODY + G # 00011 SPEC. SEPARATION MONITOR PHASE 1=DELTAV 2=STATE VECTOR UPDATE P46 LUMINARY # 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY diff --git a/Comanche055/AUTOMATIC_MANEUVERS.s b/Comanche055/AUTOMATIC_MANEUVERS.s index 3aff078..177f86c 100644 --- a/Comanche055/AUTOMATIC_MANEUVERS.s +++ b/Comanche055/AUTOMATIC_MANEUVERS.s @@ -490,7 +490,7 @@ ZEROCMDS CAF ZERO TS TAU1 TS TAU2 T6PROG EXTEND # WHEN THE ROTATION COMMANDS (TAUS) - DCA JETADDR # HAVE BEEN DETERINED + DCA JETADDR # HAVE BEEN DETERMINED DXCH T5LOC # RESET T5LOC FOR PHASE3 TCF RESUME diff --git a/Comanche055/CM_ENTRY_DIGITAL_AUTOPILOT.s b/Comanche055/CM_ENTRY_DIGITAL_AUTOPILOT.s index 96ecd42..6efa3bc 100644 --- a/Comanche055/CM_ENTRY_DIGITAL_AUTOPILOT.s +++ b/Comanche055/CM_ENTRY_DIGITAL_AUTOPILOT.s @@ -32,7 +32,7 @@ # Page 1063 # SUBROUTINE TO READ GIMBAL ANGLES AND FORM DIFFERENCES. GIMBAL ANGLES ARE SAVED IN 2'S COMPLEMENT, BUT THE -# DIFFERENECES ARE IN 1'S COMP. ENTER AND READ ANGLES EACH .1 SEC. +# DIFFERENCES ARE IN 1'S COMP. ENTER AND READ ANGLES EACH .1 SEC. # # CM/DSTBY = 1 FOR DAP OPERATION # CM/DSTBY = 0 TO TERMINATE DAP OPERATION @@ -289,7 +289,7 @@ T5IDLER1 2CADR T5IDLOC # Page 1070 # THIS SECTION CALCULATES THE ANGULAR BODY RATES EACH .1 SEC. THE ANGULAR RATES ARE THOSE ALONG THE BODY AXES -# XB, YB, ZB, AND ARE NORMALLY DESIGNATED P, Q, R. REQIREMENT: TEMPORARILY ERASE. JETEM, JETEM +1 +# XB, YB, ZB, AND ARE NORMALLY DESIGNATED P, Q, R. REQUIREMENT: TEMPORARILY ERASE. JETEM, JETEM +1 # # SINCE RESTARTS ZERO THE JET OUTPUT CHANNELS, NO ATTEMPT IS MADE TO RESTART THE ENTRY DAPS. THAT IS, # THE 0.1 SEC DAPS WILL MISS A CYCLE, AND WILL PICK UP AT THE NEXT 0.1 SEC UPDATE. MOST OF THE TIME THE 2 SEC @@ -1079,7 +1079,7 @@ TIMETST5 CS ONE # SECTION JETCALL EXAMINES CONTENTS OF JET TIMES IN LIST, ESTABLISHES WTLST ENTRIES, AND EXECUTES CORRESPONDING # JET CODES. A POSITIVE NZ NUMBER IN A TIME REGISTER INDICATES THAT A WTLST CALL IS TO BE MADE, AND ITS JET BITS -# EXECUTED. A +0 INDICATES THAT THE TIME INTERVAL DOES NOT APPLY, BUT THE CORRESPOINDING JET BITS ARE TO BE +# EXECUTED. A +0 INDICATES THAT THE TIME INTERVAL DOES NOT APPLY, BUT THE CORRESPONDING JET BITS ARE TO BE # EXECUTED. A NEG NUMBER INDICATES THAT THE TIME INTERVAL HAS BEEN PROCESSED. IN EVENT OF +0 OR -1, THE # SUBSEQUENT TIME REGISTER IS EXAMINED FOR POSSIBLE ACTION. THUS JET BITS TO BE EXECUTED MAY COME FROM MORE # THAN ONE REGISTER. diff --git a/Comanche055/CONIC_SUBROUTINES.s b/Comanche055/CONIC_SUBROUTINES.s index 9bd7ac8..c10fc10 100644 --- a/Comanche055/CONIC_SUBROUTINES.s +++ b/Comanche055/CONIC_SUBROUTINES.s @@ -106,7 +106,7 @@ # RESPECTIVELY, IS THE CENTRAL BODY # TAU +28 DESIRED TRANSFER TIME IN CENTISECONDS (DP) # MAY BE POS OR NEG AND ABSOLUTE VALUE MAY BE GREATER OR LESS THAN ONE ORBITAL PERIOD. -# XKEPNEW +17 FOR EARTH DP GUESS OF ROOT X OF KEPLERS EQN IN SQRT(METERS).SIGN SHOULD AGREE WTIH THAT OF TAU. +# XKEPNEW +17 FOR EARTH DP GUESS OF ROOT X OF KEPLERS EQN IN SQRT(METERS).SIGN SHOULD AGREE WITH THAT OF TAU. # +16 FOR MOON AND ABS VALUE SHOULD BE LESS THAN THAT CORRESPONDING TO A PERIOD, VIZ, 2PI SQRT(SEMI- # MAJOR AXIS), FOR SPEED OF CONVERGENCE, BUT IF EITHER CONDITION FAILS, XKEPNEW IS RESET # BY KEPLER TO A POOR BUT VALID GUESS. @@ -286,7 +286,7 @@ # STATE IS TO BE UPDATED ALONG A CONIC TRAJECTORY, CALCULATES THE CORRESPONDING TIME-OF-FLIGHT AND, IN ADDITION, # PROVIDES THE OPTION OF COMUTING THE NEW UPDATED STATE VECTOR. THE RESULTING TRAJECTORY MAY BE A SECTION OF A # CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE SUBROUTINE CAN BE -# EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WTIHOUT INTRODUCING ANY CODING CHANGES, +# EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES, # ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY. # # THE RESTRICTIONS ARE -- @@ -1776,7 +1776,7 @@ MUTABLE 2DEC* 3.986032 E10 B-36* # MUE LDPOSMAX EQUALS LODPMAX # DPPOSMAX IN LOW MEMORY. -# ERASABLE ASSIGNEMENTS +# ERASABLE ASSIGNMENTS # KEPLER SUBROUTINE diff --git a/Comanche055/CSM_GEOMETRY.s b/Comanche055/CSM_GEOMETRY.s index b845bb5..1057f35 100644 --- a/Comanche055/CSM_GEOMETRY.s +++ b/Comanche055/CSM_GEOMETRY.s @@ -33,7 +33,7 @@ BANK # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT -# VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WTIH THE SEXTANT LINE OF SIGHT. +# VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT. # # THE INPUTS ARE: 1) THE SEXTAND SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR diff --git a/Comanche055/DISPLAY_INTERFACE_ROUTINES.s b/Comanche055/DISPLAY_INTERFACE_ROUTINES.s index 8eb4aba..10390c3 100644 --- a/Comanche055/DISPLAY_INTERFACE_ROUTINES.s +++ b/Comanche055/DISPLAY_INTERFACE_ROUTINES.s @@ -485,7 +485,7 @@ # 5. IT IS ALWAYS GOOD PRACTICE TO TERMINATE AN EXTENDED VERB BEFORE ASKING FOR ANOTHER ONE OR THE SAME ONE # OVER AGAIN. # -# SPECIAL CONSIDERATONS -- +# SPECIAL CONSIDERATIONS -- # Page 1464 # 1. MPAC +2 SAVED ONLY IN MARK DISPLAYS # 2. GODSP(R), REGODSP(R), GOMARK(R) ALWAYS TURN ON THE FLASH IF ENTERED WITH A PASTE VERB REQUEST. @@ -638,7 +638,7 @@ COPYPACS INDEX COPINDEX TC Q -# PINCHEK CHECKS TO SEE IF THE CURRENT MARK REQUEST IS MADE BY THE ASTRONAUT WHILE INTERUPTING A GOPLAY DISPLAY +# PINCHEK CHECKS TO SEE IF THE CURRENT MARK REQUEST IS MADE BY THE ASTRONAUT WHILE INTERRUPTING A GOPLAY DISPLAY # (A NORMAL OR A PRIO). IF THE ASTRONAUT TRIES TO MARK DURING A PRIO, THE CHECK FAIL LIGHT GOES ON AND THE MARK # REQUEST IS ENDED. IF HE TRIES TO MARK DURING A NORM, THE MARK IS ALLOWED. IN THIS CASE THE NORM IS PUT TO SLEEP # UNTIL ALL MARKING IS FINISHED. diff --git a/Comanche055/DOWN-TELEMETRY_PROGRAM.s b/Comanche055/DOWN-TELEMETRY_PROGRAM.s index f6c6027..7b98e12 100644 --- a/Comanche055/DOWN-TELEMETRY_PROGRAM.s +++ b/Comanche055/DOWN-TELEMETRY_PROGRAM.s @@ -106,7 +106,7 @@ # 1. DOWNLISTS. DOWNLISTS MUST BE COMPILED IN THE SAME BANK AS THE # DOWN-TELEMETRY PROGRAM. THIS IS DONE FOR EASE OF CODING, FASTER # EXECUTION. -# 2. EACH DOWNLINK LIST CONSISTES OF A CONTROL LIST AND A NUMBER OF +# 2. EACH DOWNLINK LIST CONSISTS OF A CONTROL LIST AND A NUMBER OF # SUBLISTS. # 3. A SUBLIST REFERS TO A SNAPSHOT OR DATA COMMON TO THE SAME OR OTHER # DOWNLINK LISTS. ANY SUBLIST CONTAINING COMMON DATA NEEDS TO BE @@ -122,7 +122,7 @@ # 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. @@ -347,7 +347,7 @@ 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 diff --git a/Comanche055/EXECUTIVE.s b/Comanche055/EXECUTIVE.s index 7548f2c..6f68477 100644 --- a/Comanche055/EXECUTIVE.s +++ b/Comanche055/EXECUTIVE.s @@ -47,7 +47,7 @@ NOVAC INHINT TS EXECTEM1 TCF NOVAC2 # ENTER EXECUTIVE BANK. -# TO ENTER A JOB REQUEST REQUIREING A VAC AREA -- E.G., ALL (PARTIALLY) INTERPRETIVE JOBS. +# TO ENTER A JOB REQUEST REQUIRING A VAC AREA -- E.G., ALL (PARTIALLY) INTERPRETIVE JOBS. FINDVAC INHINT TS NEWPRIO @@ -157,7 +157,7 @@ NOVAC2 CAF ZERO # NOVAC ENTERS HERE. FIND A CORE SET. NOVAC3 TS EXECTEM2 INDEX LOCCTR CCS PRIORITY # EACH PRIORITY REGISTER CONTAINS -0 IF - TCF NEXTCORE # THE CORESPONDING CORE SET IS AVAILABLE. + TCF NEXTCORE # THE CORRESPONDING CORE SET IS AVAILABLE. NO.CORES DEC 6 TCF NEXTCORE # AN ACTIVE JOB HAS A POSITIVE PRIORITY # BUT A DORMANT JOB'S PRIORITY IS NEGATIVE @@ -319,7 +319,7 @@ JOBWAKE3 CAF COREINC ADS LOCCTR CCS EXECTEM2 TCF JOBWAKE4 - CS ONE # EXIT IF SLEEPIG JOB NOT FOUND. + CS ONE # EXIT IF SLEEPING JOB NOT FOUND. TS LOCCTR TCF ENDFIND diff --git a/Comanche055/FRESH_START_AND_RESTART.s b/Comanche055/FRESH_START_AND_RESTART.s index d0be47d..d0748c5 100644 --- a/Comanche055/FRESH_START_AND_RESTART.s +++ b/Comanche055/FRESH_START_AND_RESTART.s @@ -99,7 +99,7 @@ # # 1. INTIALIZE OUTBIT CHANNELS 11,12,13, AND 14 # 2. REPLACE ALL TASKS ON WAITLIST WITH ENDTASK -# 3. MAKE ALL EXECUTEVE REGISTERS AVAILABLE +# 3. MAKE ALL EXECUTIVE REGISTERS AVAILABLE # 4. MAKE ALL VAC AREAS AVAILABLE # 5. CLEAR DSKY REGISTERS # 6. ZERO NUMEROUS SWITCHES @@ -130,7 +130,7 @@ # B. ALARMS # # 1107 PHASE TABLE ERROR -# 1110 RESTART WTIH NO ACTIVE GROUPS +# 1110 RESTART WITH NO ACTIVE GROUPS # Page 183 BANK 10 diff --git a/Comanche055/INTERPRETER.s b/Comanche055/INTERPRETER.s index 20f716e..c7202da 100644 --- a/Comanche055/INTERPRETER.s +++ b/Comanche055/INTERPRETER.s @@ -2626,7 +2626,7 @@ NORMTEST CCS CYL # SEE IF ARGUMENT NOW NORMALIZED AT # Page 1187 # TRIGONOMETRIC FUNCTION PACKAGE. -# THE FOLLOWING TRIGONOMETRIC FUNCTIONS ARE AVAIALABLE AS INTERPRETIVE OPERATIONS: +# THE FOLLOWING TRIGONOMETRIC FUNCTIONS ARE AVAILABLE AS INTERPRETIVE OPERATIONS: # 1. SIN COMPUTES (1/2)SINE(2 PI MPAC). # 2. COS COMPUTES (1/2)COSINE(2 PI MPAC). # 3. ASIN COMPUTES (1/2PI)ARCSINE(2 MPAC). diff --git a/Comanche055/JET_SELECTION_LOGIC.s b/Comanche055/JET_SELECTION_LOGIC.s index f59608f..7eed1a9 100644 --- a/Comanche055/JET_SELECTION_LOGIC.s +++ b/Comanche055/JET_SELECTION_LOGIC.s @@ -365,7 +365,7 @@ NOACY CA RWORD1 # Y-TRANSLATION NOT ACCEPTED # FAILURES. IF THERE ARE BD FAILURES, Z-TRANSLATION COMMANDS WILL BE IGNORED, IN WHICH CASE THE ASTRONAUT SHOULD # SWITCH TO AC ROLL. # -# NOTE THAT IF ONE QUAD FAILS (E.G. B FAILED), Z-TRANSLATION IS STILL POSSIBLE AND THAT THE UNDESIREABLE ROLL +# NOTE THAT IF ONE QUAD FAILS (E.G. B FAILED), Z-TRANSLATION IS STILL POSSIBLE AND THAT THE UNDESIRABLE ROLL # INTRODUCED BY THIS TRANSLATION WILL BE COMPENSATED BY THE TWO AC ROLL JETS ACTUATED BY THE AUTOPILOT LOGIC. # # WORD MAKE UP....RTABLE @@ -386,7 +386,7 @@ NOACY CA RWORD1 # Y-TRANSLATION NOT ACCEPTED # THIS WORD MAY THEN BE ADDED TO THE WORD SELECTED FROM THE YZ-TRANSLATION TABLE, WHICH HAS THE SAME TYPE OF # CODING AS ABOVE, AND THE NET ROLL DETERMINED BY SHIFTING THE RESULTANT WORD RIGHT 8 PLACES AND SUBTRACTING FOUR. # -# THE WORD CORRESPONDING TO THE BD ROLL HAS A SIMILAR INTEPRETATION, EXCEPT THAT BITS 12, 13, 14 ARE CODED +# THE WORD CORRESPONDING TO THE BD ROLL HAS A SIMILAR INTERPRETATION, EXCEPT THAT BITS 12, 13, 14 ARE CODED # (AS ABOVE) TO GIVE THE NET ROLL TORQUE. # ROLL TRANS QUADFAIL BIAS diff --git a/Comanche055/KALCMANU_STEERING.s b/Comanche055/KALCMANU_STEERING.s index 2156c78..712a1ed 100644 --- a/Comanche055/KALCMANU_STEERING.s +++ b/Comanche055/KALCMANU_STEERING.s @@ -89,7 +89,7 @@ INCRDCDU TS KSPNDX TCF INCRDCDU # LOOP FOR THREE AXES RELINT -# COMPARE PRESENT TIME WTIH TIME TO TERMINATE MANEUVER +# COMPARE PRESENT TIME WITH TIME TO TERMINATE MANEUVER TMANUCHK TC TIMECHK TC POSTJUMP diff --git a/Comanche055/KEYRUPT_UPRUPT.s b/Comanche055/KEYRUPT_UPRUPT.s index cfa480d..8a138d9 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 PRECEEDED BY 16 BITS THE FIRST OF WHICH IS 1 FOLLOWED +# (IT IS RECOMMENDED THAT THE `ERROR LIGHT RESET' CODE IS PRECEDED 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/P20-P25.s b/Comanche055/P20-P25.s index d6303f3..f3e9779 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 REQURIES, NORMALLY CALLED BY P23 +# INPUT: NONE REQUIRES, 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 @@ -1407,7 +1407,7 @@ INITB STORE W +90D,1 # CLEAR 54 - 89 # # OMETATHSM = (REFSMMAT)(OMEGATH). # -# (10) OBTAIN GIMBAL ANGLE INCREMETNS FOR 0.1 SECOND. +# (10) OBTAIN GIMBAL ANGLE INCREMENTS FOR 0.1 SECOND. # # DTHETASM = (0.1)(OMEGATHSM) # @@ -1776,7 +1776,7 @@ FURST3 EQUALS 13,14,15 # CONSTANT FOR AUTOCK (OCT 70000). # ..... S22.1 ORBITAL NAVIGATION ROUTINE # MOD 1 # -# FUNCTONAL DESCRIPTION +# FUNCTIONAL DESCRIPTION # 1. UPDATE CSM STATE VECTOR # 2. UPDATE LANDMARK POSITION # 3. CONVERT W MATRIX FROM 9 TO 6 DIMENSIONS diff --git a/Comanche055/P32-P33_P72-P73.s b/Comanche055/P32-P33_P72-P73.s index 20889f6..2de37d6 100644 --- a/Comanche055/P32-P33_P72-P73.s +++ b/Comanche055/P32-P33_P72-P73.s @@ -42,7 +42,7 @@ # MOD BY WHITE, P. DATE 1 JUNE 67 # # PURPOSE -# (1) TO CALCULATE PARAMETERS ASSOCIATED WTIH THE FOLLOWING +# (1) TO CALCULATE PARAMETERS ASSOCIATED WITH THE FOLLOWING # CONCENTRIC FLIGHT PLAN MANEUVERS -- THE CO-ELLIPTIC SEQUENCE # INITIATION (CSI) MANEUVER AND THE CONSTANT DELTA ALTITUDE # (CDH) MANEUVER. diff --git a/Comanche055/P34-35_P74-75.s b/Comanche055/P34-35_P74-75.s index 84e6591..f7cd212 100644 --- a/Comanche055/P34-35_P74-75.s +++ b/Comanche055/P34-35_P74-75.s @@ -31,7 +31,7 @@ # Page 460 -# TRANSFER PHASE INITITIATION (TPI) PROGRAMS (P34 AND P74) +# TRANSFER PHASE INITIATION (TPI) PROGRAMS (P34 AND P74) # MOD NO -1 LOG SECTION -- P32-P35, P72-P75 # MOD BY WHITE, P. DATE: 1 JUNE 67 # diff --git a/Comanche055/P37_P70.s b/Comanche055/P37_P70.s index 544f574..0cbac46 100644 --- a/Comanche055/P37_P70.s +++ b/Comanche055/P37_P70.s @@ -44,7 +44,7 @@ # DESCRIPTION # A RETURN TO EARTH TRAJECTORY IS COMPUTED PROVIDED THE CSM IS OUTSIDE THE LUNAR SPHERE OF INFLUENCE AT THE # TIME OF IGNITION. INITIALLY A CONIC TRAJECTORY IS DETERMINED AND RESULTING IGNITION AND REENTRY PARAMETERS ARE -# DISPLAYED TO THE ASTRONAUT. THEN IF THE ASTRONAUT SO DESIRES, A PRECISION TRAJECTORY IS DETERMINED WTIH THE +# DISPLAYED TO THE ASTRONAUT. THEN IF THE ASTRONAUT SO DESIRES, A PRECISION TRAJECTORY IS DETERMINED WITH THE # RESULTING IGNITION AND REENTRY PARAMETERS DISPLAYED. UPON FINAL ACCEPTANCE BY THE ASTRONAUT, THE PROGRAM # COMPUTES AND STORES THE TARGET PARAMETERS FOR RETURN TO EARTH FOR USE BY SPS PROGRAM (P40) OR RCS PROGRAM (P41). # diff --git a/Comanche055/P51-P53.s b/Comanche055/P51-P53.s index baf2fba..073640f 100644 --- a/Comanche055/P51-P53.s +++ b/Comanche055/P51-P53.s @@ -318,7 +318,7 @@ 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 -# ORIENTATIION FOR P52 OR P54. +# ORIENTATION FOR P52 OR P54. # # LET: # RLS = LANDING SITE VECTOR IN REF COORDINATES @@ -1633,7 +1633,7 @@ MKDNCDR ECADR MARKDOWN # MOD. NO. 2 21 DEC 66 # MOD. BY STURLAUGSON # -# FUNCTIONAL DESCRIPTIION: +# FUNCTIONAL DESCRIPTION: # # TO PERFORM A SATISFACTORY NUMBER OF SIGHTING MARKS FOR THE REQUESTING PROGRAM (OR ROUTINE). SIGHTINGS # CAN BE MADE ON A STAR OR LANDMARK. WHEN THE CMC ACCEPTS A MARK IT RECORDS AND STORES 5 ANGLES (3 ICDUS AND 2 @@ -1682,7 +1682,7 @@ R53A CA MARKINDX # NUMBER OF MARKS CADR OPTSTALL TC CURTAINS INDEX MARKSTAT - CCS QPRET # NUMNBER OF MARKS ACTUALLY DONE + CCS QPRET # NUMBER OF MARKS ACTUALLY DONE TCF R53B TCF +2 # ZERO TCF +1 # CCS HOLE diff --git a/Comanche055/P61-P67.s b/Comanche055/P61-P67.s index ced25b3..932d31c 100644 --- a/Comanche055/P61-P67.s +++ b/Comanche055/P61-P67.s @@ -343,7 +343,7 @@ POSECADR 2CADR CM/POSE # MOD BY: R. HIRSCHKOP # MOD NO: 2 MOD BY: RR BAIRNSFATHER DATE: 8 MAY 68 REVISED COMMENTS FOR COLOSSUS # FUNCTION: 1. TO START ENTRY GUIDANCE AT .05G SELECTING ROLL ATTITUDE, CONSTANT DRAG LEVEL, AND -# DRAG THRESHHOLD, KA, WHICH ARE KEYED TO THE .05G POINT. +# DRAG THRESHOLD, KA, WHICH ARE KEYED TO THE .05G POINT. # 2. SELECT FINAL PHASE P67 IF V < 27000 FPS WHEN .2G OCCURS. # 3. ITERATE FOR UP-CONTROL SOLUTION P65 IF V > 27000 FPS AND IF ALTITUDE RATE AND DRAG # LEVEL CONDITIONS ARE SATISFIED. ENTER P65 WHEN CONSTANT DRAG CONTROLLER HAS BROUGHT RANGE @@ -950,7 +950,7 @@ DUMPFISH GOTO # MOD NO: 2 MOD BY: RR BAIRNSFATHER DATE: 21 NOV 67 VARIABLE MU ADDED. # MOD NO: 3 MOD BY: RR BAIRNSFATHER DATE: 21 MAR 68 ACCEPT DIFFERENT EARTH/MOON SCALE # -# FUNCTONAL DESCRIPTION: EARTH CENTERED VIS VIVA CALCULATION OF TERMINAL VELOCITY AND GAMMA (REL TO +# FUNCTIONAL DESCRIPTION: EARTH CENTERED VIS VIVA CALCULATION OF TERMINAL VELOCITY AND GAMMA (REL TO # HORIZONTAL) GIVEN THE SCALAR QUANTITIES: PRESENT RADIUS AND VELOCITY AND THE TERMINAL RADIUS. # THE USER MUST APPEND PROPER SIGN TO GAMMA, SINCE IT IS CALCULATED AS A POSITIVE NUMBER. # THE EQUATIONS ARE diff --git a/Comanche055/P76.s b/Comanche055/P76.s index 9adb9c8..5584d91 100644 --- a/Comanche055/P76.s +++ b/Comanche055/P76.s @@ -37,7 +37,7 @@ # BEEN TRANSFORMED FROM LV TO REF COSYS). USING INTEGRVS, THE PROGRAM THEN INTEGRATES THE OTHER # VEHICLE STATE VECTOR TO THE STATE VECTOR OF THIS VEHICLE, THUS INSURING THAT THE W-MATRIX AND BOTH VEHICLE # STATES CORRESPOND TO THE SAME TIME. -# 3) ERASABLE INIITIALIZATION REQUIRED -- NONE. +# 3) ERASABLE INITIALIZATION REQUIRED -- NONE. # 4) CALLING SEQUENCES AND EXIT MODES -- CALLED BY ASTRONAUT REQUEST THRU DSKY V 37 E 76E. # EXITS BY TCF ENDOFJOB. # 5) OUTPUT -- OTHER VEHICLE STATE VECTOR INTEGRATED TO TIG AND INCREMENTED BY DELTA V IN REF COSYS. diff --git a/Comanche055/PHASE_TABLE_MAINTENANCE.s b/Comanche055/PHASE_TABLE_MAINTENANCE.s index 247b4bd..0ffc0d0 100644 --- a/Comanche055/PHASE_TABLE_MAINTENANCE.s +++ b/Comanche055/PHASE_TABLE_MAINTENANCE.s @@ -99,7 +99,7 @@ DSPMMJOB EQUALS DSPMMJB # WHERE EACH LETTER OR NUMBER STANTS FOR A BIT. THE G'S STAND FOR THE GROUP, OCTAL 1-7, THE P'S FOR THE PHASE, # OCTAL 0 - 127. 0'S MUST BE 0. IF ONE WISHES TO HAVE THE TBASE OF GROUP G TO BE SET AT THIS TIME, # T IS SET TO 1, OTHERWISE IT IS SET TO 0. SIMILARLY IF ONE WISHES TO SET LONGBASE, THEN L IS SET TO 1, OTHERWISE -# IT IS SET TO 0. SOME EXAMLES, +# IT IS SET TO 0. SOME EXAMPLES, # TC PHASCHNG # THIS WILL CAUSE GROUP 3 TO BE SET TO 0, # OCT 00003 # MAKING GROUP 3 INACTIVE # diff --git a/Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s b/Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s index 266b32b..b1a15b4 100644 --- a/Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s +++ b/Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s @@ -84,7 +84,7 @@ # Page 308 # 2) EXTENDED VERBS TO TO THE EXTENDED VERB FAN AS PART OF THE # PINBALL EXECUTIVE JOB WITH PRIORITY 30000. IT IS THE -# RESPONSIBILITY OF THE EXTEDED VERB CALLED TO EVENTUALLY +# RESPONSIBILITY OF THE EXTENDED VERB CALLED TO EVENTUALLY # CHANGE PRIORITY (IF NECESSARY) AD DO AN ENDOFJOB. # ALSO PINBALL IS A NOVAC JOB. EBANK SET FOR COMMON. # 3) VERB 37. CHANGE OF PROGRAM (MAJOR MODE) CALLS `V37' IN THE @@ -1128,7 +1128,7 @@ GODSPALM TC POSTJUMP # S'S ARE THE SF ROUTINE 1 CODE NUMBER # # IN OCTAL DISPLAY AND LOAD (OCT OR DEC) VERBS, EXCLUDE USE OF VERBS WHOSE -# COMPONENT NUMBER IS GREATER THAN THE NUMBER OF COMONENTS IN NOUN. +# COMPONENT NUMBER IS GREATER THAN THE NUMBER OF COMPONENTS IN NOUN. # (ALL MACHINE ADDRESS TO BE SPECIFIED NOUNS ARE 3 COMPONENT.) # # IN MULTI-COMPONENT LOAD VERBS, NO MIXING OF OCTAL AND DECIMAL DATA @@ -2817,7 +2817,7 @@ SETVAC CAF TCFINDVC # VBRQWAIT ENTERS REQUEST TO WAITLIST FOR ANY ADDRESS WITH ANY DELAY. # IT DOES ENDOFJOB AFTER ENTERING REQUEST. DISPLAY SYST IS RELEASED. -# IT ASSUMES NOUN 26 HAS BEEN PRELOADED WTIH +# IT ASSUMES NOUN 26 HAS BEEN PRELOADED WITH # COMPONENT 1 DELAY (LOW BITS) # COMPONENT 2 TASK ADRES (12 BIT) # COMPONENT 3 BBCON @@ -2921,11 +2921,11 @@ ENDRELDS EQUALS # PLACE 0VVVVVVVNNNNNNN INTO A. # V'S ARE THE 7-BIT VERB CODE. N'S ARE THE 7-BIT NOUN CODE. # -# IF NVSUB IS CALLED WTIH THE FOLLOWING NEGATIVE NUMBERS (RATHER THAN THE +# IF NVSUB IS CALLED WITH THE FOLLOWING NEGATIVE NUMBERS (RATHER THAN THE # VERB-NOUN CODE) IN A, THEN THE DISPLAY IS BLANKED AS FOLLOWS --- # -4 FULL BLANK, -3 LEAVE MODE, -2 LEAVE MODE AND VERB, -1 BLANK R'S ONLY. # -# NVSUB CAN BE USED WTIH MACHINE CADR TO BE SPECIFIED BY PLACING THE CADR INTO +# NVSUB CAN BE USED WITH MACHINE CADR TO BE SPECIFIED BY PLACING THE CADR INTO # MPAC+2 BEFORE THE STANDARD NVSUB CALL. # # NVSUB RETURNS TO 2+ CALLING LOC AFTER PERFORMING TASK, IF DISPLAY @@ -2942,7 +2942,7 @@ ENDRELDS EQUALS # THE DISPLAY SYSTEM IS BLOCKED BY THE DEPRESSION OF ANY # KEY, EXCEPT ERROR LIGHT RESET. # IT IS RELEASED BY THE KEY RELEASE BUTTON, ALL EXTENDED VERBS, -# PROCED WITOHOUT DATA, TERMINATE, RESEQUENCE, INITIALIZE EXECUTIVE, +# PROCEED WITHOUT DATA, TERMINATE, RESEQUENCE, INITIALIZE EXECUTIVE, # RECALL PART OF RECALTST IF ENDIDLE WAS USED, # VB = REQUEST EXECUTIVE, VB = REQUEST WAITLIST, # MONITOR SET UP. @@ -2960,7 +2960,7 @@ ENDRELDS EQUALS # (SIMILARLY FOR PLEASE MARK). FIRST PLACE THE CODED NUMBER FOR WHAT # ACTION IS DESIRED OF OPERATOR INTO THEREGISTERS REFERRED TO BY THE # `CHECKLIST' NOUN. GO TO NVSUB WITH A DISPLAY VERB AND THE `CHECKLIST' -# NOUN. GO TO NVSUB AGAIN WTIH THE `PLEASE PERFORM' VERB AND ZEROS IN THE +# NOUN. GO TO NVSUB AGAIN WITH THE `PLEASE PERFORM' VERB AND ZEROS IN THE # LOW 7 BITS. THIS `PASTES UP' THE `PLEASE PERFORM' VERB INTO THE VERB # LIGHTS. # diff --git a/Comanche055/PINBALL_NOUN_TABLES.s b/Comanche055/PINBALL_NOUN_TABLES.s index 8fbd97a..3b9bc7e 100644 --- a/Comanche055/PINBALL_NOUN_TABLES.s +++ b/Comanche055/PINBALL_NOUN_TABLES.s @@ -120,7 +120,7 @@ # (WHICH ARE IN A SEPARATE BANK FROM THE REST OF PINBALL). THESE READING # ROUTINES ARE IN THE SAME BANK AS THE TABLES. THEY ARE CALLED BY DXCH Z. -# LODNNTAB LOADS NNADTEM WTIH THE NNADTAB ENTRY, NNTYPTEM WITH THE +# LODNNTAB LOADS NNADTEM WITH THE NNADTAB ENTRY, NNTYPTEM WITH THE # NNTYPTAB ENTRY. IF THE NOUN IS MIXED, IDADITEM IS LOADED WITH THE FIRST # IDADDTAB ENTRY, IDAD2TEM THE SECOND IDADDTAB ENTRY, IDAD3TEM THE THIRD # IDADDTAB ENTRY, RUTMXTEM WITH THE RUTMXTAB ENTRY. MIXBR IS SET FOR @@ -165,7 +165,7 @@ LODNLV DXCH IDAD2TEM # PUT RETURN INFO INTO A, L. MIXCON = OCT50 # FIRST MIXED NOUN =40. (DEC 40) -# GTSFOUT LOADS SFTEMP1, SFTEMP2 WTIH THE DP SFOUTAB ENTRIES. +# GTSFOUT LOADS SFTEMP1, SFTEMP2 WITH THE DP SFOUTAB ENTRIES. # Page 271 GTSFOUT DXCH SFTEMP1 # 2X (SFCONUM) ARRIVES IN SFTEMP1. @@ -214,7 +214,7 @@ NNADTAB OCT 00000 # 00 NOT IN USE OCT 00000 # 23 SPARE ECADR DSPTEM2 +1 # 24 DELTA TIME FOR AGC CLOCK (HRS,MIN,SEC) ECADR DSPTEM1 # 25 CHECKLIST - # (USED WTIH PLEASE PERFORM ONLY) + # (USED WITH PLEASE PERFORM ONLY) ECADR DSPTEM1 # 26 PRIO/DELAY, ADRES, BBCON ECADR SMODE # 27 SELF TEST ON/OFF SWITCH # Page 272 @@ -588,7 +588,7 @@ SFOUTAB OCT 05174 # WHOLE, DP TIME (SEC) OCT 15340 OCT 01031 # VELOCITY3 (POINT BETWN BITS 7-8) OCT 21032 - OCT 34631 # ELEVATION DETREES + OCT 34631 # ELEVATION DEGREES OCT 23146 OCT 14340 # TRIM DEGREES OCT 24145 diff --git a/Comanche055/R60_62.s b/Comanche055/R60_62.s index f436b2b..26b3b83 100644 --- a/Comanche055/R60_62.s +++ b/Comanche055/R60_62.s @@ -159,7 +159,7 @@ V06N18 VN 0618 # BEGINNING WITH THE LOCATION CALLED SCAXIS. THE COMPONENTS OF THIS VECTOR ARE GIVEN IN SPACECRAFT COORDINATES. # THE DIRECTION IN WHICH THIS AXIS IS TO BE POINTED MUST APPEAR AS A HALF UNIT DOUBLE PRECISION VECTOR IN # SUCCESSIVE LOCATIONS OF ERASABLE MEMORY BEGINNING WITH THE ADDRESS CALLED POINTVSM. THE COMPONENTS OF THIS -# VECTOR ARE GIVEN IN STABLE MEMBER COORDINATES. WITH THIS INFORMTION VECPOINT COMPUTES A SET OF THREE GIMBAL +# VECTOR ARE GIVEN IN STABLE MEMBER COORDINATES. WITH THIS INFORMATION VECPOINT COMPUTES A SET OF THREE GIMBAL # ANGLES (2'S COMPLEMENT) CORRESPONDING TO THE CROSS-PRODUCT ROTATION BETWEEN SCAXIS AND POINTVSM AND STORES THEM # IN T(MPAC) BEFORE RETURNING TO THE CALLER. # diff --git a/Comanche055/RCS-CSM_DIGITAL_AUTOPILOT.s b/Comanche055/RCS-CSM_DIGITAL_AUTOPILOT.s index 20a7872..31c55f6 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) OCCURANCE OF RHC COMMANDS +# 2) OCCURRENCE OF RHC COMMANDS # 3) FREE MODE # 4) SWITCH OVER TO ATTITUDE HOLD FROM AUTO # WHILE DOING AUTOMATIC STEERING (IN THIS CASE diff --git a/Comanche055/RT8_OP_CODES.s b/Comanche055/RT8_OP_CODES.s index c823fdb..003fbf2 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 UNCORRECT AND IN MSU. + INDEX A # OVERFLOW INCORRECT AND IN MSU. CAF LIMITS ADS MPAC TC Q diff --git a/Comanche055/STABLE_ORBIT.s b/Comanche055/STABLE_ORBIT.s index c1a21d5..b5c972c 100644 --- a/Comanche055/STABLE_ORBIT.s +++ b/Comanche055/STABLE_ORBIT.s @@ -86,7 +86,7 @@ # (6) DELVTPI MAGNITUDE OF DELTA V AT SOI (SOR) TIME # (7) DELVTPF MAGNITUDE OF DELTA V AT INTERCEPT TIME # (8) DELTA VELOCITY AT SOI (AND SOR) - LOCAL VERTICAL -# CORDINATES +# COORDINATES # # SUBROUTINES USED # diff --git a/Comanche055/SXTMARK.s b/Comanche055/SXTMARK.s index a6ad217..4e520a8 100644 --- a/Comanche055/SXTMARK.s +++ b/Comanche055/SXTMARK.s @@ -520,7 +520,7 @@ REJECT3 CAF LOW9 # DECREMENT POINTER TO REJECT MARK TC RESUME # Page 232 -# PROGRAM DESCRIPTON MKVB51 AND MKVB50 +# PROGRAM DESCRIPTION MKVB51 AND MKVB50 # # AUTHOR: BARNERT DATE: 2-15-67 MOD: 0 # PURPOSE: FLASH V51N70,V51N43, OR V51 TO REQUEST MARKING, diff --git a/Comanche055/T4RUPT_PROGRAM.s b/Comanche055/T4RUPT_PROGRAM.s index e36a18d..db620f5 100644 --- a/Comanche055/T4RUPT_PROGRAM.s +++ b/Comanche055/T4RUPT_PROGRAM.s @@ -577,7 +577,7 @@ NXTFL33 CCS RUPTREG2 # PROCESS POSSIBLE ADDITIONAL CHANGES. # # ERASABLE INITIALIZATION: # 1) FRESH START OR RESTART WITH NO GROUPS ACTIVE: C(CDUZ) = 0, IMODES30 BIT 6 = 0, IMODES33 BIT 1 = 0. -# 2) RESTART WTIH GROUPS ACTIVE: SAME AS FRESH START EXCEPT C(CDUZ) NOT CHANGED SO GIMBAL MONITOR +# 2) RESTART WITH GROUPS ACTIVE: SAME AS FRESH START EXCEPT C(CDUZ) NOT CHANGED SO GIMBAL MONITOR # PROCEEDS AS BEFORE. # # ALARMS: 1) MGA REGION (2) CAUSES GIMBAL LOCK LAMP TO BE LIT. @@ -863,7 +863,7 @@ IMUOP2 CAF BIT2 # SEE IF FAILED ISS TURN-ON SEQ IN PROG. # # JOBS OR TASKS INITIATED: NONE. # -# SUBROUTINES CALLED: 1) SETISSW, AND 2) ALARM (SEE FUNCITONAL DESCRIPTION). +# SUBROUTINES CALLED: 1) SETISSW, AND 2) ALARM (SEE FUNCTIONAL DESCRIPTION). # # ERASABLE INITIALIZATION: SEE IMUMON FOR INITIALIZATION OF IMODES30. THE RELEVANT BITS ARE 5, 7, 8, 9, AND 10. # diff --git a/Comanche055/TIME_OF_FREE_FALL.s b/Comanche055/TIME_OF_FREE_FALL.s index 83714b0..9e96c71 100644 --- a/Comanche055/TIME_OF_FREE_FALL.s +++ b/Comanche055/TIME_OF_FREE_FALL.s @@ -31,7 +31,7 @@ # Page 1373 # THE TFF SUBROUTINES MAY BE USED IN EITHER EARTH OR MOON CENTERED COORDINATES. THE TFF ROUTINES NEVER # KNOW WHICH ORIGIN APPLIES. IT IS THE USER WHO KNOWS, AND WHO SUPPLIES RONE, VONE, AND 1/SQRT(MU) AT THE -# APPROPIRATE SCALE LEVEL FOR THE PROPER PRIMARY BODY. +# APPROPRIATE SCALE LEVEL FOR THE PROPER PRIMARY BODY. # # EARTH ORIGIN POSITION -29 METERS # VELOCITY -7 METERS/CENTISECOND @@ -81,7 +81,7 @@ NRMAG = 32D # PRESENT RADIUS M E: (-29+NR) TFFX = 34D # TFFTEM = 36D # TEMPORARY # Page 1374 -# REGISTERS S1, S2 ARE UNTOUCED BY ANY TFF SUBROUTINE +# REGISTERS S1, S2 ARE UNTOUCHED BY ANY TFF SUBROUTINE # INDEX REGISTERS X1, X2 ARE USED BY ALL TFF SUBROUTINES. THEY ARE ESTAB- # LISHED IN TFF/CONIC AND MUST BE PRESERVED BETWEEN CALLS TO SUBSEQUENT # SUBROUTINES. @@ -341,7 +341,7 @@ DUMPRPRA RVQ # 2 3 2 # 1/3 - X/5 + X /7 - X /8 ... (X < 1.0) # -# CALLING SEQUENC: TIME TO RTERM TIME TO PERIGEE +# CALLING SEQUENCE: TIME TO RTERM TIME TO PERIGEE # CALL CALL # CALCTFF CALCTPER # C(MPAC) = TERMNL RAD M C(MPAC) = PERIGEE RAD M diff --git a/Comanche055/TVCEXECUTIVE.s b/Comanche055/TVCEXECUTIVE.s index 578ab5b..cc59ea5 100644 --- a/Comanche055/TVCEXECUTIVE.s +++ b/Comanche055/TVCEXECUTIVE.s @@ -100,7 +100,7 @@ ROLLPREP CAE CDUX # UPDATE ROLL LADDERS (NO NEED TO RESTART- XCH OGANOW # PROTECT, SINCE ROLL DAPS RE-START) XCH OGAPAST - CAE OGAD # PREPARE ROLL FDAI NEEDLE WTIH FLY-TO + CAE OGAD # PREPARE ROLL FDAI NEEDLE WITH FLY-TO EXTEND # ERROR (COMMAND - MEASURED) MSU OGANOW TS AK # FLY-TO OGA ERROR, SC.AT B-1 REVS diff --git a/Comanche055/TVCRESTARTS.s b/Comanche055/TVCRESTARTS.s index da4d43f..bf09087 100644 --- a/Comanche055/TVCRESTARTS.s +++ b/Comanche055/TVCRESTARTS.s @@ -122,7 +122,7 @@ # # OTHER INTERFACES....DOTVCON AND RCSDAPON (T5 BITS), ELRSKIP (CALLS IT) # -# ERASABLE ININTIALIZATION REQUIRED.... +# ERASABLE INITIALIZATION REQUIRED.... # # *T5 BITS (1,0), TVCPHASE (-2,-1,0,1,2,3), TVCEXPHS (1 THRU 6) # *TVC DAP VARIABLES diff --git a/Comanche055/TVCSTROKETEST.s b/Comanche055/TVCSTROKETEST.s index 1844343..cd7ad15 100644 --- a/Comanche055/TVCSTROKETEST.s +++ b/Comanche055/TVCSTROKETEST.s @@ -41,8 +41,8 @@ # IMMEDIATELY. IF NOT CSM/LM, PROGRAM EXITS WITH NO ACTION. # HACK (STROKE TEST) GENERATES THE WAVEFORM BY DUMPING PULSE BURSTS # OF PROPER SIGN AND IN PROPER SEQUENCE DIRECTLY INTO -# TVCPITCH, WORKING IN CONJUNCITON WITH BOTH PITCH AND YAW -# TVC DAPS, WITH INTERMEDIAT WAITLIST CALLS. NOTE, HOWEVER +# TVCPITCH, WORKING IN CONJUNCTION WITH BOTH PITCH AND YAW +# TVC DAPS, WITH INTERMEDIATE WAITLIST CALLS. NOTE, HOWEVER # THAT THE STROKE TEST IS PERFORMED ONLY IN THE PITCH AXIS. # AN EXAMPLE WAVEFORM IS GIVEN BELOW, TO DEMONSTRATE STROKE- # TEST PARAMETER SELECTION. diff --git a/Comanche055/UPDATE_PROGRAM.s b/Comanche055/UPDATE_PROGRAM.s index 3b86857..0ae6a85 100644 --- a/Comanche055/UPDATE_PROGRAM.s +++ b/Comanche055/UPDATE_PROGRAM.s @@ -122,7 +122,7 @@ # V33E VERB 33 TO SIGNAL THAT THE STATE VECTOR IS READY TO BE STORED. # # 2. REFSMMAT (ALL DATA ENTRIES IN OCTAL) -# ENTRIES DATA DEFINITITIONS SCALE FACTORS: +# ENTRIES DATA DEFINITIONS SCALE FACTORS: # Page 1499 # V71E CONTIGUOUS BLOCK UPDATE VERB # 24E NUMBER OF COMPONENTS FOR REFSMMAT UPDATE diff --git a/Luminary099/AOTMARK.s b/Luminary099/AOTMARK.s index e83936a..ad6d09a 100644 --- a/Luminary099/AOTMARK.s +++ b/Luminary099/AOTMARK.s @@ -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 diff --git a/Luminary099/BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s b/Luminary099/BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s index ac7c532..570975a 100644 --- a/Luminary099/BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s +++ b/Luminary099/BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s @@ -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. # ******************************** diff --git a/Luminary099/DOWN_TELEMETRY_PROGRAM.s b/Luminary099/DOWN_TELEMETRY_PROGRAM.s index 1a72d0a..889bb49 100644 --- a/Luminary099/DOWN_TELEMETRY_PROGRAM.s +++ b/Luminary099/DOWN_TELEMETRY_PROGRAM.s @@ -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 diff --git a/Luminary099/FINDCDUW--GUIDAP_INTERFACE.s b/Luminary099/FINDCDUW--GUIDAP_INTERFACE.s index 637f04e..3e09042 100644 --- a/Luminary099/FINDCDUW--GUIDAP_INTERFACE.s +++ b/Luminary099/FINDCDUW--GUIDAP_INTERFACE.s @@ -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 diff --git a/Luminary099/IMU_PERFORMANCE_TESTS_4.s b/Luminary099/IMU_PERFORMANCE_TESTS_4.s index ebb7849..8776338 100644 --- a/Luminary099/IMU_PERFORMANCE_TESTS_4.s +++ b/Luminary099/IMU_PERFORMANCE_TESTS_4.s @@ -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 diff --git a/Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s b/Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s index eaab1a2..8019b5d 100644 --- a/Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s +++ b/Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s @@ -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. diff --git a/Luminary099/P-AXIS_RCS_AUTOPILOT.s b/Luminary099/P-AXIS_RCS_AUTOPILOT.s index 41b0cfd..8a11483 100644 --- a/Luminary099/P-AXIS_RCS_AUTOPILOT.s +++ b/Luminary099/P-AXIS_RCS_AUTOPILOT.s @@ -964,7 +964,7 @@ HEADTJET CA ZERO -FOURDEG DEC -.08888 # Page 1440 -# JET POLICY CONTSTRUCTION SUBROUTINE +# JET POLICY CONSTRUCTION SUBROUTINE # # INPUT: ROTINDEX, NUMBERT # diff --git a/Luminary099/P30_P37.s b/Luminary099/P30_P37.s index 34f9ffc..dca84cc 100644 --- a/Luminary099/P30_P37.s +++ b/Luminary099/P30_P37.s @@ -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 ** # diff --git a/Luminary099/P32-P35_P72-P75.s b/Luminary099/P32-P35_P72-P75.s index 9f1c7b8..a6856dd 100644 --- a/Luminary099/P32-P35_P72-P75.s +++ b/Luminary099/P32-P35_P72-P75.s @@ -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. diff --git a/Luminary099/P70-P71.s b/Luminary099/P70-P71.s index 933f970..edd7286 100644 --- a/Luminary099/P70-P71.s +++ b/Luminary099/P70-P71.s @@ -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 diff --git a/Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s b/Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s index f3265b5..7a7f1a4 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 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 # diff --git a/Luminary099/RTB_OP_CODES.s b/Luminary099/RTB_OP_CODES.s index ad480e2..76cb1a6 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 UNCORRECT AND IN MSU. + INDEX A # OVERFLOW INCORRECT AND IN MSU. CAF LIMITS ADS MPAC TC Q diff --git a/Luminary099/SERVICER.s b/Luminary099/SERVICER.s index c3a8f2f..0d75df2 100644 --- a/Luminary099/SERVICER.s +++ b/Luminary099/SERVICER.s @@ -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/ diff --git a/Luminary099/THE_LUNAR_LANDING.s b/Luminary099/THE_LUNAR_LANDING.s index 775f08d..930a4d0 100644 --- a/Luminary099/THE_LUNAR_LANDING.s +++ b/Luminary099/THE_LUNAR_LANDING.s @@ -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. diff --git a/Luminary099/THROTTLE_CONTROL_ROUTINES.s b/Luminary099/THROTTLE_CONTROL_ROUTINES.s index c43b9c9..bb24381 100644 --- a/Luminary099/THROTTLE_CONTROL_ROUTINES.s +++ b/Luminary099/THROTTLE_CONTROL_ROUTINES.s @@ -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 # diff --git a/Luminary099/TJET_LAW.s b/Luminary099/TJET_LAW.s index 9b15a67..c7d7fe8 100644 --- a/Luminary099/TJET_LAW.s +++ b/Luminary099/TJET_LAW.s @@ -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: diff --git a/Luminary099/TRIM_GIMBAL_CNTROL_SYSTEM.s b/Luminary099/TRIM_GIMBAL_CNTROL_SYSTEM.s index 226d0b5..e33e031 100644 --- a/Luminary099/TRIM_GIMBAL_CNTROL_SYSTEM.s +++ b/Luminary099/TRIM_GIMBAL_CNTROL_SYSTEM.s @@ -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. From afa13e736438957d7645b17f00b9db7c8d1dc76e Mon Sep 17 00:00:00 2001 From: oldmud0 Date: Mon, 11 Jul 2016 07:35:15 -0500 Subject: [PATCH 2/3] Fix all the typos! (and add some too) --- Comanche055/ALARM_AND_ABORT.s | 2 +- .../ASSEMBLY_AND_OPERATION_INFORMATION.s | 6 ++-- Comanche055/CM_BODY_ATTITUDE.s | 2 +- Comanche055/CONIC_SUBROUTINES.s | 8 ++--- Comanche055/CSM_GEOMETRY.s | 6 ++-- Comanche055/DISPLAY_INTERFACE_ROUTINES.s | 8 ++--- Comanche055/DOWN-TELEMETRY_PROGRAM.s | 2 +- Comanche055/DOWNLINK_LISTS.s | 2 +- Comanche055/ENTRY_LEXICON.s | 2 +- Comanche055/ERASABLE_ASSIGNMENTS.s | 14 ++++----- Comanche055/EXECUTIVE.s | 2 +- Comanche055/EXTENDED_VERBS.s | 4 +-- Comanche055/FRESH_START_AND_RESTART.s | 8 ++--- Comanche055/GIMBAL_LOCK_AVOIDANCE.s | 2 +- .../GROUND_TRACKING_DETERMINATION_PROGRAM.s | 2 +- Comanche055/IMU_CALIBRATION_AND_ALIGNMENT.s | 10 +++---- Comanche055/IMU_MODE_SWITCHING_ROUTINES.s | 2 +- Comanche055/INTER-BANK_COMMUNICATION.s | 2 +- Comanche055/INTERPRETER.s | 30 +++++++++---------- Comanche055/INTERRUPT_LEAD_INS.s | 2 +- Comanche055/KALCMANU_STEERING.s | 2 +- Comanche055/KEYRUPT_UPRUPT.s | 2 +- .../LUNAR_AND_SOLAR_EPHEMERIDES_SUBROUTINES.s | 2 +- Comanche055/MEASUREMENT_INCORPORATION.s | 2 +- Comanche055/ORBITAL_INTEGRATION.s | 2 +- Comanche055/P20-P25.s | 4 +-- Comanche055/P30-P37.s | 2 +- Comanche055/P32-P33_P72-P73.s | 4 +-- Comanche055/P34-35_P74-75.s | 10 +++---- Comanche055/P40-P47.s | 2 +- Comanche055/P51-P53.s | 4 +-- Comanche055/P61-P67.s | 2 +- Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s | 6 ++-- Comanche055/PINBALL_NOUN_TABLES.s | 2 +- Comanche055/R30.s | 6 ++-- Comanche055/R31.s | 2 +- Comanche055/RCS-CSM_DIGITAL_AUTOPILOT.s | 2 +- Comanche055/RESTARTS_ROUTINE.s | 2 +- Comanche055/RESTART_TABLES.s | 2 +- Comanche055/RT8_OP_CODES.s | 8 ++--- Comanche055/SERVICER207.s | 4 +-- Comanche055/SERVICE_ROUTINES.s | 2 +- Comanche055/SXTMARK.s | 2 +- Comanche055/SYSTEM_TEST_STANDARD_LEAD_INS.s | 2 +- Comanche055/T4RUPT_PROGRAM.s | 6 ++-- Comanche055/TIME_OF_FREE_FALL.s | 2 +- Comanche055/TPI_SEARCH.s | 2 +- Comanche055/TVCDAPS.s | 2 +- Comanche055/TVCEXECUTIVE.s | 2 +- Comanche055/TVCRESTARTS.s | 2 +- Comanche055/TVCROLLDAP.s | 4 +-- Comanche055/UPDATE_PROGRAM.s | 2 +- Comanche055/WAITLIST.s | 6 ++-- Luminary099/AOSTASK_AND_AOSJOB.s | 2 +- Luminary099/AOTMARK.s | 2 +- Luminary099/ASCENT_GUIDANCE.s | 8 ++--- Luminary099/ATTITUDE_MANEUVER_ROUTINE.s | 8 ++--- .../BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s | 4 +-- Luminary099/DAPIDLER_PROGRAM.s | 2 +- Luminary099/DOWN_TELEMETRY_PROGRAM.s | 2 +- Luminary099/FINDCDUW--GUIDAP_INTERFACE.s | 2 +- Luminary099/FLAGWORD_ASSIGNMENTS.s | 4 +-- .../INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.s | 4 +-- Luminary099/LAMBERT_AIMPOINT_GUIDANCE.s | 2 +- Luminary099/LANDING_ANALOG_DISPLAYS.s | 2 +- Luminary099/LEM_GEOMETRY.s | 2 +- .../LUNAR_LANDING_GUIDANCE_EQUATIONS.s | 4 +-- Luminary099/P-AXIS_RCS_AUTOPILOT.s | 2 +- Luminary099/P12.s | 2 +- Luminary099/P32-P35_P72-P75.s | 8 ++--- Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s | 2 +- Luminary099/RADAR_LEADIN_ROUTINES.s | 2 +- Luminary099/RCS_FAILURE_MONITOR.s | 4 +-- Luminary099/RTB_OP_CODES.s | 2 +- Luminary099/SERVICER.s | 2 +- Luminary099/SPS_BACK-UP_RCS_CONTROL.s | 2 +- Luminary099/THROTTLE_CONTROL_ROUTINES.s | 2 +- Luminary099/TJET_LAW.s | 2 +- 78 files changed, 150 insertions(+), 150 deletions(-) diff --git a/Comanche055/ALARM_AND_ABORT.s b/Comanche055/ALARM_AND_ABORT.s index bd483b2..de6ba0f 100644 --- a/Comanche055/ALARM_AND_ABORT.s +++ b/Comanche055/ALARM_AND_ABORT.s @@ -22,7 +22,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.s b/Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.s index 62c2db8..8084ace 100644 --- a/Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.s +++ b/Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.s @@ -121,7 +121,7 @@ # UPDATE PROGRAM # RTB OP CODES # SYMBOL TABLE LISTING -# UNREFERANCES SYMBOL LISTING +# UNREFERENCED SYMBOL LISTING # ERASABLE & EQUALS CROSS-REFERENCE TABLE # SUMMARY OF SYMBOL TABLE LISTINGS # MEMORY TYPE & AVAILABILITY DISPLAY @@ -254,11 +254,11 @@ # SCALE TYPE L (MIN/SEC) OR PP (2 INTEGERS). # IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22, OR 23 -# MAY BE USED TO LOAD ANY O FTHE NOUN'S COMPONENTS WHICH ARE NOT OF THE +# MAY BE USED TO LOAD ANY OF THE NOUN'S COMPONENTS WHICH ARE NOT OF THE # ABOVE SCALE TYPES. # THE 'DEC ONLY' RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON -# EVERY COMPONENT IN THENOUN. (NOT THAT 'NO LOAD' IMLIES 'DEC ONLY'.) +# EVERY COMPONENT IN THE NOUN. (NOT THAT 'NO LOAD' IMLIES 'DEC ONLY'.) # NORMAL NOUNS COMPONENTS SCALE & DECIMAL POINT RESTRICTION # diff --git a/Comanche055/CM_BODY_ATTITUDE.s b/Comanche055/CM_BODY_ATTITUDE.s index 048a601..9761c84 100644 --- a/Comanche055/CM_BODY_ATTITUDE.s +++ b/Comanche055/CM_BODY_ATTITUDE.s @@ -19,7 +19,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/CONIC_SUBROUTINES.s b/Comanche055/CONIC_SUBROUTINES.s index c10fc10..d2972fe 100644 --- a/Comanche055/CONIC_SUBROUTINES.s +++ b/Comanche055/CONIC_SUBROUTINES.s @@ -69,7 +69,7 @@ # FUNCTIONAL DESCRIPTION -- # THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR AND THE DESIRED TRANSFER TIME THROUGH WHICH THE STATE IS TO # BE UPDATED ALONG A CONIC TRAJECTORY, COMPUTES THE NEW, UPDATED STATE VECTOR. THE TRAJECTORY MAY BE ANY CONIC -# SECTION -- CIRCULAR, ELLIPTIC, PARABOLIC, HYPERPOLIC, OR RECTILINEAR WITH RESPECT TO THE EARTH OR THE MOON. THE +# SECTION -- CIRCULAR, ELLIPTIC, PARABOLIC, HYPERBOLIC, OR RECTILINEAR WITH RESPECT TO THE EARTH OR THE MOON. THE # USE OF THE SUBROUTINE CAN BE EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT # INTRODUCING ANY CODING CHANGES, ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY. AN ITERATION # TECHNIQUE IS UTILIZED IN THE COMPUTATION. @@ -284,7 +284,7 @@ # FUNCTIONAL DESCRIPTION -- # THIS SUBROUTINE, GIVEN AN INITIAL STATE VECTOR AND A DESIRED TRUE-ANOMALY-DIFFERENCE THROUGH WHICH THE # STATE IS TO BE UPDATED ALONG A CONIC TRAJECTORY, CALCULATES THE CORRESPONDING TIME-OF-FLIGHT AND, IN ADDITION, -# PROVIDES THE OPTION OF COMUTING THE NEW UPDATED STATE VECTOR. THE RESULTING TRAJECTORY MAY BE A SECTION OF A +# PROVIDES THE OPTION OF COMPUTING THE NEW UPDATED STATE VECTOR. THE RESULTING TRAJECTORY MAY BE A SECTION OF A # CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE SUBROUTINE CAN BE # EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES, # ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY. @@ -387,7 +387,7 @@ # STATE IS TO BE UPDATED ALONG A CONIC TRAJECTORY, CALCULATES THE CORRESPONDING TIME-OF-FLIGHT AND, IN ADDITION, # PROVIDES THE OPTION OF COMPUTING THE NEW UPDATED STATE VECTOR. THE RESULTING TRAJECTORY MAY BE A SECTION OF A # CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE SUBROUTINE CAN BE -# EXTENDED USING OTHER PRIMARY BODIES BY SIMMPE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES, +# EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES, # ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY. # # IF THE DESIRED RADIUS IS BEYOND THE RADIUS OF APOCENTER OF THE CONIC OR BELOW THE RADIUS OF PERICENTER, @@ -1825,7 +1825,7 @@ KEPC2 EQUALS 36D # R2VEC ERASE +5 # TDESIRED ERASE +1 # GEOMSGN ERASE +0 -# GUESSW # 0 IF COGA GUESS AVIABLE, 1 IF NOT +# GUESSW # 0 IF COGA GUESS AVAILABLE, 1 IF NOT # COGA ERASE +1 # INPUT ONLY IF GUESS IS ZERO. # NORMSW # 0 IF UN TO BE COMPUTED, 1 IF UN INPUT # UN ERASE +5 # ONLY USED IF NORMSW IS 1 diff --git a/Comanche055/CSM_GEOMETRY.s b/Comanche055/CSM_GEOMETRY.s index 1057f35..41ee100 100644 --- a/Comanche055/CSM_GEOMETRY.s +++ b/Comanche055/CSM_GEOMETRY.s @@ -35,7 +35,7 @@ # THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT # VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT. # -# THE INPUTS ARE: 1) THE SEXTAND SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE +# THE INPUTS ARE: 1) THE SEXTANT SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE # MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR # JOB VAC AREA. # @@ -83,7 +83,7 @@ SXTLOGIC CAF 10DEGS- # CORRECT FOR 19.775 DEGREE OFFSET # ERENECED TO THE OPTICS COORDINATE SYSTEM. IN ADDITION IT SETS UP THREE UNIT VECTORS DEFINING THE X, Y, AND Z AXES # REFERENCED TO THE OPTICS COORDINATE SYSTEM. # -# THE INPUTS ARE: 1) THE STAR VECTOR REFERRED TO THE PRESENT STABLE MEMMBER COORDINATES STORED AT STAR. 2) SAME ANGLE +# THE INPUTS ARE: 1) THE STAR VECTOR REFERRED TO THE PRESENT STABLE MEMBER COORDINATES STORED AT STAR. 2) SAME ANGLE # INPUT AS *SMNB*, I.E., SINES AND COSINES OF THE CDU ANGLES, IN THE ORDER Y Z X, AT SINCDU AND COSCDU. A CALL # TO CDUTRIG WILL PROVIDE THIS INPUT. # @@ -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 STROED 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/DISPLAY_INTERFACE_ROUTINES.s b/Comanche055/DISPLAY_INTERFACE_ROUTINES.s index 10390c3..d50d74e 100644 --- a/Comanche055/DISPLAY_INTERFACE_ROUTINES.s +++ b/Comanche055/DISPLAY_INTERFACE_ROUTINES.s @@ -22,7 +22,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # @@ -79,12 +79,12 @@ # IS TO THE USER'S CALLING LOC +1. # 2. ALL ROUTINES NOT ENDING IN R DO NOT DO AN IMMEDIATE RETURN TO THE USER. # 3. ALL ROUTINES THAT END IN R START A SEPARATE JOB (MAKEPLAY) WITH USER'S JOB PRIORITY. -# 4. ALL ROUTIENS NOT ENDING IN R BRANCH DIRECTLY TO MAKEPLAY WHICH MAKES THESE DISPLAYS A PART OF THE +# 4. ALL ROUTINES NOT ENDING IN R BRANCH DIRECTLY TO MAKEPLAY WHICH MAKES THESE DISPLAYS A PART OF THE # USER'S JOB. -# 5. ALL DISPLAY ROUTIENS ARE CALLED VIA BANKCALL. +# 5. ALL DISPLAY ROUTINES ARE CALLED VIA BANKCALL. # 6. TO RESTART A DISPLAY THE USER WILL GENERALLY USE A PHASE OF ONE WITH DESIRED RESTART GROUP (SEE # DESCRIPTION OF RESTARTS). -# 7. ALL FLASHING DISPLAYS HAVE 3 RETURNS TO THE USER FROM ASTRONAUT RESPOSES. A TERMINATE (V34) BRANCHES +# 7. ALL FLASHING DISPLAYS HAVE 3 RETURNS TO THE USER FROM ASTRONAUT RESPONSES. A TERMINATE (V34) BRANCHES # TO THE USER'S CALL CADR +1. A PROCEED (V33) BRANCHES TO THE USER'S CALL CADR +2. AN ENTER OR RECYCLE # (V32) BRANCHES TO THE USER'S CALL CADR +3. # 8. ALL ROUTINES MUST BE USED UNDER EXECUTIVE CONTROL diff --git a/Comanche055/DOWN-TELEMETRY_PROGRAM.s b/Comanche055/DOWN-TELEMETRY_PROGRAM.s index 7b98e12..f75b3bb 100644 --- a/Comanche055/DOWN-TELEMETRY_PROGRAM.s +++ b/Comanche055/DOWN-TELEMETRY_PROGRAM.s @@ -22,7 +22,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/DOWNLINK_LISTS.s b/Comanche055/DOWNLINK_LISTS.s index e772786..4de2ae1 100644 --- a/Comanche055/DOWNLINK_LISTS.s +++ b/Comanche055/DOWNLINK_LISTS.s @@ -19,7 +19,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/ENTRY_LEXICON.s b/Comanche055/ENTRY_LEXICON.s index a692067..20dfc5c 100644 --- a/Comanche055/ENTRY_LEXICON.s +++ b/Comanche055/ENTRY_LEXICON.s @@ -19,7 +19,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/ERASABLE_ASSIGNMENTS.s b/Comanche055/ERASABLE_ASSIGNMENTS.s index 7388dc0..64cf49c 100644 --- a/Comanche055/ERASABLE_ASSIGNMENTS.s +++ b/Comanche055/ERASABLE_ASSIGNMENTS.s @@ -87,7 +87,7 @@ # PRIOR TO INVOCATION OF THE ROUTINE NOR DOES IT # CONTAIN USEFUL OUTPUT TO ANOTHER ROUTINE. THUS # Page 38 -# IT MAY BE SHARED WITHANY OTHER ROUTINE WHICH +# IT MAY BE SHARED WITH ANY OTHER ROUTINE WHICH # IS NOT ACTIVE IN PARALLEL # IN MEANS INPUT TO THE ROUTINE AND IT IS PROBABLY # TEMPORARY FOR A HIGHER-LEVEL ROUTINE/PROGRAM. @@ -492,7 +492,7 @@ ERADFLAG = 017D # EARTH, COMPUTE EARTH, USED FIXED ERADFBIT = BIT13 # BIT 12 FLAG 1 -NODOP01 = 018D # P01 NOT ALLOWED P01 ALLOWD +NODOP01 = 018D # P01 NOT ALLOWED P01 ALLOWED NOP01BIT = BIT12 # BIT 11 FLAG 1 @@ -546,8 +546,8 @@ TRM03FLG = 026D # REQUEST TO NO REQUEST TO TRM03BIT = BIT4 # BIT 3 FLAG 1 -SLOPESW = 027D # ITERATE WITH BIAS ITERATE WITH REGULA - # METHOD IN ITERATOR FALSI METHOD IN +SLOPESW = 027D # ITERATE WITH BIAS ITERATE WITH REGULAR + # METHOD IN ITERATOR FALSE METHOD IN # ITERATOR SLOPEBIT = BIT3 @@ -1564,7 +1564,7 @@ DOTRET ERASE # RETURN FROM DOT SUBROUTINE DVNORMCT EQUALS DOTRET # DIVIDENT NORMALIZATION COUNT IN DDV. ESCAPE2 EQUALS DOTRET # ALTERNATE ARCSIN/ARCCOS SWITCH WDCNT EQUALS DOTRET # CHAR COUNTER FOR DSPWD -INREL EQUALS DOTRET # INPUT BUFFER SELECTIOR ( X,Y,Z, REG ) +INREL EQUALS DOTRET # INPUT BUFFER SELECTOR ( X,Y,Z, REG ) MATINC ERASE # VECTOR INCREMENT IN MXV AND VXM MAXDVSW EQUALS MATINC # +0 IF DP QUOTIENT IS NEAR ONE -- ELSE -1. @@ -2181,7 +2181,7 @@ TDELTAV EQUALS TET +2 # B(6)TMP POSITION DEVIATION KM*2(14) TNUV EQUALS TDELTAV +6 # B(6)TMP VEL DEVIATION KM(-1/2)*2(14) RCV EQUALS TNUV +6 # B(6)TMP CONIC POSITION KM*2(-14) VCV EQUALS RCV +6 # B(6)TMP CONIC VELOCITY KM(-1/2)*2(6) -TC EQUALS VCV +6 # B(2)TMP TIME SINCE RECITIFICATION +TC EQUALS VCV +6 # B(2)TMP TIME SINCE RECTIFICATION XKEP EQUALS TC +2 # B(2)TMP ROOT OF KEPLER EQ KM(1/2)*2(-10) # **** TEMP -- IN VAC AREA **** @@ -3541,7 +3541,7 @@ TNITPREV EQUALS TNIT +2 # I(2) AXISCODE EQUALS TNITPREV +2 # I(1)IN # P30'S-P17 COMMON STORAGE. (24D) -RACT3 EQUALS GRP2SVQ +1 # I(6)TMP POSITION OF ACTIE AT TPI TIME. +RACT3 EQUALS GRP2SVQ +1 # I(6)TMP POSITION OF ACTIVE AT TPI TIME. VACT3 EQUALS RACT3 +6 # I(6)TMP VELOCITY OF ACTIVE AT TPI TIME. RPASS3 EQUALS VACT3 +6 # I(6)TMP POSITION OF PASSIVE AT TPI TIME. VPASS3 EQUALS RPASS3 +6 # I(6)TMP VELOCITY OF PASSIVE AT TPI TIME. diff --git a/Comanche055/EXECUTIVE.s b/Comanche055/EXECUTIVE.s index 6f68477..ea92c99 100644 --- a/Comanche055/EXECUTIVE.s +++ b/Comanche055/EXECUTIVE.s @@ -448,7 +448,7 @@ EJ2 TS BUF +1 TC 2 # Page 1220 -# IDLING AND COMPUTER ACTIVITY (GREEN) LIGHT MAINTENANCE. THE IDLING ROUTIEN IS NOT A JOB IN ITSELF, +# IDLING AND COMPUTER ACTIVITY (GREEN) LIGHT MAINTENANCE. THE IDLING ROUTINE IS NOT A JOB IN ITSELF, # BUT RATHER A SUBROUTINE OF THE EXECUTIVE. EBANK= SELFRET # SELF-CHECK STORAGE IN EBANK. diff --git a/Comanche055/EXTENDED_VERBS.s b/Comanche055/EXTENDED_VERBS.s index aa44901..b82eff7 100644 --- a/Comanche055/EXTENDED_VERBS.s +++ b/Comanche055/EXTENDED_VERBS.s @@ -27,7 +27,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # @@ -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 PRELAUNC + TC CKOPTVB # V 65 E OPTICAL VERIFICATION FOR PRELAUNCH 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 d0748c5..ca56a99 100644 --- a/Comanche055/FRESH_START_AND_RESTART.s +++ b/Comanche055/FRESH_START_AND_RESTART.s @@ -22,7 +22,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # @@ -932,7 +932,7 @@ DUMMYAD EXIT # Page 200 TC BANKCALL - CADR UPACTOFF # TURN OFF UPLINK ACTIV LIGHT + CADR UPACTOFF # TURN OFF UPLINK ACTIVE LIGHT TC DOWNFLAG ADRES VHFRFLAG @@ -1000,7 +1000,7 @@ RENDN00 CS MMNUMBER EXTEND BZF KILL20 - CA FLAGWRD0 # IS RENDZVOO FLAG SET + CA FLAGWRD0 # IS RENDEZVOUS FLAG SET MASK RNDVZBIT CCS A TCF STATQUO @@ -1233,7 +1233,7 @@ RCSADDR4 2CADR RCSATT 3.1SEC OCT 37312 # 2.5 + 0.6 SEC -# FOR VERB 37 TWO TABLES ARE MAINTAINED. EACH TABLE HAS AN ETRY FOR EACH +# FOR VERB 37 TWO TABLES ARE MAINTAINED. EACH TABLE HAS AN ENTRY FOR EACH # MAJOR MODE THAT CAN BE STARTED FROM THE KEYBOARD. THE ENTRIES ARE PUT # INTO THE TABLE WITH THE ENTRY FOR THE HIGHEST MAJOR MODE COMING FIRST, # Page 206 diff --git a/Comanche055/GIMBAL_LOCK_AVOIDANCE.s b/Comanche055/GIMBAL_LOCK_AVOIDANCE.s index 779d4c7..9cd8718 100644 --- a/Comanche055/GIMBAL_LOCK_AVOIDANCE.s +++ b/Comanche055/GIMBAL_LOCK_AVOIDANCE.s @@ -18,7 +18,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/GROUND_TRACKING_DETERMINATION_PROGRAM.s b/Comanche055/GROUND_TRACKING_DETERMINATION_PROGRAM.s index bc624d7..de0a100 100644 --- a/Comanche055/GROUND_TRACKING_DETERMINATION_PROGRAM.s +++ b/Comanche055/GROUND_TRACKING_DETERMINATION_PROGRAM.s @@ -19,7 +19,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/IMU_CALIBRATION_AND_ALIGNMENT.s b/Comanche055/IMU_CALIBRATION_AND_ALIGNMENT.s index 7a49ef3..9cd552a 100644 --- a/Comanche055/IMU_CALIBRATION_AND_ALIGNMENT.s +++ b/Comanche055/IMU_CALIBRATION_AND_ALIGNMENT.s @@ -21,7 +21,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # @@ -201,7 +201,7 @@ PIPJOBB INDEX NDXCTR AINGOTN PDDL DDV DATAPL +4 SL4 DMPR - DEC585 # DEC585 HAS BEEN REDEVINED FOR LEM + DEC585 # DEC585 HAS BEEN REDEFINED FOR LEM RTB SGNAGREE STORE DSPTEM2 @@ -426,11 +426,11 @@ FINETIME INHINT # RETURNS WITH INTERRUPT INHIBITED # # FUNCTIONAL DESCRIPTION # -# THIS SECTON CONSISTS OF PRELAUNCH ALIGNMENT AND GYRO DRIFT TESTS +# THIS SECTION CONSISTS OF PRELAUNCH ALIGNMENT AND GYRO DRIFT TESTS # 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 RECYCL +# IF A RESTART OCCURS THE DATA WILL STILL BE GOOD. GOOD PRACTICE TO RECYCLE # WHEN A RESTART OCCURS UNLESS IT HAPPENS NEAR THE END OF A TEST -- THEN WAIT # FOR THE DATA TO FLASH. # @@ -457,7 +457,7 @@ FINETIME INHINT # RETURNS WITH INTERRUPT INHIBITED # TO PERFORM AS PART OF COMPASS # # 1. OPTICAL VERIFICATION: V 65 E -# 2. AXIMUTH CHANGE: V 78 E +# 2. AZIMUTH CHANGE: V 78 E # # SUBROUTINES CALLED # diff --git a/Comanche055/IMU_MODE_SWITCHING_ROUTINES.s b/Comanche055/IMU_MODE_SWITCHING_ROUTINES.s index 3948cb8..0cfdcbb 100644 --- a/Comanche055/IMU_MODE_SWITCHING_ROUTINES.s +++ b/Comanche055/IMU_MODE_SWITCHING_ROUTINES.s @@ -420,7 +420,7 @@ PIPFREE INHINT # PROGRAM DONE WITH PIPAS. DON'T LIGHT # Page 1430 # THE FOLLOWING ROUTINE TORQUES THE IRIGS ACCORDING TO DOUBLE PRECISION INPUTS IN THE SIX REGISTERS # BEGINNING AT THE ECADR ARRIVING IN A. THE MINIMUM SIZE OF ANY PULSE TRAIN IS 16 PULSES (.25 CDU COUNTS). THE -# UNSENT PORTION OF THE COMMAND IS LEFT INTACT AT TEH INPUT COMMAND REGISTERS. +# UNSENT PORTION OF THE COMMAND IS LEFT INTACT IN THE INPUT COMMAND REGISTERS. EBANK= 1400 # VARIABLE, ACTUALLY. diff --git a/Comanche055/INTER-BANK_COMMUNICATION.s b/Comanche055/INTER-BANK_COMMUNICATION.s index f79019c..3795b50 100644 --- a/Comanche055/INTER-BANK_COMMUNICATION.s +++ b/Comanche055/INTER-BANK_COMMUNICATION.s @@ -22,7 +22,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/INTERPRETER.s b/Comanche055/INTERPRETER.s index c7202da..daf91ab 100644 --- a/Comanche055/INTERPRETER.s +++ b/Comanche055/INTERPRETER.s @@ -78,7 +78,7 @@ DANZIG CA BANKSET # SET BBANK BEFORE TESTING NEWJOB SO THAT NOIBNKSW CCS EDOP # SEE IF AN ORDER CODE IS LEFT OVER FROM TCF OPJUMP # THE LAST PAIR RETRIEVED. IF SO, EXECUTE. - # EDOP IS SET TO ZERO ON ITS RE-EDITIING. + # EDOP IS SET TO ZERO ON ITS RE-EDITING. CCS NEWJOB # SEE IF A JOB OF HIGHER PRIORITY IS TCF CHANG2 # PRESENT, AND IF SO, CHANGE JOBS. @@ -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 PREFICES. + CCS CYR # CODE IS TO BE PROCESSED. TEST PREFIXES. TCF OPJUMP2 # TEST SECOND PREFIX BIT. TCF EXIT # +0 OP CODE IS EXIT @@ -209,7 +209,7 @@ ITR13 INDEX CYR # Page 1113 # PUSH-UP ROUTINES. WHEN NO OPERAND ADDRESS IS GIVEN, THE APPROPRIATE OPERAND IS TAKEN FROM THE PUSH-DOWN -# LIST. IN MOST CASES THE MODE OF THE RESULT (VECTOR OR SCALAR) OF THE LAST ARTGHMETIC OPERATION PERFORMED +# LIST. IN MOST CASES THE MODE OF THE RESULT (VECTOR OR SCALAR) OF THE LAST ARITHMETIC OPERATION PERFORMED # IS THE SAME AS THE TYPE OF OPERAND DESIRED (ALL ADD/SUBTRACT ETC.). EXCEPTIONS TO THIS GENERAL RULE ARE LISTED # BELOW (NOTE THAT IN EVERY CASE THE MODE REGISTER IS LEFT INTACT): # @@ -226,7 +226,7 @@ PUSHUP CAF OCT23 # IF THE LOW 5 BITS OF CYR ARE LESS THAN MASK CYR # 20, THIS OP REQUIRES SPECIAL ATTENTION. AD -OCT10 # (NO -0). CCS A - TCF REGUP # FOR ALL CODES GREATEER THAN OCT 7. + TCF REGUP # FOR ALL CODES GREATER THAN OCT 7. -OCT10 OCT -10 @@ -404,7 +404,7 @@ ITR1 INDEX LOC # THE STORECODE WAS STORED COMPLEMENTED TO AD NEGONE # (YUL CAN'T REMOVE 1 BECAUSE OF EARLY CCS) DOSTORE TS ADDRWD - MASK LOW11 # ENTRY FROM DISPATCHER. SAVE THE ARASABLE + MASK LOW11 # ENTRY FROM DISPATCHER. SAVE THE ERASABLE XCH ADDRWD # ADDRESS AND JUMP ON THE STORE CODE NO. MASK B12T14 EXTEND @@ -518,7 +518,7 @@ TLOAD INDEX ADDRWD DCA 0 DXCH MPAC TMODE CAF ONE - TCF NEWMODE # DECLEARE TRIPLE PRECISION MODE. + TCF NEWMODE # DECLARE TRIPLE PRECISION MODE. SLOAD ZL # LOAD A SINGLE PRECISION NUMBER INTO INDEX ADDRWD # MPAC, SETTING MPAC+1,2 TO ZERO. THE @@ -1047,7 +1047,7 @@ POLYCOM CAF LVBUF # INCOMING X WILL BE MOVED TO VBUF, SO DXCH VBUF # SAVING X IN VBUF TCF POLY2 -POLYLOOP TS POLYCNT # SAVE DECREMENTD LOOP COUNTER +POLYLOOP TS POLYCNT # SAVE DECREMENTED LOOP COUNTER CS TWO ADS POLISH # REGRESS COEFFICIENT POINTER @@ -1337,7 +1337,7 @@ UPPOS XCH L # SAVE DECREMENTED UPPER PART. TS A # SKIPS ON OVERFLOW TCF +2 INCR L # RESTORE UPPER TO ORIGINAL VALUE - XCH L # SWAP A + L BANCK. + XCH L # SWAP A + L BANK. TC Q UPNEG XCH L # SAVE COMPLEMENTED + DECREMENTED UPPER PT @@ -1361,7 +1361,7 @@ DMPR TC DMPSUB TCF DANZIG DDV EXTEND - INDEX ADDRWD # MOVE DIVIDENT INTO BUF. + INDEX ADDRWD # MOVE DIVIDEND INTO BUF. DCA 0 TCF BDDV +4 @@ -1787,7 +1787,7 @@ GENSCL CS ADDRWD # PUT ROUNDING BIT (BIT 10 OF ADDRWD) INTO DDV/BDDV CS ONE # INITIALIZATION TS DVSIGN # +-1 FOR POSITIVE QUOTIENT -- -0 FOR NEG. - TS DVNORMCT # DIVIDENT NORMALIZATION COUNT. + TS DVNORMCT # DIVIDEND NORMALIZATION COUNT. TS MAXDVSW # NEAR-ONE DIVIDE FLAG. CCS BUF # FORCE BUF POSITIVE WITH THE MAJOR PART @@ -1803,7 +1803,7 @@ BUFZERO TS MPAC +2 # ZERO THIS. TCF +2 TCF OVF+ -1 # MAJOR PART OF DIVIDEND IS NEG. NON-ZERO - XCH BUF +1 # SHIFT DIVIDENT AND DIVISOR LEFT 14 + XCH BUF +1 # SHIFT DIVIDEND AND DIVISOR LEFT 14 XCH BUF XCH MPAC +1 XCH MPAC @@ -1819,7 +1819,7 @@ SGNDVOVF EXTEND DVOVF CAF POSMAX # ON DIVISION OVERFLOW OF ANY SORT, SET TS MPAC # SET DP MPAC TO +-POSMAX. TC FINALDV +3 - CAF ONE # SET OVEFLOW INDICATOR AND EXIT. + CAF ONE # SET OVERFLOW INDICATOR AND EXIT. TS OVFIND TC DANZIG @@ -1943,7 +1943,7 @@ BUFNEG CCS A DDOUBL # PROLOGUE WHICH NORMALIZES THE DIVIDEND DDOUBL # WHEN IT IS KNOWN THAT NO DIVISION - DDOUBL # OVEFLOW WILL OCCUR. + DDOUBL # OVERFLOW WILL OCCUR. DDOUBL DDOUBL DDOUBL @@ -1959,7 +1959,7 @@ BUFNEG CCS A MAXTEST CCS MAXDVSW # 0 IF MAJORS MIGHT BE =, -1 OTHERWISE. BIASHI DEC .4192 B-1 # SQRT CONSTANTS. - TCF MAXDV # CHECK TO SEE IF THAY ARE NOW EQUAL. + TCF MAXDV # CHECK TO SEE IF THEY ARE NOW EQUAL. # Page 1167 # THE FOLLOWING IS A GENERAL PURPOSE DOUBLE PRECISION DIVISION ROUTINE. IT DIVIDES MPAC BY BUF AND LEAVES @@ -2287,7 +2287,7 @@ LARGE2 INDEX FIXLOC # Page 1178 # IF THE LENGTH OF THE ARGUMENT VECTOR WAS LESS THAN 2(-28), EACH COMPONENT MUST BE SHIFTED LEFT AT LEAST -# 14 PLACES BEFORE TEH DIVIDE, NOTE THAT IN THIS CASE, THE MAJOR PART OF EACH COMPONENT IS ZERO. +# 14 PLACES BEFORE THE DIVIDE, NOTE THAT IN THIS CASE, THE MAJOR PART OF EACH COMPONENT IS ZERO. SMALL TS MPTEMP # NEGATIVE OF PRE-DIVIDE SHIFT COUNT. diff --git a/Comanche055/INTERRUPT_LEAD_INS.s b/Comanche055/INTERRUPT_LEAD_INS.s index c36ad41..85fdd14 100644 --- a/Comanche055/INTERRUPT_LEAD_INS.s +++ b/Comanche055/INTERRUPT_LEAD_INS.s @@ -19,7 +19,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/KALCMANU_STEERING.s b/Comanche055/KALCMANU_STEERING.s index 712a1ed..18cb6d1 100644 --- a/Comanche055/KALCMANU_STEERING.s +++ b/Comanche055/KALCMANU_STEERING.s @@ -18,7 +18,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/KEYRUPT_UPRUPT.s b/Comanche055/KEYRUPT_UPRUPT.s index 8a138d9..f3c1985 100644 --- a/Comanche055/KEYRUPT_UPRUPT.s +++ b/Comanche055/KEYRUPT_UPRUPT.s @@ -22,7 +22,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/LUNAR_AND_SOLAR_EPHEMERIDES_SUBROUTINES.s b/Comanche055/LUNAR_AND_SOLAR_EPHEMERIDES_SUBROUTINES.s index 0a072a8..534fb1f 100644 --- a/Comanche055/LUNAR_AND_SOLAR_EPHEMERIDES_SUBROUTINES.s +++ b/Comanche055/LUNAR_AND_SOLAR_EPHEMERIDES_SUBROUTINES.s @@ -21,7 +21,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/MEASUREMENT_INCORPORATION.s b/Comanche055/MEASUREMENT_INCORPORATION.s index 7cfb133..6ecdee5 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 COMPONENTN OF STATE VECTOR + X789 # 7TH, 8TH, 9TH COMPONENTS 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 14c51aa..f5b6c2d 100644 --- a/Comanche055/ORBITAL_INTEGRATION.s +++ b/Comanche055/ORBITAL_INTEGRATION.s @@ -227,7 +227,7 @@ GAMCOMP VLOAD VSR1 # Page 1339 36D STORE BETAM - NORM BDDV # FORM NORMALIZE QUOTIEN ALPHAM/BETAM + NORM BDDV # FORM NORMALIZE QUOTIENT ALPHAM/BETAM 33D SR1R PUSH # C(PDL+2) = ALMOST NORMALIZE RHO. DLOAD* diff --git a/Comanche055/P20-P25.s b/Comanche055/P20-P25.s index f3e9779..9d1da62 100644 --- a/Comanche055/P20-P25.s +++ b/Comanche055/P20-P25.s @@ -724,7 +724,7 @@ DECRM61 TS R61CNTR # # USTAR, MODIFIED FICTITIOUS STAR DIRECTION (1/2 UNIT VECTOR) # -# BVECTOR = 9 DIMENTIONAL BVECTOR (1/2 UNIT VEC.) +# BVECTOR = 9 DIMENSIONAL BVECTOR (1/2 UNIT VEC.) # # DELTAQ = MEASURED DEVIATION # @@ -2706,7 +2706,7 @@ DP1MIN 2DEC 6000 V89CALL TC BANKCALL # IMU STATUS CHECK. RETURNS IF ORIENTATION CADR R02BOTH # KNOWN. ALARMS IF NOT. - CAF THREE # ALLOW ASTRONAUT TO SELECT DESURED + CAF THREE # ALLOW ASTRONAUT TO SELECT DESIRED TS OPTION1 # TRACKING ATTITUDE AXIS CAF ONE TS OPTION1 +1 diff --git a/Comanche055/P30-P37.s b/Comanche055/P30-P37.s index 5ded0b3..4f2d137 100644 --- a/Comanche055/P30-P37.s +++ b/Comanche055/P30-P37.s @@ -207,7 +207,7 @@ V16N35 VN 1635 V06N45 VN 0645 # Page 639 -# PROGRAM DESCRPTION S30.1 DATE 9NOV66 +# PROGRAM DESCRIPTION S30.1 DATE 9NOV66 # MOD NO 1 LOG SECTION P30,P37 # MOD BY RAMA AIYAWAR ** # MOD.2 BY S.ZELDIN -- TO CORRECT MOD.1 FOR COLOSSUS 29DEC67 diff --git a/Comanche055/P32-P33_P72-P73.s b/Comanche055/P32-P33_P72-P73.s index 2de37d6..35a4fe4 100644 --- a/Comanche055/P32-P33_P72-P73.s +++ b/Comanche055/P32-P33_P72-P73.s @@ -50,12 +50,12 @@ # APPROVED AND KEYED INTO THE DSKY BY THE ASTRONAUT. # (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. diff --git a/Comanche055/P34-35_P74-75.s b/Comanche055/P34-35_P74-75.s index f7cd212..eea2d1e 100644 --- a/Comanche055/P34-35_P74-75.s +++ b/Comanche055/P34-35_P74-75.s @@ -20,7 +20,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # @@ -38,7 +38,7 @@ # PURPOSE # (1) TO CALCULATE THE REQUIRED DELTA V AND OTHER INITIAL CONDITIONS # REQUIRED BY THE ACTIVE VEHICLE FOR EXECUTION OF THE TRANSFER -# PHASE INITITATION (TPI) MANEUVER, GIVEN -- +# PHASE INITIATION (TPI) MANEUVER, GIVEN -- # (A) TIME OF IGNITION TIG (TPI) OR THE ELEVATION ANGLE (E) OF # THE ACTIVE/PASSIVE VEHICLE LOS AT TIG (TPI). # (B) CENTRAL ANGLE OF TRANSFER (CENTANG) FROM TIG (TPI) TO @@ -759,7 +759,7 @@ NOVRWRT VLOAD PUSH # Page 478 # ***** S34/35.4 ***** -S34/35.4 STQ SETPD NO ASTRONAUT OVERWRITE +S34/35.4 STQ SETPD # NO ASTRONAUT OVERWRITE NORMEX 0D GOTO @@ -1023,14 +1023,14 @@ EPSFOUR 2DEC .0416666666 # # IN ORDER TO AVOID THE INHERENT SINGULARITIES IN THE 180 DEGREE # TRANSFER CASE WHEN THE (TRUE OR OFFSET) TARGET VECTOR MAY BE -# SLIGHTLYOUT OF THE ORBITAL PLANE, THIS SUBROUTINE ROTATES THIS +# SLIGHTLY OUT OF THE ORBITAL PLANE, THIS SUBROUTINE ROTATES THIS # VECTOR INTO A PLANE DEFINED BY THE INPUT INITIAL POSITION VECTOR # AND ANOTHER INPUT VECTOR (USUALLY THE INITIAL VELOCITY VECTOR), # WHENEVER THE INPUT TARGET VECTOR LIES INSIDE A CONE WHOSE VERTEX # IS THE ORIGIN OF COORDINATES, WHOSE AXIS IS THE 180 DEGREE # TRANSFER DIRECTION, AND WHOSE CONE ANGLE IS SPECIFIED BY THE USER. # -# THE LAMBERT SUBROUTINE IS UTILIZED FOR THE CONIC COMUTATIONS AND +# THE LAMBERT SUBROUTINE IS UTILIZED FOR THE CONIC COMPUTATIONS AND # THE COASTING INTEGRATION SUBROUTINE IS UTILIZED FOR THE PRECISION # TRAJECTORY COMPUTATIONS. # diff --git a/Comanche055/P40-P47.s b/Comanche055/P40-P47.s index 72acab8..8d87759 100644 --- a/Comanche055/P40-P47.s +++ b/Comanche055/P40-P47.s @@ -802,7 +802,7 @@ SURELY.9 EXIT RN # ACTIVE VEHICLE RADIUS VECTOR AT T1 STOVL RINIT # Page 701 - VN # ACTIVE VEHICLE VELOCITY VECTORY AT T1 + VN # ACTIVE VEHICLE VELOCITY VECTOR AT T1 STODL VINIT PIPTIME STORE TNIT diff --git a/Comanche055/P51-P53.s b/Comanche055/P51-P53.s index 073640f..ae4cc8a 100644 --- a/Comanche055/P51-P53.s +++ b/Comanche055/P51-P53.s @@ -28,7 +28,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # @@ -742,7 +742,7 @@ CSSUN 2DEC .24148 # (COS 15)/4 # FUNCTION # THIS PROGRAM READS THE IMU-CDUS AND COMPUTES THE VEHICLE ORIENTATION # WITH RESPECT TO INERTIAL SPACE. IT THEN COMPUTES THE SHAFT AXIS (SAX) -# WITH RESPECT TO REFERENCE INTERTIAL. EACH STAR IN THE CATALOG IS TESTED +# WITH RESPECT TO REFERENCE INERTIAL. EACH STAR IN THE CATALOG IS TESTED # TO DETERMINE IF IT IS OCCULTED BY EITHER EARTH, SUN OR MOON. IF A # STAR IS NOT OCCULTED THEN IT IS PAIRED WITH ALL STARS OF LOWER INDEX. # THE PAIRED STAR IS TESTED FOR OCCULTATION. PAIRS OF STARS THAT PASS diff --git a/Comanche055/P61-P67.s b/Comanche055/P61-P67.s index 932d31c..b854b16 100644 --- a/Comanche055/P61-P67.s +++ b/Comanche055/P61-P67.s @@ -23,7 +23,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s b/Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s index b1a15b4..3bac890 100644 --- a/Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s +++ b/Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s @@ -136,7 +136,7 @@ # THE FOLLOWING ARE OF GENERAL INTEREST -- # # REMARKS CARDS PRECEDE THE REFERENCED SYMBOL DEFINITION. SEE SYMBOL -# TABLE TO FIND APPROPRIATE PACE NUMBERS. +# TABLE TO FIND APPROPRIATE PAGE NUMBERS. # # NVSUB CALLING POINT FOR INTERNAL USE OF PINBALL. # OF RELATED INTEREST NVSBWAIT @@ -1656,7 +1656,7 @@ SEPMIN XCH Q # FIND WHOLE MINUTES IN BIT13 ADRES MINCON1 # GIVES FRACT MIN/60 IN MPAC+1. ENDSPMIN TC SEPMNRET # GIVES WHOLE HOURS IN MPAC. -# THIS IS A SPECIAL PURPOS VERB FOR DISPLAYING A DOUBLE PRECISION AGC +# THIS IS A SPECIAL PURPOSE VERB FOR DISPLAYING A DOUBLE PRECISION AGC # WORD AS 10 DECIMAL DIGITS ON THE AGC DISPLAY PANEL. IT CAN BE USED WITH # ANY NOUN, EXCEPT MIXED NOUNS. IT DISPLAYS THE CONTENTS # OF THE REGISTER NOUNADD IS POINTING TO. IF USED WITH NOUNS WHICH ARE @@ -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 PASED INT THE VERB +# A. AFTER EACH MONITOR DISPLAY A *PLEASE* VERB WILL BE PASSED INT 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/PINBALL_NOUN_TABLES.s b/Comanche055/PINBALL_NOUN_TABLES.s index 3b9bc7e..f75fe46 100644 --- a/Comanche055/PINBALL_NOUN_TABLES.s +++ b/Comanche055/PINBALL_NOUN_TABLES.s @@ -20,7 +20,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/R30.s b/Comanche055/R30.s index 1ee43f8..ddb5eb5 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 DONT' CHANGE TFF OR + TC TASKOVER # IF NO FLAGBITS SET DON'T 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 # WITHOLD V16 N44 UNTIL FIRST ORBIT CALC + CCS NEWJOB # WITHHOLD 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 SIGNALLED TERMINATE + MASK EXTVBACT # SEE IF ASTRONAUT HAS SIGNALED TERMINATE EXTEND BZF ENDEXT # YES, TERMINATE VB 82 LOOP CAF 1SEC diff --git a/Comanche055/R31.s b/Comanche055/R31.s index 3d11ea5..8fef656 100644 --- a/Comanche055/R31.s +++ b/Comanche055/R31.s @@ -19,7 +19,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/RCS-CSM_DIGITAL_AUTOPILOT.s b/Comanche055/RCS-CSM_DIGITAL_AUTOPILOT.s index 31c55f6..9a5ca3a 100644 --- a/Comanche055/RCS-CSM_DIGITAL_AUTOPILOT.s +++ b/Comanche055/RCS-CSM_DIGITAL_AUTOPILOT.s @@ -397,7 +397,7 @@ KRESUME1 TCF RESUME # END PHASE 1 # MASK BIT3 # ADS RCSFLAGS # -# THEREAFTER, THE ATTITUDE ERRORS GENERATED BY THE USER SHOULD BE TRANFERRED TO THE FOLLOWING LOCATIONS IN EBANK6: +# THEREAFTER, THE ATTITUDE ERRORS GENERATED BY THE USER SHOULD BE TRANSFERRED 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/RESTARTS_ROUTINE.s b/Comanche055/RESTARTS_ROUTINE.s index fb0de01..cfe42ea 100644 --- a/Comanche055/RESTARTS_ROUTINE.s +++ b/Comanche055/RESTARTS_ROUTINE.s @@ -22,7 +22,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/RESTART_TABLES.s b/Comanche055/RESTART_TABLES.s index bd25dd2..293e119 100644 --- a/Comanche055/RESTART_TABLES.s +++ b/Comanche055/RESTART_TABLES.s @@ -22,7 +22,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/RT8_OP_CODES.s b/Comanche055/RT8_OP_CODES.s index 003fbf2..1bf169a 100644 --- a/Comanche055/RT8_OP_CODES.s +++ b/Comanche055/RT8_OP_CODES.s @@ -20,7 +20,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # @@ -162,7 +162,7 @@ INCRCDUS CAF LOCTHETA LOCTHETA ADRES THETAD # THE FOLLOWING ROUTINE INCREMENTS IN 2'S COMPLEMENT THE REGISTER WHOSE ADDRESS IS IN BUF BY THE 1'S COMPL. -# QUANTITY FOUND IN TEM2. THIS MAY BE USED TO INCRMENT DESIRED IMU AND OPTICS CDU ANGLES OR ANY OTHER 2'S COMPL. +# QUANTITY FOUND IN TEM2. THIS MAY BE USED TO INCREMENT DESIRED IMU AND OPTICS CDU ANGLES OR ANY OTHER 2'S COMPL. # (+0 UNEQUAL TO -0) QUANTITY. MAY BE CALLED BY BANKCALL/SWCALL. CDUINC TS TEM2 # 1'S COMPL. QUANT. ARRIVES IN ACC. STORE IT @@ -264,9 +264,9 @@ DPMODE CAF ZERO # SETS MPAC +2 TO ZERO IN THE PROCESS TCF SLOAD2 # RTB OP CODE NORMUNIT IS LIKE INTERPRETIVE INSTRUCTION UNIT, EXCEPT THAT IT CAN BE DEPENDED ON NOT TO BLOW -# UP WHEN THE VECTOR BEING UNITIZED IS VERY SAMLL -- IT WILL BLOW UP WHEN ALL COMPONENT ARE ZERO. IF NORMUNIT +# UP WHEN THE VECTOR BEING UNITIZED IS VERY SMALL -- IT WILL BLOW UP WHEN ALL COMPONENT ARE ZERO. IF NORMUNIT # IS USED AND THE UPPER ORDER HALVES OF ALL COMPONENTS ARE ZERO, THE MAGNITUDE RETURNS IN 36D WILL BE TOO LARGE -# BY A FACTOR OF 2(13) AND THE SQURED MAGNITUDE RETURNED AT 34D WILL BE TOO BIG BY A FACTOR OF 2(26). +# BY A FACTOR OF 2(13) AND THE SQUARED MAGNITUDE RETURNED AT 34D WILL BE TOO BIG BY A FACTOR OF 2(26). NORMUNX1 CAF ONE TCF NORMUNIT +1 diff --git a/Comanche055/SERVICER207.s b/Comanche055/SERVICER207.s index f9316be..19cc951 100644 --- a/Comanche055/SERVICER207.s +++ b/Comanche055/SERVICER207.s @@ -19,7 +19,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # @@ -617,7 +617,7 @@ NORMLIZE CAF THIRTEEN # SET UP TO COPY 14 REGS: RN1,VN1,PIPTIME1 PIPASR EXTEND DCA TIME2 DXCH PIPTIME1 # CURRENT TIME POSITIVE VALUE - CS ZERO # INITIALIZAE THESE AT NEG ZERO. + CS ZERO # INITIALIZE THESE AT NEG ZERO. TS TEMX TS TEMY TS TEMZ diff --git a/Comanche055/SERVICE_ROUTINES.s b/Comanche055/SERVICE_ROUTINES.s index 64479cc..4b89e09 100644 --- a/Comanche055/SERVICE_ROUTINES.s +++ b/Comanche055/SERVICE_ROUTINES.s @@ -22,7 +22,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/SXTMARK.s b/Comanche055/SXTMARK.s index 4e520a8..803c053 100644 --- a/Comanche055/SXTMARK.s +++ b/Comanche055/SXTMARK.s @@ -19,7 +19,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/SYSTEM_TEST_STANDARD_LEAD_INS.s b/Comanche055/SYSTEM_TEST_STANDARD_LEAD_INS.s index a92f944..fbff01d 100644 --- a/Comanche055/SYSTEM_TEST_STANDARD_LEAD_INS.s +++ b/Comanche055/SYSTEM_TEST_STANDARD_LEAD_INS.s @@ -18,7 +18,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/T4RUPT_PROGRAM.s b/Comanche055/T4RUPT_PROGRAM.s index db620f5..af8594d 100644 --- a/Comanche055/T4RUPT_PROGRAM.s +++ b/Comanche055/T4RUPT_PROGRAM.s @@ -19,7 +19,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # @@ -244,7 +244,7 @@ QUIKOFF EXTEND # PROGRAM NAME: IMUMON # # FUNCTIONAL DESCRIPTION: THIS PROGRAM IS ENTERED EVERY 480 MS. IT DETECTS CHANGES OF THE IMU STATUS BITS IN -# CHANNEL 30 AND CALLS THE APPROPRIATE SUBROUTINES. THE BITS PROCESSED AND THEIR RELEVANT SUROUTINES ARE: +# CHANNEL 30 AND CALLS THE APPROPRIATE SUBROUTINES. THE BITS PROCESSED AND THEIR RELEVANT SUBROUTINES ARE: # # FUNCTION BIT SUBROUTINE CALLED # -------- --- ----------------- @@ -1240,7 +1240,7 @@ ENDZOPT TC ZEROPCDU # ZERO OCDU COUNTERS ZEROPCDU CAF ZERO TS CDUS # ZERO IN CDUS, -20 IN CDUT - TS ZONE # INITIALZE 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 9e96c71..8846c10 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, NORMLIZED. FOR VGAMCALC +# TFFVSQ E:(20) M:(18) 1/M -(V SQ/MU): PRESENT VELOCITY, NORMALIZED. 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/TPI_SEARCH.s b/Comanche055/TPI_SEARCH.s index b31452b..36a7058 100644 --- a/Comanche055/TPI_SEARCH.s +++ b/Comanche055/TPI_SEARCH.s @@ -45,7 +45,7 @@ # # THE S17.2 ROUTINE FURTHER DEFINES THE SEARCH SECTOR BY COMPUTING ANGULAR LIMITS AND USES THE TIME THETA # SUBROUTINE TO COMPUTE THE SEARCH START AND END TIMES. THE SEARCH IS THEN MADE IN AN ITERATIVE LOOP USING THE -# LAMBERT SUBROUTINE TO COMPUTE TEH VELOCITIES REQUIRED AT TPI TIME AND AT TPF TIME. EXIT FROM THE SEARCH LOOP +# LAMBERT SUBROUTINE TO COMPUTE THE VELOCITIES REQUIRED AT TPI TIME AND AT TPF TIME. EXIT FROM THE SEARCH LOOP # IS MADE WHEN SOLUTION CRITERIA ARE MET (NORMAL EXIT) OR AS SOON AS IT IS EVIDENT THAT NO SOLUTION EXISTS IN # THE SECTOR SEARCHED. # diff --git a/Comanche055/TVCDAPS.s b/Comanche055/TVCDAPS.s index c6ba2ca..ed346ff 100644 --- a/Comanche055/TVCDAPS.s +++ b/Comanche055/TVCDAPS.s @@ -365,7 +365,7 @@ YOFFSET EXTEND YACLIM TCR ACTLIM # YAW ACTUATOR-COMMAND-LIMITER -YOUT CS YCMD # INCRMENTAL YAW COMMAND +YOUT CS YCMD # INCREMENTAL YAW COMMAND AD CMDTMP ADS TVCYAW # UPDATE THE ERROR COUNTER (NO RESTART- # PROTECT, SINCE ERROR CNTR ZEROED) diff --git a/Comanche055/TVCEXECUTIVE.s b/Comanche055/TVCEXECUTIVE.s index cc59ea5..09cc153 100644 --- a/Comanche055/TVCEXECUTIVE.s +++ b/Comanche055/TVCEXECUTIVE.s @@ -149,7 +149,7 @@ GAINCHNG TC IBNKCALL # UPDATE IXX, IAVG, IAVG/TLX CAF NINETEEN # RESET THE VARIABLE-GAIN UPDATE COUNTER TS VCNTRTMP -EXECCOPY INCR TVCEXPHS # RESTART-PROTECT TEH COPYCYCLE (1) +EXECCOPY INCR TVCEXPHS # RESTART-PROTECT THE COPYCYCLE (1) CAE MASSTMP # CSMMASS KG B+16 TS CSMMASS diff --git a/Comanche055/TVCRESTARTS.s b/Comanche055/TVCRESTARTS.s index bf09087..e030f4c 100644 --- a/Comanche055/TVCRESTARTS.s +++ b/Comanche055/TVCRESTARTS.s @@ -197,7 +197,7 @@ ENABL2 LXCH BANKRUPT # CONTINUE PREPARATION OF OUTCOUNTERS TCF NOQRSM -CMDSOUT LXCH BANKRUPT # CONTNUE PREPARATION OF OUTCOUNTERS +CMDSOUT LXCH BANKRUPT # CONTINUE PREPARATION OF OUTCOUNTERS EXTEND QXCH QRUPT diff --git a/Comanche055/TVCROLLDAP.s b/Comanche055/TVCROLLDAP.s index 160acc1..952efec 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 BOUNDRY SWITCH LINES). AN APPROXIMATION IS MADE +# LINE OR MINLIM BOUNDARY 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... @@ -150,7 +150,7 @@ # SECOND INTERVALS) WILL BENEFIT FROM THE CONVERGENT NATURE OF THE # APPROXIMATION. # -# FOR LARGE OGAERROR THE TANGENT INTERSECTS +-MINLIM SWITCH BOUNDRY BEFORE +# FOR LARGE OGAERROR THE TANGENT INTERSECTS +-MINLIM SWITCH BOUNDARY BEFORE # INTERSECTING THE STRAIGHT LINE SWITCH. HOWEVER THE MINLIM IS # IGNORED IN COMPUTING THE FIRING TIME, SO THAT THE EXTENSION (INTO # THE COAST REGION) OF THE STRAIGHT LINE SWITCH IS WHAT IS FIRED TO. diff --git a/Comanche055/UPDATE_PROGRAM.s b/Comanche055/UPDATE_PROGRAM.s index 0ae6a85..eeec43e 100644 --- a/Comanche055/UPDATE_PROGRAM.s +++ b/Comanche055/UPDATE_PROGRAM.s @@ -22,7 +22,7 @@ # This AGC program shall also be referred to as Colossus 2A # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Comanche055/WAITLIST.s b/Comanche055/WAITLIST.s index e9b1d30..8433ca4 100644 --- a/Comanche055/WAITLIST.s +++ b/Comanche055/WAITLIST.s @@ -55,7 +55,7 @@ # C(LST2 +16) = 2CADR OF TASK9 # # WARNINGS -- -# 1) 1 <= C(A) <= 16250D (1 CENTISCOND TO 162.5 SEC) +# 1) 1 <= C(A) <= 16250D (1 CENTISECOND TO 162.5 SEC) # 2) 9 TASKS MAXIMUM # 3) TASKS CALLED UNDER INTERRUPT INHIBITED # 4) TASKS END BY TC TASKOVER @@ -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 ERASIBLE ** +# *** THE FOLLOWING IS TO BE IN FIXED-FIXED AND UNSWITCHED ERASABLE ** 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 SUCCESFULLY TAKE ABOUT 1.25 +LONGCYCL EXTEND # CAN WE SUCCESSFULLY TAKE ABOUT 1.25 DCS DPBIT14 # MINUTES OFF OF LONGTIME DAS LONGTIME diff --git a/Luminary099/AOSTASK_AND_AOSJOB.s b/Luminary099/AOSTASK_AND_AOSJOB.s index 83fba58..3e0dba1 100644 --- a/Luminary099/AOSTASK_AND_AOSJOB.s +++ b/Luminary099/AOSTASK_AND_AOSJOB.s @@ -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 diff --git a/Luminary099/AOTMARK.s b/Luminary099/AOTMARK.s index ad6d09a..047f614 100644 --- a/Luminary099/AOTMARK.s +++ b/Luminary099/AOTMARK.s @@ -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 # diff --git a/Luminary099/ASCENT_GUIDANCE.s b/Luminary099/ASCENT_GUIDANCE.s index d59444b..70e654b 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 # 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 diff --git a/Luminary099/ATTITUDE_MANEUVER_ROUTINE.s b/Luminary099/ATTITUDE_MANEUVER_ROUTINE.s index ac4a0d2..05e18b9 100644 --- a/Luminary099/ATTITUDE_MANEUVER_ROUTINE.s +++ b/Luminary099/ATTITUDE_MANEUVER_ROUTINE.s @@ -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 ) diff --git a/Luminary099/BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s b/Luminary099/BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s index 570975a..b88a489 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 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 diff --git a/Luminary099/DAPIDLER_PROGRAM.s b/Luminary099/DAPIDLER_PROGRAM.s index fb42a73..164f84a 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 # JASK NOT IN PROGRESS, INITIALIZE NEG. + TS DAPZRUPT # TASK NOT IN PROGRESS, INITIALIZE NEG. CA TWO TS NPTRAPS TS NQTRAPS diff --git a/Luminary099/DOWN_TELEMETRY_PROGRAM.s b/Luminary099/DOWN_TELEMETRY_PROGRAM.s index 889bb49..74ccad5 100644 --- a/Luminary099/DOWN_TELEMETRY_PROGRAM.s +++ b/Luminary099/DOWN_TELEMETRY_PROGRAM.s @@ -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 diff --git a/Luminary099/FINDCDUW--GUIDAP_INTERFACE.s b/Luminary099/FINDCDUW--GUIDAP_INTERFACE.s index 3e09042..b0f88be 100644 --- a/Luminary099/FINDCDUW--GUIDAP_INTERFACE.s +++ b/Luminary099/FINDCDUW--GUIDAP_INTERFACE.s @@ -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). diff --git a/Luminary099/FLAGWORD_ASSIGNMENTS.s b/Luminary099/FLAGWORD_ASSIGNMENTS.s index 787b568..ee51fef 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 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 diff --git a/Luminary099/INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.s b/Luminary099/INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.s index a838518..3d71a44 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 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 diff --git a/Luminary099/LAMBERT_AIMPOINT_GUIDANCE.s b/Luminary099/LAMBERT_AIMPOINT_GUIDANCE.s index cd367f4..fd09189 100644 --- a/Luminary099/LAMBERT_AIMPOINT_GUIDANCE.s +++ b/Luminary099/LAMBERT_AIMPOINT_GUIDANCE.s @@ -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. diff --git a/Luminary099/LANDING_ANALOG_DISPLAYS.s b/Luminary099/LANDING_ANALOG_DISPLAYS.s index 2698cef..ede4e48 100644 --- a/Luminary099/LANDING_ANALOG_DISPLAYS.s +++ b/Luminary099/LANDING_ANALOG_DISPLAYS.s @@ -17,7 +17,7 @@ # 2021112-061. July 14, 1969. # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Luminary099/LEM_GEOMETRY.s b/Luminary099/LEM_GEOMETRY.s index 33af2e7..9eca786 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 PRECEEDING STORE + MPAC # SET MODE TO DP. (THE PRECEDING 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 8019b5d..6207887 100644 --- a/Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s +++ b/Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s @@ -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 diff --git a/Luminary099/P-AXIS_RCS_AUTOPILOT.s b/Luminary099/P-AXIS_RCS_AUTOPILOT.s index 8a11483..851f2a7 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 ESTIMATER +# BEGIN OFFSET ESTIMATOR # 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 41c8775..b298382 100644 --- a/Luminary099/P12.s +++ b/Luminary099/P12.s @@ -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 diff --git a/Luminary099/P32-P35_P72-P75.s b/Luminary099/P32-P35_P72-P75.s index a6856dd..8be357c 100644 --- a/Luminary099/P32-P35_P72-P75.s +++ b/Luminary099/P32-P35_P72-P75.s @@ -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. # diff --git a/Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s b/Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s index 7a7f1a4..3de826f 100644 --- a/Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s +++ b/Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s @@ -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: diff --git a/Luminary099/RADAR_LEADIN_ROUTINES.s b/Luminary099/RADAR_LEADIN_ROUTINES.s index b2f23b7..266f861 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 SAMLING +RADSAMP CCS RSAMPDT # TIMES NORMAL ONCE PER SECOND SAMPLING TCF +2 TCF TASKOVER # +0 INSERTED MANUALLY TERMINATES TEST. diff --git a/Luminary099/RCS_FAILURE_MONITOR.s b/Luminary099/RCS_FAILURE_MONITOR.s index f8c72d5..347aac5 100644 --- a/Luminary099/RCS_FAILURE_MONITOR.s +++ b/Luminary099/RCS_FAILURE_MONITOR.s @@ -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: diff --git a/Luminary099/RTB_OP_CODES.s b/Luminary099/RTB_OP_CODES.s index 76cb1a6..b1f0e4b 100644 --- a/Luminary099/RTB_OP_CODES.s +++ b/Luminary099/RTB_OP_CODES.s @@ -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 diff --git a/Luminary099/SERVICER.s b/Luminary099/SERVICER.s index 0d75df2..c57513e 100644 --- a/Luminary099/SERVICER.s +++ b/Luminary099/SERVICER.s @@ -19,7 +19,7 @@ # 2021112-061. July 14, 1969. # # Prepared by -# Massachussets Institute of Technology +# Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # diff --git a/Luminary099/SPS_BACK-UP_RCS_CONTROL.s b/Luminary099/SPS_BACK-UP_RCS_CONTROL.s index 0935a86..14654e7 100644 --- a/Luminary099/SPS_BACK-UP_RCS_CONTROL.s +++ b/Luminary099/SPS_BACK-UP_RCS_CONTROL.s @@ -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 diff --git a/Luminary099/THROTTLE_CONTROL_ROUTINES.s b/Luminary099/THROTTLE_CONTROL_ROUTINES.s index bb24381..49c2289 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 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/ diff --git a/Luminary099/TJET_LAW.s b/Luminary099/TJET_LAW.s index c7d7fe8..2ea0ece 100644 --- a/Luminary099/TJET_LAW.s +++ b/Luminary099/TJET_LAW.s @@ -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 From 2f62a05a56e5481306c5f0b89cb11e9e77de0bc8 Mon Sep 17 00:00:00 2001 From: James Harris Date: Tue, 12 Jul 2016 18:52:11 -0500 Subject: [PATCH 3/3] 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/