From 6088e4655e45054f25c0cd848a2ad4eb4b6b2c04 Mon Sep 17 00:00:00 2001 From: Andrew Murray Date: Fri, 8 Jul 2016 20:45:31 +1000 Subject: [PATCH] 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.