Co-authored-by: James Harris <wopian@wopian.me>
This commit is contained in:
Leandro Matheus
GitHub
parent
7c7680fcc4
commit
6f7d132239
@ -25,32 +25,31 @@
|
|||||||
# 16:27 JULY 14, 1969
|
# 16:27 JULY 14, 1969
|
||||||
|
|
||||||
# Page 1140
|
# Page 1140
|
||||||
# ***** RP-TO-R SUBROUTINE *****
|
# ..... RP-TO-R SUBROUTINE .....
|
||||||
# SUBROUTINE TO CONVERT RP (VECTOR IN PLANETARY COORDINATE SYSTEM, EITHER
|
# SUBROUTINE TO CONVERT RP (VECTOR IN PLANETARY COORDINATE SYSTEM,EITHER
|
||||||
# EARTH-FIXED OR MOON-FIXED) TO R (SAME VECTOR IN THE BASIC REF. SYSTEM)
|
# EARTH-FIXED OR MOON-FIXED) TO R (SAME VECTOR IN THE BASIC REF. SYSTEM)
|
||||||
#
|
#
|
||||||
# R = MT(T) * (RP + LP X RP) MT = M MATRIX TRANSPOSE
|
# R=MT(T)*(RP+LPXRP) MT= M MATRIX TRANSPOSE
|
||||||
#
|
#
|
||||||
# CALLING SEQUENCE
|
# CALLING SEQUENCE
|
||||||
# L CALL
|
# L CALL
|
||||||
# L+1 RP-TO-R
|
# L+1 RP-TO-R
|
||||||
#
|
#
|
||||||
# SUBROUTINES USED
|
# SUBROUTINES USED
|
||||||
# EARTHMX, MOONMX, EARTHL
|
# EARTHMX,MOONMX,EARTHL
|
||||||
#
|
|
||||||
# ITEMS AVAILABLE FROM LAUNCH DATA
|
|
||||||
# 504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
|
|
||||||
# IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
|
|
||||||
#
|
#
|
||||||
|
# ITEMS AVAILABLE FROM LAUNCH DATA
|
||||||
|
# 504LM= THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL,EXPRESSED
|
||||||
|
# IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
|
||||||
# ITEMS NECESSARY FOR SUBR. USED (SEE DESCRIPTION OF SUBR.)
|
# ITEMS NECESSARY FOR SUBR. USED (SEE DESCRIPTION OF SUBR.)
|
||||||
#
|
#
|
||||||
# INPUT
|
# INPUT
|
||||||
# MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
|
# MPAC= 0 FOR EARTH,NON-ZERO FOR MOON
|
||||||
# 0-5D = RP VECTOR
|
# 0-5D= RP VECTOR
|
||||||
# 6-7D = TIME
|
# 6-7D= TIME
|
||||||
#
|
#
|
||||||
# OUTPUT
|
# OUTPUT
|
||||||
# MPAC = R VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
|
# MPAC= R VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
|
||||||
|
|
||||||
SETLOC PLANTIN1
|
SETLOC PLANTIN1
|
||||||
BANK
|
BANK
|
||||||
@ -84,32 +83,31 @@ RPTORA CALL # EARTH COMPUTATIONS
|
|||||||
COUNT* $$/LUROT
|
COUNT* $$/LUROT
|
||||||
|
|
||||||
# Page 1142
|
# Page 1142
|
||||||
# ***** R-TO-RP SUBROUTINE *****
|
# ..... R-TO-RP SUBROUTINE .....
|
||||||
# SUBROUTINE TO CONVERT R (VECTOR IN REFERENCE COORD. SYSTEM) TO RP
|
# SUBROUTINE TO CONVERT R (VECTOR IN REFERENCE COORD. SYSTEM) TO RP
|
||||||
# (VECTOR IN PLANETARY COORD SYSTEM) EITHER EARTH-FIXED OR MOON-FIXED
|
# (VECTOR IN PLANETARY COORD SYSTEM) EITHER EARTH-FIXED OR MOON-FIXED
|
||||||
#
|
#
|
||||||
# RP = M(T) * (R - L X R)
|
# RP=M(T)*(R-LXR)
|
||||||
#
|
#
|
||||||
# CALLING SEQUENCE
|
# CALLING SEQUENCE
|
||||||
# L CALL
|
# L CALL
|
||||||
# L+1 R-TO-RP
|
# L+1 R-TO-RP
|
||||||
#
|
#
|
||||||
# SUBROUTINES USED
|
# SUBROUTINES USED
|
||||||
# EARTHMX, MOONMX, EARTHL
|
# EARTHMX,MOONMX,EARTHL
|
||||||
#
|
#
|
||||||
# INPUT
|
# INPUT
|
||||||
# MPAC = 0 FOR EARTH, NON-ZERO FOR MOON
|
# MPAC= 0 FOR EARTH, NON-ZERO FOR MOON
|
||||||
# 0-5D = R VECTOR
|
# 0-5D= R VECTOR
|
||||||
# 6-7D = TIME
|
# 6-7D= TIME
|
||||||
#
|
|
||||||
# ITEMS AVAILABLE FROM LAUNCH DATA
|
|
||||||
# 504LM = THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL, EXPRESSED
|
|
||||||
# IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
|
|
||||||
#
|
#
|
||||||
|
# ITEMS AVAILABLE FROM LAUNCH DATA
|
||||||
|
# 504LM= THE LIBRATION VECTOR L OF THE MOON AT TIME TIMSUBL,EXPRESSED
|
||||||
|
# IN THE MOON-FIXED COORD. SYSTEM RADIANS B0
|
||||||
# ITEMS NECESSARY FOR SUBROUTINES USED (SEE DESCRIPTION OF SUBR.)
|
# ITEMS NECESSARY FOR SUBROUTINES USED (SEE DESCRIPTION OF SUBR.)
|
||||||
#
|
#
|
||||||
# OUTPUT
|
# OUTPUT
|
||||||
# MPAC = RP VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
|
# MPAC=RP VECTOR METERS B-29 FOR EARTH, B-27 FOR MOON
|
||||||
|
|
||||||
R-TO-RP STQ BHIZ
|
R-TO-RP STQ BHIZ
|
||||||
RPREXIT
|
RPREXIT
|
||||||
@ -119,11 +117,11 @@ R-TO-RP STQ BHIZ
|
|||||||
VLOAD VXM
|
VLOAD VXM
|
||||||
504LM # LP=LM
|
504LM # LP=LM
|
||||||
MMATRIX
|
MMATRIX
|
||||||
VSL1 # L = MT(T)*LP RADIANS B0
|
VSL1 # L=MT(T)*LP RADIANS B0
|
||||||
RTORPB VXV BVSU
|
RTORPB VXV BVSU
|
||||||
504RPR
|
504RPR
|
||||||
504RPR
|
504RPR
|
||||||
MXV # M(T)*(R-LXR) B-2
|
MXV # M(T)*(R-LXR) B-2
|
||||||
MMATRIX
|
MMATRIX
|
||||||
RPRPXXXX VSL1 SETPD
|
RPRPXXXX VSL1 SETPD
|
||||||
0D
|
0D
|
||||||
@ -133,74 +131,73 @@ RTORPA CALL # EARTH COMPUTATIONS
|
|||||||
EARTHMX
|
EARTHMX
|
||||||
CALL
|
CALL
|
||||||
EARTHL
|
EARTHL
|
||||||
GOTO # MPAC=L=(-AX,-AY,0) RAD B-0
|
GOTO # MPAC=L=(-AX,-AY,0) RAD B-0
|
||||||
RTORPB
|
RTORPB
|
||||||
|
|
||||||
# Page 1143
|
# Page 1143
|
||||||
# ***** MOONMX SUBROUTINE *****
|
# ..... MOONMX SUBROUTINE .....
|
||||||
# SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE MOON
|
# SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE MOON
|
||||||
#
|
#
|
||||||
# CALLING SEQUENCE
|
# CALLING SEQUENCE
|
||||||
# L CALL
|
# L CALL
|
||||||
# L+1 MOONMX
|
# L+1 MOONMX
|
||||||
#
|
#
|
||||||
# SUBROUTINES USED
|
# SUBROUTINES USED
|
||||||
# NEWANGLE
|
# NEWANGLE
|
||||||
#
|
#
|
||||||
# INPUT
|
# INPUT
|
||||||
# 6-7D = TIME
|
# 6-7D= TIME
|
||||||
#
|
# ITEMS AVAILABLE FROM LAUNCH DATA
|
||||||
# ITEMS AVAILABLE FROM LAUNCH DATA
|
# BSUBO,BDOT
|
||||||
# BSUBO, BDOT
|
# TIMSUBO,NODIO,NODDOT,FSUBO,FDOT
|
||||||
# TIMSUBO, NODIO, NODDOT, FSUBO, FDOT
|
# COSI= COS(I) B-1
|
||||||
# COSI = COS(I) B-1
|
# SINI= SIN(I) B-1
|
||||||
# SINI = SIN(I) B-1
|
# I IS THE ANGLE BETWEEN THE MEAN LUNAR EQUATORIAL PLANE AND THE
|
||||||
# I IS THE ANGLE BETWEEN THE MEAN LUNAR EQUATORIAL PLANE AND THE
|
# PLANE OF THE ECLIPTIC (1 DEGREE 32.1 MINUTES)
|
||||||
# PLANE OF THE ECLIPTIC (1 DEGREE 32.1 MINUTES)
|
|
||||||
#
|
#
|
||||||
# OUTPUT
|
# OUTPUT
|
||||||
# MMATRIX = 3X3 M MATRIX B-1 (STORED IN VAC AREA)
|
# MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
|
||||||
|
|
||||||
MOONMX STQ SETPD
|
MOONMX STQ SETPD
|
||||||
EARTHMXX
|
EARTHMXX
|
||||||
8D
|
8D
|
||||||
AXT,1 # B REQUIRES SL 0, SL 5 IN NEWANGLE
|
AXT,1 # B REQUIRES SL 0, SL 5 IN NEWANGLE
|
||||||
5
|
5
|
||||||
DLOAD PDDL # PD 10D 8-9D=BSUBO
|
DLOAD PDDL # PD 10D 8-9D=BSUBO
|
||||||
BSUBO # 10-11D=BDOT
|
BSUBO # 10-11D= BDOT
|
||||||
BDOT
|
BDOT
|
||||||
PUSH CALL # PD 12D
|
PUSH CALL # PD 12D
|
||||||
NEWANGLE # EXIT WITH PD 8D AND MPAC= B REVS B0
|
NEWANGLE # EXIT WITH PD 8D AND MPAC= B REVS B0
|
||||||
PUSH COS # PD 10D
|
PUSH COS # PD 10D
|
||||||
STODL COB # PD 8D COS(B) B-1
|
STODL COB # PD 8D COS(B) B-1
|
||||||
SIN # SIN(B) B-1
|
SIN # SIN(B) B-1
|
||||||
STODL SOB # SETUP INPUT FOR NEWANGLE
|
STODL SOB # SETUP INPUT FOR NEWANGLE
|
||||||
FSUBO # 8-9D=FSUBO
|
FSUBO # 8-9D=FSUBO
|
||||||
PDDL PUSH # PD 10D THEN 12D 10-11D=FDOT
|
PDDL PUSH # PD 10D THEN 12D 10-11D=FDOT
|
||||||
FDOT
|
FDOT
|
||||||
AXT,1 CALL # F REQUIRES SL 1, SL 6 IN NEWANGLE.
|
AXT,1 CALL # F REQUIRES SL 1, SL 6 IN NEWANGLE
|
||||||
4
|
4
|
||||||
NEWANGLE # EXIT WITH PD 8D AND MPAC= F REVS B0
|
NEWANGLE # EXIT WITH PD 8D AND MPAC= F REVS B0
|
||||||
STODL AVECTR +2 # SAVE F TEMP
|
STODL AVECTR +2 # SAVE F TEMP
|
||||||
NODIO # 8-9D=NODIO
|
NODIO # 8-9D=NODIO
|
||||||
PDDL PUSH # PD 10D THEN 12D 10-11D=NODDOT
|
PDDL PUSH # PD 10D THEN 12D 10-11D=NODDOT
|
||||||
NODDOT # MPAC=T
|
NODDOT # MPAC=T
|
||||||
AXT,1 CALL # NODE REQUIRES SL 0, SL 5 IN NEWANGLE
|
AXT,1 CALL # NODE REQUIRES SL 0, SL 5 IN NEWANGLE
|
||||||
5
|
5
|
||||||
NEWANGLE # EXIT WITH PD 8D AND MPAC= NODI REVS B0
|
NEWANGLE # EXIT WITH PD 8D AND MPAC= NODI REVS B0
|
||||||
# Page 1144
|
# Page 1144
|
||||||
PUSH COS # PD 10D 8-9D= NODI REVS B0
|
PUSH COS # PD 10D 8-9D= NODI REVS B0
|
||||||
PUSH # PD 12D 10-11D= COS(NODI) B-1
|
PUSH # PD 12D 10-11D= COS(NODI) B-1
|
||||||
STORE AVECTR
|
STORE AVECTR
|
||||||
DMP SL1R
|
DMP SL1R
|
||||||
COB # COS(NODI) B-1
|
COB # COS(NODI) B-1
|
||||||
STODL BVECTR +2 # PD 10D 20-25D=AVECTR= COB*SIN(NODI)
|
STODL BVECTR +2 # PD 10D 20-25D=AVECTR= COB*SIN(NODI)
|
||||||
DMP SL1R # SOB*SIN(NODI)
|
DMP SL1R # SOB*SIN(NODI)
|
||||||
SOB
|
SOB
|
||||||
STODL BVECTR +4 # PD 8D
|
STODL BVECTR +4 # PD 8D
|
||||||
SIN PUSH # PD 10D -SIN(NODI) B-1
|
SIN PUSH # PD 10D -SIN(NODI) B-1
|
||||||
DCOMP # 26-31D=BVECTR= COB*COS(NODI)
|
DCOMP # 26-31D=BVECTR= COB*COS(NODI)
|
||||||
STODL BVECTR # PD 8D SOB*COS(NODI)
|
STODL BVECTR # PD 8D SOB*COS(NODI)
|
||||||
AVECTR +2 # MOVE F FROM TEMP LOC. TO 504F
|
AVECTR +2 # MOVE F FROM TEMP LOC. TO 504F
|
||||||
STODL 504F
|
STODL 504F
|
||||||
DMP SL1R
|
DMP SL1R
|
||||||
@ -214,30 +211,30 @@ MOONMX STQ SETPD
|
|||||||
COUNT* $$/LUROT
|
COUNT* $$/LUROT
|
||||||
|
|
||||||
MOONMXA STODL AVECTR +2
|
MOONMXA STODL AVECTR +2
|
||||||
SINNODI # 8-9D=SIN(NODI) B-1
|
SINNODI # 8-9D=SIN(NODI) B-1
|
||||||
DMP SL1R
|
DMP SL1R
|
||||||
SOB
|
SOB
|
||||||
STODL AVECTR +4 # 0
|
STODL AVECTR +4 # 0
|
||||||
HI6ZEROS # 8-13D= CVECTR= -SOB B-1
|
HI6ZEROS # 8-13D= CVECTR= -SOB B-1
|
||||||
PDDL DCOMP # PD 10D COB
|
PDDL DCOMP # PD 10D COB
|
||||||
SOB
|
SOB
|
||||||
PDDL PDVL # PD 12D THEN PD 14D
|
PDDL PDVL # PD 12D THEN PD 14D
|
||||||
COB
|
COB
|
||||||
BVECTR
|
BVECTR
|
||||||
VXSC PDVL # PD 20D BVECTR*SINI B-2
|
VXSC PDVL # PD 20D BVECTR*SINI B-2
|
||||||
SINI
|
SINI
|
||||||
CVECTR
|
CVECTR
|
||||||
VXSC VAD # PD 14D CVECTR*COSI B-2
|
VXSC VAD # PD 14D CVECTR*COSI B-2
|
||||||
COSI
|
COSI
|
||||||
VSL1
|
VSL1
|
||||||
STOVL MMATRIX +12D # PD 8D M2=BVECTR*SINI+CVECTR*COSI B-1
|
STOVL MMATRIX +12D # PD 8D M2=BVECTR*SINI+CVECTR*COSI B-1
|
||||||
VXSC PDVL # PD 14D
|
VXSC PDVL # PD 14D
|
||||||
SINI # CVECTR*SINI B-2
|
SINI # CVECTR*SINI B-2
|
||||||
BVECTR
|
BVECTR
|
||||||
VXSC VSU # PD 8D BVECTR*COSI B-2
|
VXSC VSU # PD 8D BVECTR*COSI B-2
|
||||||
COSI
|
COSI
|
||||||
VSL1 PDDL # PD 14D
|
VSL1 PDDL # PD 14D
|
||||||
504F # 8-13D=DVECTR=BVECTR*COSI-CVECTR*SINI B-1
|
504F # 8-13D=DVECTR=BVECTR*COSI-CVECTR*SINI B-1
|
||||||
COS VXSC
|
COS VXSC
|
||||||
# Page 1145
|
# Page 1145
|
||||||
DVECTR
|
DVECTR
|
||||||
@ -256,13 +253,12 @@ MOONMXA STODL AVECTR +2
|
|||||||
VSL1 VCOMP
|
VSL1 VCOMP
|
||||||
STCALL MMATRIX # M0= -(AVECTR*COSF+DVECTR*SINF) B-1
|
STCALL MMATRIX # M0= -(AVECTR*COSF+DVECTR*SINF) B-1
|
||||||
EARTHMXX
|
EARTHMXX
|
||||||
|
|
||||||
# COMPUTE X=X0+(XDOT)(T+T0)
|
# COMPUTE X=X0+(XDOT)(T+T0)
|
||||||
# 8-9D= X0 (REVS B-0), PUSHLOC SET AT 12D
|
# 8-9D= X0 (REVS B-0),PUSHLOC SET AT 12D
|
||||||
# 10-11D=XDOT (REVS/CSEC) SCALED B+23 FOR WEARTH,B+28 FOR NODDOT AND BDOT
|
# 10-11D=XDOT (REVS/CSEC) SCALED B+23 FOR WEARTH,B+28 FOR NODDOT AND BDOT
|
||||||
# AND B+27 FOR FDOT
|
# AND B+27 FOR FDOT
|
||||||
# X1=DIFFERENCE IN 23 AND SCALING OF XDOT, =0 FOR WEARTH, 5 FOR NDDOT AND
|
# X1=DIFFERENCE IN 23 AND SCALING OF XDOT,=0 FOR WEARTH,5 FOR NODDOT AND
|
||||||
# BDOT AND 4 FOR FDOT
|
# BDOT AND 4 FOR FDOT
|
||||||
# 6-7D=T (CSEC B-28), TIMSUBO= (CSEC B-42 TRIPLE PREC.)
|
# 6-7D=T (CSEC B-28), TIMSUBO= (CSEC B-42 TRIPLE PREC.)
|
||||||
|
|
||||||
NEWANGLE DLOAD SR # ENTER PD 12D
|
NEWANGLE DLOAD SR # ENTER PD 12D
|
||||||
@ -273,58 +269,58 @@ NEWANGLE DLOAD SR # ENTER PD 12D
|
|||||||
MPAC
|
MPAC
|
||||||
STODL TIMSUBM # T+T0 CSEC B-42
|
STODL TIMSUBM # T+T0 CSEC B-42
|
||||||
TIMSUBM +1
|
TIMSUBM +1
|
||||||
DMP # PD 10D MULT BY XDOT IN 10-11D
|
DMP # PD 10D MULT BY XDOT IN 10-11D
|
||||||
SL* DAD # PD 8D ADD X0 IN 8-9D AFTER SHIFTING
|
SL* DAD # PD 8D ADD X0 IN 8-9D AFTER SHIFTING
|
||||||
5,1 # SUCH THAT SCALING IS B-0
|
5,1 # SUCH THAT SCALING IS B-0
|
||||||
PUSH SLOAD # PD 10D SAVE PARTIAL (X0+XDOT*T) IN 8-9D
|
PUSH SLOAD # PD 10D SAVE PARTIAL (X0+XDOT*T) IN 8-9D
|
||||||
TIMSUBM
|
TIMSUBM
|
||||||
SL DMP
|
SL DMP
|
||||||
9D
|
9D
|
||||||
10D # XDOT
|
10D # XDOT
|
||||||
SL* DAD # PD 8D SHIFT SUCH THAT THIS PART OF X
|
SL* DAD # PD 8D SHIFT SUCH THAT THIS PART OF X
|
||||||
10D,1 # IS SCALED REVS/CSEC B-0
|
10D,1 # IS SCALED REVS/CSEC B-0
|
||||||
BOV # TURN OFF OVERFLOW IF SET BY SHIFT
|
BOV # TURN OFF OVERFLOW IF SET BY SHIFT
|
||||||
+1 # INSTRUCTION BEFORE EXITING.
|
+1 # INSTRUCTION BEFORE EXITING
|
||||||
RVQ # MPAC=X= X0+(XDOT)(T+T0) REVS B0
|
RVQ # MPAC=X= X0+(XDOT)(T+T0) REVS B0
|
||||||
|
|
||||||
# Page 1146
|
# Page 1146
|
||||||
# ***** EARTHMX SUBROUTINE *****
|
# ..... EARTHMX SUBROUTINE .....
|
||||||
# SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE EARTH
|
# SUBROUTINE TO COMPUTE THE TRANSFORMATION MATRIX M FOR THE EARTH
|
||||||
#
|
#
|
||||||
# CALLING SEQUENCE
|
# CALLING SEQUENCE
|
||||||
# L CALL
|
# L CALL
|
||||||
# L+1 EARTHMX
|
# L+1 EARTHMX
|
||||||
#
|
#
|
||||||
# SUBROUTINE USED
|
# SUBROUTINE USED
|
||||||
# NEWANGLE
|
# NEWANGLE
|
||||||
#
|
#
|
||||||
# INPUT
|
# INPUT
|
||||||
# INPUT AVAILABLE FROM LAUNCH DATA AZO REVS B-0
|
# INPUT AVAILABLE FROM LAUNCH DATA AZO REVS B-0
|
||||||
# TEPHEM CSEC B-42
|
# TEPHEM CSEC B-42
|
||||||
# 6-7D= TIME CSEC B-28
|
# 6-7D= TIME CSEC B-28
|
||||||
#
|
#
|
||||||
# OUTPUT
|
# OUTPUT
|
||||||
# MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
|
# MMATRIX= 3X3 M MATRIX B-1 (STORED IN VAC AREA)
|
||||||
|
|
||||||
BANK 26
|
BANK 26
|
||||||
SETLOC PLANTIN1
|
SETLOC PLANTIN1
|
||||||
BANK
|
BANK
|
||||||
COUNT* $$/LUROT
|
COUNT* $$/LUROT
|
||||||
|
|
||||||
EARTHMX STQ SETPD # SET 8-9D=AZO
|
EARTHMX STQ SETPD # SET 8-9D=AZO
|
||||||
EARTHMXX
|
EARTHMXX
|
||||||
8D # 10-11D=WEARTH
|
8D # 10-11D=WEARTH
|
||||||
AXT,1 # FOR SL 5, AND SL 10 IN NEWANGLE
|
AXT,1 # FOR SL 5, AND SL 10 IN NEWANGLE
|
||||||
0
|
0
|
||||||
DLOAD PDDL # LEAVING PD SET AT 12D FOR NEWANGLE
|
DLOAD PDDL # LEAVING PD SET AT 12D FOR NEWANGLE
|
||||||
AZO
|
AZO
|
||||||
WEARTH
|
WEARTH
|
||||||
PUSH CALL
|
PUSH CALL
|
||||||
NEWANGLE
|
NEWANGLE
|
||||||
SETPD PUSH # 18-19D=504AZ
|
SETPD PUSH # 18-19D=504AZ
|
||||||
18D # COS(AZ) SIN(AZ) 0
|
18D # COS(AZ) SIN(AZ) 0
|
||||||
COS PDDL # 20-37D= MMATRIX= -SIN(AZ) COS(AZ) 0 B-1
|
COS PDDL # 20-37D= MMATRIX= -SIN(AZ) COS(AZ) 0 B-1
|
||||||
504AZ # 0 0 1
|
504AZ # 0 0 1
|
||||||
SIN PDDL
|
SIN PDDL
|
||||||
HI6ZEROS
|
HI6ZEROS
|
||||||
PDDL SIN
|
PDDL SIN
|
||||||
@ -339,20 +335,20 @@ EARTHMX STQ SETPD # SET 8-9D=AZO
|
|||||||
EARTHMXX
|
EARTHMXX
|
||||||
|
|
||||||
# Page 1147
|
# Page 1147
|
||||||
# ***** EARTHL SUBROUTINE *****
|
# ..... EARTHL SUBROUTINE .....
|
||||||
# SUBROUTINE TO COMPUTE L VECTOR FOR EARTH
|
# SUBROUTINE TO COMPUTE L VECTOR FOR EARTH
|
||||||
#
|
#
|
||||||
# CALLING SEQUENCE
|
# CALLING SEQUENCE
|
||||||
# L CALL
|
# L CALL
|
||||||
# L+1 EARTHL
|
# L+1 EARTHL
|
||||||
#
|
#
|
||||||
# INPUT
|
# INPUT
|
||||||
# AXO,AYO SET AT LAUNCH TIME WITH AYO IMMEDIATELY FOLLOWING AXO IN CORE
|
# AXO,AYO SET AT LAUNCH TIME WITH AYO IMMEDIATELY FOLLOWING AXO IN CORE
|
||||||
#
|
#
|
||||||
# OUTPUT
|
# OUTPUT
|
||||||
# -AX
|
# -AX
|
||||||
# MPAC= -AY RADIANS B-0
|
# MPAC= -AY RADIANS B-0
|
||||||
# 0
|
# 0
|
||||||
|
|
||||||
BANK 06
|
BANK 06
|
||||||
SETLOC EARTHLOC
|
SETLOC EARTHLOC
|
||||||
@ -371,21 +367,19 @@ EARTHL DLOAD DCOMP
|
|||||||
|
|
||||||
# Page 1148
|
# Page 1148
|
||||||
# CONSTANTS AND ERASABLE ASSIGNMENTS
|
# CONSTANTS AND ERASABLE ASSIGNMENTS
|
||||||
|
|
||||||
1B1 = DP1/2 # 1 SCALED B-1
|
1B1 = DP1/2 # 1 SCALED B-1
|
||||||
RPREXIT = S1 # R-TO-RP AND RP-TO-R SUBR EXIT
|
RPREXIT = S1 # R-TO-RP AND RP-TO-R SUBR EXIT
|
||||||
EARTHMXX = S2 # EARTHMX, MOONMX SUBR. EXITS
|
EARTHMXX = S2 # EARTHMX,MOONMX SUBR. EXITS
|
||||||
504RPR = 0D # 6 REGS R OR RP VECTOR
|
504RPR = 0D # 6 REGS R OR RP VECTOR
|
||||||
SINNODI = 8D # 2 SIN(NODI)
|
SINNODI = 8D # 2 SIN(NODI)
|
||||||
DVECTR = 8D # 6 D VECTOR MOON
|
DVECTR = 8D # 6 D VECTOR MOON
|
||||||
CVECTR = 8D # 6 C VECTR MOON
|
CVECTR = 8D # 6 C VECTR MOON
|
||||||
504AZ = 18D # 2 AZ
|
504AZ = 18D # 2 AZ
|
||||||
TIMSUBM = 14D # 3 TIME SUB M (MOON) T+T0 IN GETAZ
|
TIMSUBM = 14D # 3 TIME SUB M (MOON) T+T0 IN GETAZ
|
||||||
504LPL = 14D # 6 L OR LP VECTOR
|
504LPL = 14D # 6 L OR LP VECTOR
|
||||||
AVECTR = 20D # 6 A VECTOR (MOON)
|
AVECTR = 20D # 6 A VECTOR (MOON)
|
||||||
BVECTR = 26D # 6 B VECTOR (MOON)
|
BVECTR = 26D # 6 B VECTOR (MOON)
|
||||||
MMATRIX = 20D # 18 M MATRIX
|
MMATRIX = 20D # 18 M MATRIX
|
||||||
COB = 32D # 2 COS(B) B-1
|
COB = 32D # 2 COS(B) B-1
|
||||||
SOB = 34D # 2 SIN(B) B-1
|
SOB = 34D # 2 SIN(B) B-1
|
||||||
504F = 6D # 2 F(MOON)
|
504F = 6D # 2 F (MOON)
|
||||||
|
|
||||||
|
|||||||
Loading…
Reference in New Issue
Block a user