typo corrections for Push Requst to chrislgarry/Apollo-11
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@ -329,7 +329,7 @@ DNTMEXIT EXTEND # DOWN-TELEMETRY EXIT
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CA L # RESPECTIVELY
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TMEXITL EXTEND
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WRITE DNTM2
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TMRESUME TCF RESUME # EXIT TELEMTRY PROGRAM VIA RESUME.
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TMRESUME TCF RESUME # EXIT TELEMETRY PROGRAM VIA RESUME.
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MINB12 EQUALS -1/8
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DNECADR EQUALS TMINDEX
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@ -1561,7 +1561,7 @@ ESCAPE EQUALS DOTINC # USED IN ARCSIN/ARCCOS.
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ENTRET EQUALS DOTINC # EXIT FROM ENTER
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DOTRET ERASE # RETURN FROM DOT SUBROUTINE
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DVNORMCT EQUALS DOTRET # DIVIDENT NORMALIZATION COUNT IN DDV.
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DVNORMCT EQUALS DOTRET # DIVIDEND NORMALIZATION COUNT IN DDV.
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ESCAPE2 EQUALS DOTRET # ALTERNATE ARCSIN/ARCCOS SWITCH
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WDCNT EQUALS DOTRET # CHAR COUNTER FOR DSPWD
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INREL EQUALS DOTRET # INPUT BUFFER SELECTOR ( X,Y,Z, REG )
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@ -97,7 +97,7 @@
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#
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# 2.2 SCALING
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#
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# THE INTEGRATION ROUTIEN WILL MAINTAIN THE PERMANENT MEMORY STATE VECTORS IN THE SCALING AND UNITS DEFINED IN
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# THE INTEGRATION ROUTINE WILL MAINTAIN THE PERMANENT MEMORY STATE VECTORS IN THE SCALING AND UNITS DEFINED IN
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# APPENDIX B OF THE USERS' GUIDE. THE SCALING OF THE OUTPUT POSITION VECTOR DEPENDS ON THE ORIGIN OF THE COORDINATE
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# SYSTEM AT THE DESIRED INTEGRATION TIME. THE COORDINATE SYSTEM TRANSFORMATION WILL BE DONE AUTOMATICALLY ON
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# MULTIPLE TIMESTEP ENCKE INTEGRATION ONLY. THUS IT IS POSSIBLE TO HAVE OUTPUT FROM SUCCESSIVE INTEGRATIONS IN
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@ -1336,8 +1336,8 @@ UPPOS XCH L # SAVE DECREMENTED UPPER PART.
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AD HALF
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TS A # SKIPS ON OVERFLOW
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TCF +2
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INCR L # RESTORE UPPER TO ROIGINAL VALUE
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XCH L # SWAP A + L BACK.
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INCR L # RESTORE UPPER TO ORIGINAL VALUE
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XCH L # SWAP A + L BANK.
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TC Q
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UPNEG XCH L # SAVE COMPLEMENTED + DECREMENTED UPPER PT
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@ -2458,7 +2458,7 @@ DSQSUB CA MPAC +1 # SQUARES THE SCALAR CONTENTS OF MPAC.
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XCH MPAC +1
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EXTEND
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MP MPAC
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DDOUBL # AND MAYBE OVEFLOW.
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DDOUBL # AND MAYBE OVERFLOW.
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DAS MPAC +1 # AND SET A TO NET OVERFLOW.
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XCH MPAC
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EXTEND
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@ -278,7 +278,7 @@ BDZCHECK CA ZNDX
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BZF TAUCHECK
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ACRBDZ CA T5TEMP # Z-TRANSLATION ACCEPTED EVEN THO WE MAY
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TS RWORD1 # HAVE INTRODUCED AN UNDESIREABLE ROLL
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TS RWORD1 # HAVE INTRODUCED AN UNDESIRABLE ROLL
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TCF ROLLTIME # BRANCH TO JET ON-TIME CALCULATIONS
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TAUCHECK CCS TAU
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@ -362,7 +362,7 @@ FAZC CALL
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GRP2PC
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# Page 1259
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VLOAD VAD # START 3RD PHASE OF INCORP2
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X789 # 7TH,8TH,9TH,COMPONENT OF STATE VECTOR
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X789 # 7TH, 8TH, 9TH COMPONENT OF STATE VECTOR
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DELTAX +12D # INCORPORATION FOR X789
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STORE TX789
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BON RTB
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@ -531,7 +531,7 @@ V51NB VN 5100
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# 7 REGISTER MRKBUF2 CONTAINING TIME2,TIME1,CDUY,OPTICS X,CDUZ, OPTICS Y,
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# CDUX.
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#
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# ERASABLE INTIALIZATION REQUIRED
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# ERASABLE INITIALIZATION REQUIRED
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#
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# FLAGS SET AND RESET
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# R21MARK (COMMUNICATION TO MARKRUPT TO STORE MARKS IN MRKBUF1 +2)
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@ -782,7 +782,7 @@ PI/4.0 2DEC .785398164
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# MARKDATA, BASE ADDRESS OF MARK DATA
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# REFSMMAT, ROTATION MATRIX FROM STABLE MEMBER TO BASIC REF. COORD. SYSTEM
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#
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# SUROUTINES CALLED:
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# SUBROUTINES CALLED:
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#
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# SXTNB -- SEXT. ANGULAR READINGS TO NAV. BASE COOR.
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# NBSM -- TRANSFORM FROM NAV. BASE TO STABLE MEMBER
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@ -39,7 +39,7 @@
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# COELLIPTIC SEQUENCE INITIATION (CSI) PROGRAMS (P32 AND P72)
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#
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# MOD NO -1 LOG SECTION -- P32-P35, P72-P75
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# MOD BY WHITE. P DATE 1JUNE67
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# MOD BY WHITE, P. DATE 1JUNE67
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#
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# PURPOSE
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# (1) TO CALCULATE PARAMETERS ASSOCIATED WITH THE FOLLOWING
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@ -1419,7 +1419,7 @@ RTRNMU STORE RTMU
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# INPUT
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# (1) RVEC POSITION VECTOR IN METERS
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# SCALE FACTOR -- EARTH +29, MOON +27
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# (2) VVEC VELOCITY VECTORY IN METERS/CENTISECOND
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# (2) VVEC VELOCITY VECTOR IN METERS/CENTISECOND
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# SCALE FACTOR -- EARTH +7, MOON +5
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# (3) X1 PRIMARY BODY INDICATOR
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# EARTH -2, MOON -10
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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 COMPUTE THE LANDING SITE
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# ORIENTATION 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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@ -2105,7 +2105,7 @@ R56A1 CAF VB53 # DISPLAY V53 REQUESTING ALTERNATE MARK
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# Page 782
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CADR GOMARK2
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TCF GOTOP00H # V34: TERMINATE
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TCF R56A1 # V33: DON'T PROCEED -- JUST ENTER TO MARK
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TCF R56A1 # V33: DONT PROCEED -- JUST ENTER TO MARK
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TC INTPRET
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DLOAD
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MRKBUF1 +3
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@ -1358,7 +1358,7 @@ OPDEGOUT CCS MPAC # RANGE IS 90 DEG
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TC NEGOPT # IF NEG NON ZERO
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AD NEG1 # IF NEG ZERO SUBTRACT 1
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AD 20BIAS
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BIASCOM TS MPAC # TEST FOR OVEFLOW
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BIASCOM TS MPAC # TEST FOR OVERFLOW
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TC +3 # NO OVFLOW
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CAF BIT15 # IF OVFLOW
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ADS MPAC
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@ -2187,7 +2187,7 @@ HMSIN TC ALL3DEC # IF ALL 3 WORDS WERE NOT LOADED, ALARM.
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MP MINCON # LEAVES MINUTES CONTRIBUTION IN A,L
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# Page 353
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DAS HITEMIN # ADD IN MINUTES CONTRIBUTION
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EXTEND # IF THIS DAS OVEFLOWS, G/ 745 HR, 39MIN
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EXTEND # IF THIS DAS OVERFLOWS, G/ 745 HR, 39MIN
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BZF +2
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TC ALMCYCLE
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CA ZREG # PUT ZREG, ZREGLP INTO MPAC +1.
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@ -171,7 +171,7 @@ CDUINC TS TEM2 # 1'S COMPL. QUANT. ARRIVES IN ACC. STORE IT
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AD ONE
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TCF +4
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AD ONE
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AD ONE # OVEFLOW HERE IF 2'S COMPL. IS 180 DEG.
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AD ONE # OVERFLOW HERE IF 2'S COMPL. IS 180 DEG.
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COM
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AD TEM2 # SULT MOVES FROM 2ND TO 3D QUAD. (OR BACK)
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@ -250,7 +250,7 @@ TRANSP2 CAF XNB1EB
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# 2. GENERATE IN MPAC THE SIGNUM FUNCTION OF MPAC:
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# ENTRY: RTB
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# SIGNMPAC
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# IN EITHER CASE, RETURN IS TO TEH NEXT INTERPRETIVE INSTRUCTION IN THE CALLING SEQUENCE.
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# IN EITHER CASE, RETURN IS TO THE NEXT INTERPRETIVE INSTRUCTION IN THE CALLING SEQUENCE.
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SIGNMPAC EXTEND
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DCA DPOSMAX
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@ -199,7 +199,7 @@ ATTINIT CAE DAPDATR1 # ATTITUDE-ERROR INITIALIZATION LOGIC
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+8 CCS TTMP1 # TEST TEMPORARY COUNTER
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TCF ATTINIT +5 # BACK TO REPEAT FOR PITCH ERROR
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CA ERRBTMP # ERROS ESTABLISHED AND LIMITED
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CA ERRBTMP # ERRORS ESTABLISHED AND LIMITED
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TS PERRB
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CA ERRBTMP +1
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TS YERRB
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@ -123,7 +123,7 @@
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# CONTROL ACCELERATION CONACC, OR ITS RECIPROCAL, 1/CONACC, THE TVC
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# ROLL DAP GAIN (SEE TVCEXECUTIVE VARIABLE GAIN PACKAGE). JET
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# FIRING TIME IS SIMPLY THAT REQUIRED TO ACHIEVE THE DESIRED OGARATE,
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# SUBJECT TO TEH LIMITATIONS DISCUSSED UNDER FUNCTIONAL DESCRIPTION,
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# SUBJECT TO THE LIMITATIONS DISCUSSED UNDER FUNCTIONAL DESCRIPTION,
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# ABOVE.
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#
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# THE THREE CONTROL REGIONS (+, -, AND ZERO TORQUE) ARE COMPRISED OF
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@ -150,7 +150,7 @@
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# SECOND INTERVALS) WILL BENEFIT FROM THE CONVERGENT NATURE OF THE
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# APPROXIMATION.
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#
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# FOR LARGE OGAERROR THE TANGENT INTERSECTS +-MINLIM SWITCH BOUNDARY BEFORE
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# FOR LARGE OGAERROR THE TANGENT INTERSECTS +-MINLIM SWITCH BOUNDRY BEFORE
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# INTERSECTING THE STRAIGHT LINE SWITCH. HOWEVER THE MINLIM IS
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# IGNORED IN COMPUTING THE FIRING TIME, SO THAT THE EXTENSION (INTO
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# THE COAST REGION) OF THE STRAIGHT LINE SWITCH IS WHAT IS FIRED TO.
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@ -381,7 +381,7 @@ TIMEDIDL EXTEND
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TIMEDIDR INHINT
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CAF ZERO
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ZL # PICK UP INCRMENTER (AND ZERO
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ZL # PICK UP INCREMENTER (AND ZERO
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TS MPAC +2 # IT IN CASE OF RESTARTS) AND
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DXCH UPBUFF +8D # STORE IT
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DXCH MPAC # INTO MPAC FOR TPAGREE.
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@ -34,8 +34,8 @@
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## At the get-together of the AGC developers celebrating the 40th anniversary
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## of the first moonwalk, Don Eyles (one of the authors of this routine along
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## with Peter Adler) has related to us a little interesting history behind the
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## naming of the routine.
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##
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## naming of the routine.<br>
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## <br>
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## It traces back to 1965 and the Los Angeles riots, and was inspired
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## by disc jockey extraordinaire and radio station owner Magnificent Montague.
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## Magnificent Montague used the phrase "Burn, baby! BURN!" when spinning the
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@ -30,7 +30,7 @@
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# COELLIPTIC SEQUENCE INITIATION (CSI) PROGRAMS (P32 AND P72)
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#
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# MOD NO -1 LOG SECTION -- P32-P35, P72-P75
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# MOD BY WHITE.P DATE 1JUNE67
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# MOD BY WHITE, P. DATE 1JUNE67
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#
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# PURPOSE
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@ -129,7 +129,7 @@ CDUINC TS TEM2 # 1S COMPL.QUANT. ARRIVES IN ACC. STORE IT
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TCF +4
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AD ONE
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# Page 1399
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AD ONE # OVEFLOW HERE IF 2S COMPL. IS 180 DEG.
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AD ONE # OVERFLOW HERE IF 2S COMPL. IS 180 DEG.
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COM
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AD TEM2 # SULT MOVES FROM 2ND TO 3D QUAD. (OR BACK)
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@ -167,7 +167,7 @@ PULSEIMU INDEX FIXLOC # ADDRESS OF GYRO COMMANDS SHOULD BE IN X1
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# 2. GENERATE IN MPAC THE SIGNUM FUNCTION OF MPAC:
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# ENTRY: RTB
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# SIGNMPAC
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# IN EITHER CASE, RETURN IS TO TEH NEXT INTERPRETIVE INSTRUCTION IN THE CALLING SEQUENCE.
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# IN EITHER CASE, RETURN IS TO THE NEXT INTERPRETIVE INSTRUCTION IN THE CALLING SEQUENCE.
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SIGNMPAC EXTEND
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DCA DPOSMAX
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