Fixed typos
This commit is contained in:
Andrew Murray
oldmud0
parent
f0075c9e0c
commit
6088e4655e
@ -82,7 +82,7 @@
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# IN R2 THE BBCON OF SELF-CHECK, AND IN R3 THE TOTAL NUMBER OF ERRORS DETECTED BY SELF-CHECK SINCE THE LAST MAN
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# INITIATED FRESH START (SLAP1).
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#
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# SHOW-BANKSUM STARTING WTIH BANK 0 DISPLAYS IN R1 THE BANK SUM (A +-NUMBER EQUAL TO THE BANK NUMBER), IN R2
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# SHOW-BANKSUM STARTING WITH BANK 0 DISPLAYS IN R1 THE BANK SUM (A +-NUMBER EQUAL TO THE BANK NUMBER), IN R2
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# THE BANK NUMBER, AND IN R3 THE BUGGER WORD.
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#
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# ERASABLE INITIALIZATION REQUIRED
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@ -250,7 +250,7 @@
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# Page 8
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# IN THE FOLLOWING NOUN LIST THE 'NO LOAD' RESTRICTION MEANS THE NOUN
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# CONTAINS AT LEAST ONE COMONENT WHICH CANNOT BE LOADED, I.E. OF
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# CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
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# SCALE TYPE L (MIN/SEC) OR PP (2 INTEGERS).
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# IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22, OR 23
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@ -1033,7 +1033,7 @@
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# 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
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# 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
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# 00007 SPECIFY PROPULSION SYSTEM 1=SPS 2=RCS P37 COLOSSUS
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# 00010 SPECIFY ALIGNEMENT MODE 0=ANY TIME 1=REFSMMAT + G P57 LUMINARY
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# 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT + G P57 LUMINARY
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# 2=TWO BODIES 3=ONE BODY + G
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# 00011 SPEC. SEPARATION MONITOR PHASE 1=DELTAV 2=STATE VECTOR UPDATE P46 LUMINARY
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# 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
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@ -490,7 +490,7 @@ ZEROCMDS CAF ZERO
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TS TAU1
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TS TAU2
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T6PROG EXTEND # WHEN THE ROTATION COMMANDS (TAUS)
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DCA JETADDR # HAVE BEEN DETERINED
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DCA JETADDR # HAVE BEEN DETERMINED
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DXCH T5LOC # RESET T5LOC FOR PHASE3
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TCF RESUME
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@ -32,7 +32,7 @@
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# Page 1063
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# SUBROUTINE TO READ GIMBAL ANGLES AND FORM DIFFERENCES. GIMBAL ANGLES ARE SAVED IN 2'S COMPLEMENT, BUT THE
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# DIFFERENECES ARE IN 1'S COMP. ENTER AND READ ANGLES EACH .1 SEC.
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# DIFFERENCES ARE IN 1'S COMP. ENTER AND READ ANGLES EACH .1 SEC.
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#
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# CM/DSTBY = 1 FOR DAP OPERATION
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# CM/DSTBY = 0 TO TERMINATE DAP OPERATION
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@ -289,7 +289,7 @@ T5IDLER1 2CADR T5IDLOC
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# Page 1070
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# THIS SECTION CALCULATES THE ANGULAR BODY RATES EACH .1 SEC. THE ANGULAR RATES ARE THOSE ALONG THE BODY AXES
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# XB, YB, ZB, AND ARE NORMALLY DESIGNATED P, Q, R. REQIREMENT: TEMPORARILY ERASE. JETEM, JETEM +1
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# XB, YB, ZB, AND ARE NORMALLY DESIGNATED P, Q, R. REQUIREMENT: TEMPORARILY ERASE. JETEM, JETEM +1
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#
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# SINCE RESTARTS ZERO THE JET OUTPUT CHANNELS, NO ATTEMPT IS MADE TO RESTART THE ENTRY DAPS. THAT IS,
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# 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
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@ -1079,7 +1079,7 @@ TIMETST5 CS ONE
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# SECTION JETCALL EXAMINES CONTENTS OF JET TIMES IN LIST, ESTABLISHES WTLST ENTRIES, AND EXECUTES CORRESPONDING
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# JET CODES. A POSITIVE NZ NUMBER IN A TIME REGISTER INDICATES THAT A WTLST CALL IS TO BE MADE, AND ITS JET BITS
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# EXECUTED. A +0 INDICATES THAT THE TIME INTERVAL DOES NOT APPLY, BUT THE CORRESPOINDING JET BITS ARE TO BE
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# EXECUTED. A +0 INDICATES THAT THE TIME INTERVAL DOES NOT APPLY, BUT THE CORRESPONDING JET BITS ARE TO BE
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# EXECUTED. A NEG NUMBER INDICATES THAT THE TIME INTERVAL HAS BEEN PROCESSED. IN EVENT OF +0 OR -1, THE
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# SUBSEQUENT TIME REGISTER IS EXAMINED FOR POSSIBLE ACTION. THUS JET BITS TO BE EXECUTED MAY COME FROM MORE
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# THAN ONE REGISTER.
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@ -106,7 +106,7 @@
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# RESPECTIVELY, IS THE CENTRAL BODY
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# TAU +28 DESIRED TRANSFER TIME IN CENTISECONDS (DP)
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# MAY BE POS OR NEG AND ABSOLUTE VALUE MAY BE GREATER OR LESS THAN ONE ORBITAL PERIOD.
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# XKEPNEW +17 FOR EARTH DP GUESS OF ROOT X OF KEPLERS EQN IN SQRT(METERS).SIGN SHOULD AGREE WTIH THAT OF TAU.
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# XKEPNEW +17 FOR EARTH DP GUESS OF ROOT X OF KEPLERS EQN IN SQRT(METERS).SIGN SHOULD AGREE WITH THAT OF TAU.
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# +16 FOR MOON AND ABS VALUE SHOULD BE LESS THAN THAT CORRESPONDING TO A PERIOD, VIZ, 2PI SQRT(SEMI-
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# MAJOR AXIS), FOR SPEED OF CONVERGENCE, BUT IF EITHER CONDITION FAILS, XKEPNEW IS RESET
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# BY KEPLER TO A POOR BUT VALID GUESS.
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@ -286,7 +286,7 @@
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# STATE IS TO BE UPDATED ALONG A CONIC TRAJECTORY, CALCULATES THE CORRESPONDING TIME-OF-FLIGHT AND, IN ADDITION,
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# PROVIDES THE OPTION OF COMUTING THE NEW UPDATED STATE VECTOR. THE RESULTING TRAJECTORY MAY BE A SECTION OF A
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# CIRCLE, ELLIPSE, PARABOLA, OR HYPERBOLA WITH RESPECT TO THE EARTH OR THE MOON. THE USE OF THE SUBROUTINE CAN BE
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# EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WTIHOUT INTRODUCING ANY CODING CHANGES,
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# EXTENDED USING OTHER PRIMARY BODIES BY SIMPLE ADDITIONS TO THE MUTABLE WITHOUT INTRODUCING ANY CODING CHANGES,
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# ACCEPTING THE INHERENT SCALE FACTOR CHANGES IN POSITION AND VELOCITY.
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#
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# THE RESTRICTIONS ARE --
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@ -1776,7 +1776,7 @@ MUTABLE 2DEC* 3.986032 E10 B-36* # MUE
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LDPOSMAX EQUALS LODPMAX # DPPOSMAX IN LOW MEMORY.
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# ERASABLE ASSIGNEMENTS
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# ERASABLE ASSIGNMENTS
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# KEPLER SUBROUTINE
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@ -33,7 +33,7 @@
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BANK
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# THIS ROUTINE TAKES THE SHAFT AND TRUNNION ANGLES AS READ BY THE CM OPTICAL SYSTEM AND CONVERTS THEM INTO A UNIT
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# VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WTIH THE SEXTANT LINE OF SIGHT.
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# VECTOR REFERENCED TO THE NAVIGATION BASE COORDINATE SYSTEM AND COINCIDENT WITH THE SEXTANT LINE OF SIGHT.
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#
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# THE INPUTS ARE: 1) THE SEXTAND SHAFT AND TRUNNION ANGLES ARE STORED SP IN LOCATIONS 3 AND 5 RESPECTIVELY OF THE
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# MARK VAC AREA. 2) THE COMPLEMENT OF THE BASE ADDRESS OF THE MARK VAC AREA IS STORED SP AT LOCATION X1 OF YOUR
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@ -485,7 +485,7 @@
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# 5. IT IS ALWAYS GOOD PRACTICE TO TERMINATE AN EXTENDED VERB BEFORE ASKING FOR ANOTHER ONE OR THE SAME ONE
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# OVER AGAIN.
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#
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# SPECIAL CONSIDERATONS --
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# SPECIAL CONSIDERATIONS --
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# Page 1464
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# 1. MPAC +2 SAVED ONLY IN MARK DISPLAYS
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# 2. GODSP(R), REGODSP(R), GOMARK(R) ALWAYS TURN ON THE FLASH IF ENTERED WITH A PASTE VERB REQUEST.
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@ -638,7 +638,7 @@ COPYPACS INDEX COPINDEX
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TC Q
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# PINCHEK CHECKS TO SEE IF THE CURRENT MARK REQUEST IS MADE BY THE ASTRONAUT WHILE INTERUPTING A GOPLAY DISPLAY
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# PINCHEK CHECKS TO SEE IF THE CURRENT MARK REQUEST IS MADE BY THE ASTRONAUT WHILE INTERRUPTING A GOPLAY DISPLAY
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# (A NORMAL OR A PRIO). IF THE ASTRONAUT TRIES TO MARK DURING A PRIO, THE CHECK FAIL LIGHT GOES ON AND THE MARK
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# REQUEST IS ENDED. IF HE TRIES TO MARK DURING A NORM, THE MARK IS ALLOWED. IN THIS CASE THE NORM IS PUT TO SLEEP
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# UNTIL ALL MARKING IS FINISHED.
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@ -106,7 +106,7 @@
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# 1. DOWNLISTS. DOWNLISTS MUST BE COMPILED IN THE SAME BANK AS THE
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# DOWN-TELEMETRY PROGRAM. THIS IS DONE FOR EASE OF CODING, FASTER
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# EXECUTION.
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# 2. EACH DOWNLINK LIST CONSISTES OF A CONTROL LIST AND A NUMBER OF
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# 2. EACH DOWNLINK LIST CONSISTS OF A CONTROL LIST AND A NUMBER OF
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# SUBLISTS.
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# 3. A SUBLIST REFERS TO A SNAPSHOT OR DATA COMMON TO THE SAME OR OTHER
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# DOWNLINK LISTS. ANY SUBLIST CONTAINING COMMON DATA NEEDS TO BE
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@ -122,7 +122,7 @@
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# SAME AS ECADR, BUT USED WHEN THE WORD ADDRESSED IS THE LEFT
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# HALF OF A DOUBLE-PRECISION WORD FOR DOWN TELEMETRY.
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# B. 2DNADR - 6DNADR N-WORD DOWNLIST ADDRESS, N = 2 - 6.
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# SAME AS 1DNADR, BUT WTIH THE 4 UNUSED BITS OF THE ECADR FORMAT
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# SAME AS 1DNADR, BUT WITH THE 4 UNUSED BITS OF THE ECADR FORMAT
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# FILLED IN WITH 0001-0101. USED TO POINT TO A LIST OF N DOUBLE-
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# PRECISION WORDS, STORED CONSECUTIVELY, FOR DOWN TELEMETRY.
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# C. DNCHAN DOWNLIST CHANNEL ADDRESS.
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@ -347,7 +347,7 @@ SUBLIST EQUALS DNQ
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# AFTER KEYING IN V74E THE CURRENT DOWNLIST WILL BE IMMEDIATELY TERMINATED AND THE DOWNLINK ERASABLE DUMP
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# WILL BEGIN.
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#
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# ONCE INITITIATED THE DOWNLINK ERASABLE DUMP CAN BE TERMINATED (AND INTERRUPTED DOWNLIST REINSTATED) ONLY
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# ONCE INITIATED THE DOWNLINK ERASABLE DUMP CAN BE TERMINATED (AND INTERRUPTED DOWNLIST REINSTATED) ONLY
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# BY THE FOLLOWING:
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#
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# 1. A FRESH START
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@ -47,7 +47,7 @@ NOVAC INHINT
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TS EXECTEM1
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TCF NOVAC2 # ENTER EXECUTIVE BANK.
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# TO ENTER A JOB REQUEST REQUIREING A VAC AREA -- E.G., ALL (PARTIALLY) INTERPRETIVE JOBS.
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# TO ENTER A JOB REQUEST REQUIRING A VAC AREA -- E.G., ALL (PARTIALLY) INTERPRETIVE JOBS.
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FINDVAC INHINT
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TS NEWPRIO
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@ -157,7 +157,7 @@ NOVAC2 CAF ZERO # NOVAC ENTERS HERE. FIND A CORE SET.
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NOVAC3 TS EXECTEM2
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INDEX LOCCTR
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CCS PRIORITY # EACH PRIORITY REGISTER CONTAINS -0 IF
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TCF NEXTCORE # THE CORESPONDING CORE SET IS AVAILABLE.
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TCF NEXTCORE # THE CORRESPONDING CORE SET IS AVAILABLE.
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NO.CORES DEC 6
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TCF NEXTCORE # AN ACTIVE JOB HAS A POSITIVE PRIORITY
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# BUT A DORMANT JOB'S PRIORITY IS NEGATIVE
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@ -319,7 +319,7 @@ JOBWAKE3 CAF COREINC
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ADS LOCCTR
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CCS EXECTEM2
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TCF JOBWAKE4
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CS ONE # EXIT IF SLEEPIG JOB NOT FOUND.
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CS ONE # EXIT IF SLEEPING JOB NOT FOUND.
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TS LOCCTR
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TCF ENDFIND
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@ -99,7 +99,7 @@
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#
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# 1. INTIALIZE OUTBIT CHANNELS 11,12,13, AND 14
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# 2. REPLACE ALL TASKS ON WAITLIST WITH ENDTASK
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# 3. MAKE ALL EXECUTEVE REGISTERS AVAILABLE
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# 3. MAKE ALL EXECUTIVE REGISTERS AVAILABLE
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# 4. MAKE ALL VAC AREAS AVAILABLE
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# 5. CLEAR DSKY REGISTERS
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# 6. ZERO NUMEROUS SWITCHES
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@ -130,7 +130,7 @@
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# B. ALARMS
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#
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# 1107 PHASE TABLE ERROR
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# 1110 RESTART WTIH NO ACTIVE GROUPS
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# 1110 RESTART WITH NO ACTIVE GROUPS
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# Page 183
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BANK 10
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@ -2626,7 +2626,7 @@ NORMTEST CCS CYL # SEE IF ARGUMENT NOW NORMALIZED AT
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# Page 1187
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# TRIGONOMETRIC FUNCTION PACKAGE.
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# THE FOLLOWING TRIGONOMETRIC FUNCTIONS ARE AVAIALABLE AS INTERPRETIVE OPERATIONS:
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# THE FOLLOWING TRIGONOMETRIC FUNCTIONS ARE AVAILABLE AS INTERPRETIVE OPERATIONS:
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# 1. SIN COMPUTES (1/2)SINE(2 PI MPAC).
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# 2. COS COMPUTES (1/2)COSINE(2 PI MPAC).
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# 3. ASIN COMPUTES (1/2PI)ARCSINE(2 MPAC).
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@ -365,7 +365,7 @@ NOACY CA RWORD1 # Y-TRANSLATION NOT ACCEPTED
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# FAILURES. IF THERE ARE BD FAILURES, Z-TRANSLATION COMMANDS WILL BE IGNORED, IN WHICH CASE THE ASTRONAUT SHOULD
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# SWITCH TO AC ROLL.
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#
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# NOTE THAT IF ONE QUAD FAILS (E.G. B FAILED), Z-TRANSLATION IS STILL POSSIBLE AND THAT THE UNDESIREABLE ROLL
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# NOTE THAT IF ONE QUAD FAILS (E.G. B FAILED), Z-TRANSLATION IS STILL POSSIBLE AND THAT THE UNDESIRABLE ROLL
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# INTRODUCED BY THIS TRANSLATION WILL BE COMPENSATED BY THE TWO AC ROLL JETS ACTUATED BY THE AUTOPILOT LOGIC.
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#
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# WORD MAKE UP....RTABLE
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@ -386,7 +386,7 @@ NOACY CA RWORD1 # Y-TRANSLATION NOT ACCEPTED
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# THIS WORD MAY THEN BE ADDED TO THE WORD SELECTED FROM THE YZ-TRANSLATION TABLE, WHICH HAS THE SAME TYPE OF
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# CODING AS ABOVE, AND THE NET ROLL DETERMINED BY SHIFTING THE RESULTANT WORD RIGHT 8 PLACES AND SUBTRACTING FOUR.
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#
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# THE WORD CORRESPONDING TO THE BD ROLL HAS A SIMILAR INTEPRETATION, EXCEPT THAT BITS 12, 13, 14 ARE CODED
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# THE WORD CORRESPONDING TO THE BD ROLL HAS A SIMILAR INTERPRETATION, EXCEPT THAT BITS 12, 13, 14 ARE CODED
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# (AS ABOVE) TO GIVE THE NET ROLL TORQUE.
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# ROLL TRANS QUADFAIL BIAS
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@ -89,7 +89,7 @@ INCRDCDU TS KSPNDX
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TCF INCRDCDU # LOOP FOR THREE AXES
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RELINT
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# COMPARE PRESENT TIME WTIH TIME TO TERMINATE MANEUVER
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# COMPARE PRESENT TIME WITH TIME TO TERMINATE MANEUVER
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TMANUCHK TC TIMECHK
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TC POSTJUMP
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@ -127,7 +127,7 @@ ELRCODE OCT 22
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# THE RECEPTION OF A BAD CODE (I.E., CCC FAILURE) LOCKS OUT FURTHER UPLINK ACTIVITY BY SETTING BIT4 OF FLAGWRD7 = 1.
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# THIS INDICATION WILL BE TRANSFERRED TO THE GROUND BY THE DOWNLINK WHICH DOWNLINKS ALL FLAGWORDS.
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# WHEN UPLINK ACTIVITY IS LOCKED OUT, IT CAN BE ALLOWED WHEN THE GROUND UPLINKS AND `ERROR RESET' CODE.
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# (IT IS RECOMMENDED THAT THE `ERROR LIGHT RESET' CODE IS PRECEEDED BY 16 BITS THE FIRST OF WHICH IS 1 FOLLOWED
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# (IT IS RECOMMENDED THAT THE `ERROR LIGHT RESET' CODE IS PRECEDED BY 16 BITS THE FIRST OF WHICH IS 1 FOLLOWED
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# BY 15 ZEROS. THIS WILL ELIMINATE EXTRANEOUS BITS FROM INLINK WHICH MAY HAVE BEEN LEFT OVER FROM THE ORIGINAL
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# FAILURE).
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#
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@ -420,7 +420,7 @@ DE-GR-50 TC 2PHSCHNG
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#
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# ABORT MODES: P23 ABORT IF MARKING SYSTEM OR EXTENDED VERB ACTIVE
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#
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# INPUT: NONE REQURIES, NORMALLY CALLED BY P23
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# INPUT: NONE REQUIRES, NORMALLY CALLED BY P23
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#
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# OUTPUT: TRUNNION BIAS ANGLE: ANGLE DETERMINED WHEN SHAFT LINE OF SIGHT
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# (SLOS) AND LANDMARK LINE OF SIGHT (LLOS) ARE SUPERIMPOSED. THIS ANGLE
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@ -1407,7 +1407,7 @@ INITB STORE W +90D,1 # CLEAR 54 - 89
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#
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# OMETATHSM = (REFSMMAT)(OMEGATH).
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#
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# (10) OBTAIN GIMBAL ANGLE INCREMETNS FOR 0.1 SECOND.
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# (10) OBTAIN GIMBAL ANGLE INCREMENTS FOR 0.1 SECOND.
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#
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# DTHETASM = (0.1)(OMEGATHSM)
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#
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@ -1776,7 +1776,7 @@ FURST3 EQUALS 13,14,15 # CONSTANT FOR AUTOCK (OCT 70000).
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# ..... S22.1 ORBITAL NAVIGATION ROUTINE
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# MOD 1
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#
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# FUNCTONAL DESCRIPTION
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# FUNCTIONAL DESCRIPTION
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# 1. UPDATE CSM STATE VECTOR
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# 2. UPDATE LANDMARK POSITION
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# 3. CONVERT W MATRIX FROM 9 TO 6 DIMENSIONS
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@ -42,7 +42,7 @@
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# MOD BY WHITE, P. DATE 1 JUNE 67
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#
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# PURPOSE
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# (1) TO CALCULATE PARAMETERS ASSOCIATED WTIH THE FOLLOWING
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# (1) TO CALCULATE PARAMETERS ASSOCIATED WITH THE FOLLOWING
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# CONCENTRIC FLIGHT PLAN MANEUVERS -- THE CO-ELLIPTIC SEQUENCE
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# INITIATION (CSI) MANEUVER AND THE CONSTANT DELTA ALTITUDE
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# (CDH) MANEUVER.
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@ -31,7 +31,7 @@
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# Page 460
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# TRANSFER PHASE INITITIATION (TPI) PROGRAMS (P34 AND P74)
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# TRANSFER PHASE INITIATION (TPI) PROGRAMS (P34 AND P74)
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# MOD NO -1 LOG SECTION -- P32-P35, P72-P75
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# MOD BY WHITE, P. DATE: 1 JUNE 67
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#
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@ -44,7 +44,7 @@
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# DESCRIPTION
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# A RETURN TO EARTH TRAJECTORY IS COMPUTED PROVIDED THE CSM IS OUTSIDE THE LUNAR SPHERE OF INFLUENCE AT THE
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# TIME OF IGNITION. INITIALLY A CONIC TRAJECTORY IS DETERMINED AND RESULTING IGNITION AND REENTRY PARAMETERS ARE
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# DISPLAYED TO THE ASTRONAUT. THEN IF THE ASTRONAUT SO DESIRES, A PRECISION TRAJECTORY IS DETERMINED WTIH THE
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# DISPLAYED TO THE ASTRONAUT. THEN IF THE ASTRONAUT SO DESIRES, A PRECISION TRAJECTORY IS DETERMINED WITH THE
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# RESULTING IGNITION AND REENTRY PARAMETERS DISPLAYED. UPON FINAL ACCEPTANCE BY THE ASTRONAUT, THE PROGRAM
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# COMPUTES AND STORES THE TARGET PARAMETERS FOR RETURN TO EARTH FOR USE BY SPS PROGRAM (P40) OR RCS PROGRAM (P41).
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#
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@ -318,7 +318,7 @@ V06N89* VN 0689
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# FUNCTION -- TO DISPLAY THE LANDING SITE LATITUDE,
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# LONGITUDE AND ALTITUDE. TO ACCEPT NEW DATA VIA
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# THE KEYBOARD. TO COMPUT THE LANDING SITE
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# ORIENTATIION FOR P52 OR P54.
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# ORIENTATION FOR P52 OR P54.
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#
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# LET:
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# RLS = LANDING SITE VECTOR IN REF COORDINATES
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@ -1633,7 +1633,7 @@ MKDNCDR ECADR MARKDOWN
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# MOD. NO. 2 21 DEC 66
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# MOD. BY STURLAUGSON
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#
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# FUNCTIONAL DESCRIPTIION:
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# FUNCTIONAL DESCRIPTION:
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#
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# TO PERFORM A SATISFACTORY NUMBER OF SIGHTING MARKS FOR THE REQUESTING PROGRAM (OR ROUTINE). SIGHTINGS
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# CAN BE MADE ON A STAR OR LANDMARK. WHEN THE CMC ACCEPTS A MARK IT RECORDS AND STORES 5 ANGLES (3 ICDUS AND 2
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@ -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
|
||||
|
||||
@ -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
|
||||
|
||||
@ -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.
|
||||
|
||||
@ -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
|
||||
#
|
||||
|
||||
@ -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.
|
||||
#
|
||||
|
||||
@ -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
|
||||
|
||||
@ -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.
|
||||
#
|
||||
|
||||
@ -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
|
||||
|
||||
@ -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
|
||||
|
||||
@ -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
|
||||
#
|
||||
|
||||
@ -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,
|
||||
|
||||
@ -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.
|
||||
#
|
||||
|
||||
@ -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
|
||||
|
||||
@ -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
|
||||
|
||||
@ -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
|
||||
|
||||
@ -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.
|
||||
|
||||
@ -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
|
||||
|
||||
@ -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
|
||||
|
||||
@ -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.
|
||||
|
||||
# ********************************
|
||||
|
||||
@ -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
|
||||
|
||||
@ -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
|
||||
|
||||
@ -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
|
||||
|
||||
@ -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.
|
||||
|
||||
@ -964,7 +964,7 @@ HEADTJET CA ZERO
|
||||
-FOURDEG DEC -.08888
|
||||
|
||||
# Page 1440
|
||||
# JET POLICY CONTSTRUCTION SUBROUTINE
|
||||
# JET POLICY CONSTRUCTION SUBROUTINE
|
||||
#
|
||||
# INPUT: ROTINDEX, NUMBERT
|
||||
#
|
||||
|
||||
@ -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 **
|
||||
#
|
||||
|
||||
@ -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.
|
||||
|
||||
@ -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
|
||||
|
||||
@ -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
|
||||
#
|
||||
|
||||
@ -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
|
||||
|
||||
@ -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/
|
||||
|
||||
@ -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.
|
||||
|
||||
@ -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
|
||||
#
|
||||
|
||||
@ -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:
|
||||
|
||||
@ -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.
|
||||
|
||||
Loading…
Reference in New Issue
Block a user