kjodle/Apollo-11
1
0
Fork 0
Code Issues Pull Requests Projects Releases Wiki Activity

Merge pull request #91 from oldmud0/lots-of-typos

Browse Source 
Fix all the typos
This commit is contained in:
Chris Garry 2016-07-12 22:44:41 -04:00 committed by GitHub
commit 876d5fd2f5
89 changed files with 226 additions and 227 deletions
Show Stats Download Patch File Download Diff File Expand all files Collapse all files

2
Comanche055/ALARM_AND_ABORT.s
View File

@ -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
#

10
Comanche055/ASSEMBLY_AND_OPERATION_INFORMATION.s
View File

@ -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
@ -250,15 +250,15 @@
# 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
# 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
#
@ -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

2
Comanche055/AUTOMATIC_MANEUVERS.s
View File

@ -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

2
Comanche055/CM_BODY_ATTITUDE.s
View File

@ -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
#

6
Comanche055/CM_ENTRY_DIGITAL_AUTOPILOT.s
View File

@ -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.

14
Comanche055/CONIC_SUBROUTINES.s
View File

@ -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.
@ -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.
@ -284,9 +284,9 @@
# 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 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 --
@ -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,
@ -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
@ -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

8
Comanche055/CSM_GEOMETRY.s
View File

@ -33,9 +33,9 @@
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
# 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

12
Comanche055/DISPLAY_INTERFACE_ROUTINES.s
View File

@ -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
@ -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.

8
Comanche055/DOWN-TELEMETRY_PROGRAM.s
View File

@ -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
#
@ -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

2
Comanche055/DOWNLINK_LISTS.s
View File

@ -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
#

2
Comanche055/ENTRY_LEXICON.s
View File

@ -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
#

10
Comanche055/ERASABLE_ASSIGNMENTS.s
View File

@ -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
@ -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.

8
Comanche055/EXECUTIVE.s
View File

@ -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
@ -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.

2
Comanche055/EXTENDED_VERBS.s
View File

@ -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
#

10
Comanche055/FRESH_START_AND_RESTART.s
View File

@ -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
#
@ -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
@ -1000,7 +1000,7 @@ RENDN00 CS MMNUMBER
EXTEND
BZF KILL20
CA FLAGWRD0 # IS RENDZVOO FLAG SET
CA FLAGWRD0 # IS RENDEZVOO 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

2
Comanche055/GIMBAL_LOCK_AVOIDANCE.s
View File

@ -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
#

2
Comanche055/GROUND_TRACKING_DETERMINATION_PROGRAM.s
View File

@ -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
#

8
Comanche055/IMU_CALIBRATION_AND_ALIGNMENT.s
View File

@ -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
@ -426,7 +426,7 @@ 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
@ -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
#

2
Comanche055/IMU_MODE_SWITCHING_ROUTINES.s
View File

@ -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.

2
Comanche055/INTER-BANK_COMMUNICATION.s
View File

@ -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
#

34
Comanche055/INTERPRETER.s
View File

@ -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.
@ -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
@ -401,10 +401,10 @@ 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 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
@ -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 BANCK.
INCR L # RESTORE UPPER TO ROIGINAL VALUE
XCH L # SWAP A + L BACK.
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.
@ -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).

2
Comanche055/INTERRUPT_LEAD_INS.s
View File

@ -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
#

6
Comanche055/JET_SELECTION_LOGIC.s
View File

@ -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
@ -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

4
Comanche055/KALCMANU_STEERING.s
View File

@ -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
#
@ -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

2
Comanche055/KEYRUPT_UPRUPT.s
View File

@ -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
#

2
Comanche055/LUNAR_AND_SOLAR_EPHEMERIDES_SUBROUTINES.s
View File

@ -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
#

2
Comanche055/MEASUREMENT_INCORPORATION.s
View File

@ -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,COMPONENT OF STATE VECTOR
DELTAX +12D # INCORPORATION FOR X789
STORE TX789
BON RTB

4
Comanche055/ORBITAL_INTEGRATION.s
View File

@ -227,9 +227,9 @@ GAMCOMP VLOAD VSR1
# Page 1339
36D
STORE BETAM
NORM BDDV # FORM NORMALIZE QUOTIEN 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

20
Comanche055/P20-P25.s
View File

@ -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 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
@ -714,17 +714,17 @@ 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 DIMENTIONAL BVECTOR (1/2 UNIT VEC.)
# BVECTOR = 9 DIMENSIONAL BVECTOR (1/2 UNIT VEC.)
#
# DELTAQ = MEASURED DEVIATION
#
@ -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
@ -2706,8 +2706,8 @@ 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
TS OPTION1 # TRACKING ATTITUDE AXIS
CAF THREE # ALLOW ASTRONAUT TO SELECT DESIRED
TS OPTION1 # TRACKING ATTITUDE AXIS.
CAF ONE
TS OPTION1 +1
CAF VB04N06 # V 04 N 06

2
Comanche055/P30-P37.s
View File

@ -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

8
Comanche055/P32-P33_P72-P73.s
View File

@ -39,10 +39,10 @@
# 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 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.
@ -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.

12
Comanche055/P34-35_P74-75.s
View File

@ -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
#
@ -31,14 +31,14 @@
# 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
#
# 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.
#

2
Comanche055/P37_P70.s
View File

@ -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).
#

2
Comanche055/P40-P47.s
View File

@ -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

12
Comanche055/P51-P53.s
View File

@ -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
#
@ -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
# ORIENTATIION FOR P52 OR P54.
# THE KEYBOARD. TO COMPUTE THE LANDING SITE
# ORIENTATION FOR P52 OR P54
#
# LET:
# RLS = LANDING SITE VECTOR IN REF COORDINATES
@ -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
@ -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

7
Comanche055/P61-P67.s
View File

@ -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
#
@ -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
@ -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
@ -950,7 +949,7 @@ 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

2
Comanche055/P76.s
View File

@ -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.

2
Comanche055/PHASE_TABLE_MAINTENANCE.s
View File

@ -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
#

20
Comanche055/PINBALL_GAME_BUTTONS_AND_LIGHTS.s
View File

@ -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
@ -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
@ -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
@ -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
@ -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.
@ -2960,14 +2960,14 @@ 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.
#
# 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 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

10
Comanche055/PINBALL_NOUN_TABLES.s
View File

@ -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
#
@ -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

2
Comanche055/R30.s
View File

@ -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 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.

2
Comanche055/R31.s
View File

@ -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
#

2
Comanche055/R60_62.s
View File

@ -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.
#

2
Comanche055/RCS-CSM_DIGITAL_AUTOPILOT.s
View File

@ -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 TRANSFERED TO THE FOLLOWING LOCATIONS IN EBANK6:
#
# AK SCALED 180 DEGREES NOTE: THESE LOCATIONS ARE SUBJECT
# AK1 SCALED 180 DEGREES TO CHANGE

2
Comanche055/RESTARTS_ROUTINE.s
View File

@ -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
#

2
Comanche055/RESTART_TABLES.s
View File

@ -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
#

8
Comanche055/RT8_OP_CODES.s
View File

@ -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

4
Comanche055/SERVICER207.s
View File

@ -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

2
Comanche055/SERVICE_ROUTINES.s
View File

@ -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
#

2
Comanche055/STABLE_ORBIT.s
View File

@ -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
#

4
Comanche055/SXTMARK.s
View File

@ -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
#
@ -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,

2
Comanche055/SYSTEM_TEST_STANDARD_LEAD_INS.s
View File

@ -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
#

10
Comanche055/T4RUPT_PROGRAM.s
View File

@ -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
# -------- --- -----------------
@ -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.
#
@ -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

8
Comanche055/TIME_OF_FREE_FALL.s
View File

@ -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.
@ -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,NORMLIZED. FOR VGAMCALC
# TFFALFA E:(26-NR) 1/M ALFA, WEIGHTED BY NR
# M:(24-NR)
# TFFRTALF E:(10+NA) SQRT(ALFA), NORMALIZED
@ -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

2
Comanche055/TPI_SEARCH.s
View File

@ -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.
#

2
Comanche055/TVCDAPS.s
View File

@ -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)

4
Comanche055/TVCEXECUTIVE.s
View File

@ -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
@ -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

4
Comanche055/TVCRESTARTS.s
View File

@ -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
@ -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

2
Comanche055/TVCROLLDAP.s
View File

@ -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.

4
Comanche055/TVCSTROKETEST.s
View File

@ -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.

4
Comanche055/UPDATE_PROGRAM.s
View File

@ -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
#
@ -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

4
Comanche055/WAITLIST.s
View File

@ -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 ERRASIBLE ***
BLOCK 02
EBANK= LST1

2
Luminary099/AOSTASK_AND_AOSJOB.s
View File

@ -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

4
Luminary099/AOTMARK.s
View File

@ -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
#
@ -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

6
Luminary099/ASCENT_GUIDANCE.s
View File

@ -374,7 +374,7 @@ ASCTERM3 TCF ENDOFJOB
ASCTERM4 EXIT
INHINT
TC IBNKCALL # NO GUIDANCE THIS CYCLE -- HENCE ZERO
CADR ZATTEROR # THE DAP COMMANDED ERRORSss.
CADR ZATTEROR # THE DAP COMMANDED ERRORS.
TCF ASCTERM1 +1
CHECKALT DLOAD DSU
@ -425,7 +425,7 @@ OFFROT CLRGO
SETXFLAG = CHECKYAW
CHECKYAW SET
XOVINFLG # PROHIBIT X-AXIS OVERRRIDE
XOVINFLG # PROHIBIT X-AXIS OVERRIDE
DLOAD VXSC
ATY
LAXIS
@ -473,7 +473,7 @@ ENGOFF RTB
PIPTIME
TTOGO
DCOMP EXIT
TC TPAGREE # FORCH SIGN AGREEMENT ON MPAC, MPAC +1.
TC TPAGREE # FORCE SIGN AGREEMENT ON MPAC, MPAC +1.
CAF EBANK7
TS EBANK
EBANK= TGO

8
Luminary099/ATTITUDE_MANEUVER_ROUTINE.s
View File

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

4
Luminary099/BURN_BABY_BURN--MASTER_IGNITION_ROUTINE.s
View File

@ -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
@ -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.
# ********************************

6
Luminary099/DOWN_TELEMETRY_PROGRAM.s
View File

@ -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.
@ -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
@ -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

4
Luminary099/FINDCDUW--GUIDAP_INTERFACE.s
View File

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

2
Luminary099/FLAGWORD_ASSIGNMENTS.s
View File

@ -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

2
Luminary099/IMU_PERFORMANCE_TESTS_4.s
View File

@ -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

2
Luminary099/INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.s
View File

@ -158,7 +158,7 @@
# BIT 10 LM COMPUTER (NOT AGS) HAS CONTROL OF LM.
# BIT 11 IMU CAGE COMMAND TO DRIVE IMU GIMBAL ANGLES TO 0.
# BIT 12 IMU CDU FAIL (MALFUNCTION OF IMU CDU,S)
# BIT 13 IMU FAIL (MALFUCTION OF IMU STABILIZATION LOOPS)
# BIT 13 IMU FAIL (MALFUNCTION OF IMU STABILIZATION LOOPS)
# BIT 14 ISS TURN ON REQUESTED
# BIT 15 TEMPERATURE OF STABLE MEMBER WITHIN DESIGN LIMITS

2
Luminary099/LANDING_ANALOG_DISPLAYS.s
View File

@ -17,7 +17,7 @@
# 2021112-061. July 14, 1969.
#
# Prepared by
# Massachussets Institute of Technology
# Massachusetts Institute of Technology
# 75 Cambridge Parkway
# Cambridge, Massachusetts
#

14
Luminary099/LUNAR_LANDING_GUIDANCE_EQUATIONS.s
View File

@ -412,10 +412,10 @@ 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 COORDINTES:
# STATE IN GUIDANCE COORDINATES:
# ___ * _ ____
# RGU = CG (R - LAND)
# ___ * _ __ _
@ -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
@ -1257,11 +1257,11 @@ DESCBITS MASK BIT7 # COME HERE FROM MARKRUPT CODING WITH BIT
#
# PRECAUTION: ROOTPSRS MAKES NO CHECKS FOR OVERFLOW OR FOR IMPROPER USAGE. IMPROPER USAGE COULD
# PRECLUDE CONVERGENCE OR REQUIRE EXCESSIVE ITERATIONS. AS A SPECIFIC EXAMPLE, ROOTPSRS FORMS A DERIVATIVE
# COEFFICIENT TABLE BY MULTIPLYINE EACH A(I) BY I, WHERE I RANGES FROM 1 TO N. IF AN ELEMENT OF THE DERIVATIVE
# COEFFICIENT TABLE = 1 OR >1 IN MAGNITUDE, ONLY THE EXCESS IS RETAINED. ROOTPSRS MAY CONVERGE ON THE COREECT
# COEFFICIENT TABLE BY MULTIPLYING EACH A(I) BY I, WHERE I RANGES FROM 1 TO N. IF AN ELEMENT OF THE DERIVATIVE
# COEFFICIENT TABLE = 1 OR >1 IN MAGNITUDE, ONLY THE EXCESS IS RETAINED. ROOTPSRS MAY CONVERGE ON THE CORRECT
# ROOT NONETHELESS, BUT IT MAY TAKE AN EXCESSIVE NUMBER OF ITERATIONS. THEREFORE THE USER SHOULD RECOGNIZE:
# 1. USER'S RESPONSIBILITY TO ASSUR THAT I X A(I) < 1 IN MAGNITUDE FOR ALL I.
# 2. USER'S RESPONSIBILITY TO ASSURE OVERFLOW WILL NOT OCCUR IN EVALUTATING EITHER THE RESIDUAL OR THE DERIVATIVE
# 2. USER'S RESPONSIBILITY TO ASSURE OVERFLOW WILL NOT OCCUR IN EVALUATING EITHER THE RESIDUAL OR THE DERIVATIVE
# POWER SERIES. THIS OVERFLOW WOULD BE PRODUCED BY SUBROUTINE POWRSERS, CALLED BY ROOTPSRS, AND MIGHT NOT
# PRECLUDE EVENTUAL CONVERGENCE.
# 3. AT PRESENT, ERASABLE LOCATIONS ARE RESERVED ONLY FOR N UP TO 5. AN N IN EXCESS OF 5 WILL PRODUCE CHAOS.

2
Luminary099/P-AXIS_RCS_AUTOPILOT.s
View File

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

4
Luminary099/P12.s
View File

@ -47,9 +47,9 @@ 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 RENDEVOUS FLAG FOR P22
TC DOWNFLAG # CLEAR RENDEZVOUS FLAG FOR P22
ADRES RNDVZFLG
CAF THRESH2 # INITIALIZE DVMON

2
Luminary099/P30_P37.s
View File

@ -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 **
#

12
Luminary099/P32-P35_P72-P75.s
View File

@ -30,11 +30,11 @@
# 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 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.
@ -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 -- SELECTS FINAL PROGRAM DISPLAYS AFTER CREW HAS
# COMPLETED THE FINAL MANEUVER COMPUTATION AND DISPLAY
# CYCLE.
#

2
Luminary099/P70-P71.s
View File

@ -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

4
Luminary099/Q_R-AXIS_RCS_AUTOPILOT.s
View File

@ -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:
@ -538,7 +538,7 @@ TJLAW CA TJLAWADR
CADR SPSRCS # DETERMINE RCS CONTROL
RELINT
CAF FOUR # ALWAYS CALL FOR 2-JET CONTROL ABOUT U,V.
TS NUMBERT # FALL THROUGH TO JET SLECTION, ETC.
TS NUMBERT # FALL THROUGH TO JET SELECTION, ETC.
# Q,R-JET-SELECTION-LOGIC
#

2
Luminary099/RADAR_LEADIN_ROUTINES.s
View File

@ -36,7 +36,7 @@
# RADAR SAMPLING LOOP.
COUNT* $$/RLEAD
RADSAMP CCS RSAMPDT # TIMES NORMAL ONCE PER SECOND SAMLING
RADSAMP CCS RSAMPDT # TIMES NORMAL ONCE-PER-SECOND SAMPLING
TCF +2
TCF TASKOVER # +0 INSERTED MANUALLY TERMINATES TEST.

4
Luminary099/RCS_FAILURE_MONITOR.s
View File

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

2
Luminary099/RTB_OP_CODES.s
View File

@ -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

4
Luminary099/SERVICER.s
View File

@ -19,7 +19,7 @@
# 2021112-061. July 14, 1969.
#
# Prepared by
# Massachussets Institute of Technology
# Massachusetts Institute of Technology
# 75 Cambridge Parkway
# Cambridge, Massachusetts
#
@ -1067,7 +1067,7 @@ MUNRVG VLOAD VXSC
R1S
VXV VSL2
WM
STODL DELVS # LUNAR ROTATION CORRECTON TERM*2(5) M/CS.
STODL DELVS # LUNAR ROTATION CORRECTION TERM*2(5) M/CS.
36D
DSU
/LAND/

2
Luminary099/SPS_BACK-UP_RCS_CONTROL.s
View File

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

2
Luminary099/THE_LUNAR_LANDING.s
View File

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

2
Luminary099/THROTTLE_CONTROL_ROUTINES.s
View File

@ -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
#

4
Luminary099/TJET_LAW.s
View File

@ -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:
@ -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

2
Luminary099/TRIM_GIMBAL_CNTROL_SYSTEM.s
View File

@ -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.