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pages 0692-0702
This commit is contained in:
Chyanne Haugen
parent
35f3495c34
commit
e346724c13
1 changed files with 41 additions and 39 deletions
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@ -1403,7 +1403,7 @@ INITVELX LXA,1 DLOAD*
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HALFREV 2DEC 1 B-1
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GET+MGA VLOAD UNIT # (PL 0D) V (+7) TO MPAC UNITIZE UV (+1)
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GET+MGA VLOAD UNIT # (PL 0D) V (+7) TO MPAC, UNITIZE UV (+1)
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UNIT
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DOT SL1 # DOT UV WITH Y(STABLE MEMBER) AND RESCALE
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REFSMMAT +6 # FROM +2 TO +1 FOR ASIN ROUTINE
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@ -1415,7 +1415,7 @@ GET+MGA VLOAD UNIT # (PL 0D) V (+7) TO MPAC UNITIZE UV (+1)
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SETMGA STORE +MGA
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CLR RVQ # CLEAR MGLVFLAG TO INDICATE +MGA CALC
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MGLVFLAG # AND EXIT
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GET.LVC VLOAD UNIT # (PL 6D) R (+29) IN MPAC UNITIZE UR
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GET.LVC VLOAD UNIT # (PL 6D) R (+29) IN MPAC, UNITIZE UR
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RINIT
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VCOMP # U(-R)
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STORE 18D # U(-R) TO 18D
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@ -1468,14 +1468,14 @@ RTRNMU STORE RTMU
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# Page 694
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# ***** PERIAPO *****
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#
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# MOD NO -1 LOG SECTION -- P34-P35, P74-P75
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# MOD BY WHITE, P. DATE 18 JAN 68
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# MOD NO -1 LOG SECTION - P34-P35, P74-P75
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# MOD BY WHITE.P DATE 18JAN68
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#
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# FUNCTIONAL DESCRIPTION
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#
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# THIS SUBROUTINE COMPUTES THE TWO BODY APOCENTER AND PERICENTER
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# ALTITUDES GIVEN THE POSITION AND VELOCITY VECTORS FOR A POINT ON
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# TRAJECTORY AND THE PRIMARY BODY.
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# THE TRAJECTORY AND THE PRIMARY BODY.
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#
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# SETRAD IS CALLED TO DETERMINE THE RADIUS OF THE PRIMARY BODY.
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#
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@ -1486,31 +1486,31 @@ RTRNMU STORE RTMU
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#
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# L CALL
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# L+1 PERIAPO
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# L+2 (RETURN -- ALWAYS)
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# L+2 (RETURN - ALWAYS)
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#
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# INPUT
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#
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# (1) RVEC POSITION VECTOR IN METERS
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# SCALE FACTOR -- EARTH +29, MOON +27
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# SCALE FACTOR - EARTH +29, MOON +27
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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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# SCALE FACTOR - EARTH +7, MOON +5
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# (3) X1 PRIMARY BODY INDICATOR
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# EARTH -1, MOON -10
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#
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# OUTPUT
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#
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# (1) 2D APOCENTER RADIUS IN METERS
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# SCALE FACTOR -- EARTH +29, MOON +27
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# SCALE FACTOR - EARTH +29, MOON +27
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# (2) 4D APOCENTER ALTITUDE IN METERS
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# SCALE FACTOR -- EARTH +29, MOON +27
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# SCALE FACTOR - EARTH +29, MOON +27
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# (3) 6D PERICENTER RADIUS IN METERS
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# SCALE FACTOR -- EARTH +29, MOON +27
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# SCALE FACTOR - EARTH +29, MOON +27
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# (4) 8D PERICENTER ALTITUDE IN METERS
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# SCALE FACTOR -- EARTH +29, MOON +27
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# SCALE FACTOR - EARTH +29, MOON +27
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# (5) ECC ECCENTRICITY OF CONIC TRAJECTORY
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# SCALE FACTOR -- +3
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# SCALE FACTOR - +3
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# (6) XXXALT RADIUS OF THE PRIMARY BODY IN METERS
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# SCALE FACTOR -- EARTH +29, MOON +27
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# SCALE FACTOR - EARTH +29, MOON +27
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# (7) PUSHLOC EQUALS 10D
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#
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# SUBROUTINES USED
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@ -1524,7 +1524,7 @@ RTRNMU STORE RTMU
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COUNT* $$/PERAP
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RPAD 2DEC 6373338 B-29 # STANDARD RADIUS OF PAD 37-B.
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RPAD 2DEC 6373338 B-29 # STANDARD RADIUS OF PAD 37-B.
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# = 20 909 901.57 FT
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PERIAPO1 LXA,2 VSR*
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@ -1620,44 +1620,45 @@ SHIFTR1 LXA,2 SL*
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# FUNCTIONAL DESCRIPTION
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#
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# TO DISPLAY AT ASTRONAUT REQUEST LGC CALCULATED RENDEZVOUS
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# OUT-OF-PLANE PARAMETERS (Y, YDOT, PSI). (REQUESTED BY DSKY).
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# OUT-OF-PLANE PARAMETERS (Y , YDOT , PSI). (REQUESTED BY DSKY).
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#
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# CALLING SEQUENCE
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#
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# ASTRONAUT REQUEST THROUGH DSKY V 90 E
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# ASTRONAUT REQUEST THROUGH DSKY V 90 E
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#
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# SUBROUTINES CALLED
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#
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# EXDSPRET
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# GOMARKF
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# CSMPREC
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# LEMPREC
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# SGNAGREE
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# LOADTIME
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# EXDSPRET
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# GOMARKF
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# CSMPREC
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# LEMPREC
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# SGNAGREE
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# LOADTIME
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#
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# NORMAL EXIT MODES
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#
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# ASTRONAUT REQUEST THROUGH DSKY TO TERMINATE PROGRAM V 34 E
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# ASTRONAUT REQUEST THROUGH DSKY TO TERMINATE PROGRAM V 34 E
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#
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# ALARM OR ABORT EXIT MODES
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#
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# NONE
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# NONE
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#
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# OUTPUT
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#
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# DECIMAL DISPLAY OF TIME, Y, YDOT AND PSI
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# DECIMAL DISPLAY OF TIME , Y , YDOT AND PSI
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#
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# DISPLAYED VALUES Y, YDOT, AND PSI, ARE STORED IN ERASABLE
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# REGISTERS RANGE, RRATE, AND RTHETA RESPECTIVELY.
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# DISPLAYED VALUES Y , YDOT , AND PSI , ARE STORED IN ERASABLE
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# REGISTERS RANGE , RRATE AND RTHETA RESPECTIVELY.
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#
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# ERASABLE INITIALIZATION REQUIRED
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#
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# CSM AND LEM STATE VECTORS
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# CSM AND LEM STATE VECTORS
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#
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# DEBRIS
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#
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# CENTRALS A,Q,L
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# OTHER: THOSE USED BY THE ABOVE LISTED SUBROUTINES
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# CENTRALS A,Q,L
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#
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# OTHER THOSE USED BY THE ABOVE LISTED SUBROUTINES
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BANK 20
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SETLOC R36LM
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@ -1690,8 +1691,9 @@ R36INT STCALL TDEC1
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RATT # _
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STORE RPASS36 # R
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UNIT PDVL # P
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# _
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VXV UNIT
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STADR # _
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STADR
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STODL UNP36 # U
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TAT
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STCALL TDEC1
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@ -1712,9 +1714,9 @@ R36INT STCALL TDEC1
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DOT SL1
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UNP36 # . _ _
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STOVL RRATE # Y = U . V
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06D # A
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06D # _ A _
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# Page 702
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# _ _
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UNIT PUSH # U = UNIT ( R ) 18D
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VXV VXV # RA A
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00D # _ _ _ _
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@ -1731,7 +1733,7 @@ R36INT STCALL TDEC1
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PUSH DOT # LOS PROJECTED INTO HORIZONTAL 12D
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00D # PLANE
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SL1 ARCCOS # _ _
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STOVL RTHETA # PSI = ARCCOS(U . U )
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STOVL RTHETA # PSI = ARCCOS(U .U )
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VXV DOT # A L
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00D
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BPL DLOAD
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@ -1745,15 +1747,15 @@ R36TAG2 DLOAD RTB
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SGNAGREE
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STORE DSPTEMX
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EXIT
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CAF V06N90N # DISPLAY Y, YDOT, AND PSI.
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CAF V06N90N # DISPLAY Y , YDOT , AND PSI.
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TC BANKCALL
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CADR GOMARKF
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TCF ENDEXT # TERMINATE
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TCF ENDEXT # PROCEED, END OF PROGRAM
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TCF R36 +3 # REDISPLAY OUTPUT
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TCF ENDEXT # PROCEED , END OF PROGRAM
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TCF R36 +3 # REDISPLAY OUTPUT
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LREGCHK XCH L
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EXTEND
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BZF ENTTIM2 # L-REG ZERO, SET TIME = PRESENT TIME
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BZF ENTTIM2 # L-REG ZERO ,SET TIME = PRESENT TIME
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XCH L # L-REG NON ZERO, TIME = ASTRO INPUT TIME
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TCF ASTROTIM
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ENTTIM2 TC INTPRET
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