VOYAGER
Voyager LECP Data Analysis Handbook
Instrument Modeling Reports
by Sheela Shodhan
E.9 TRAJRT2BDET5
**************************************************************************
* PURPOSE : THIS IS A FILE OF ROUTINES THAT HAVE BEEN DECLARED EXTERNAL *
* IN THE MAIN PROGRAM & WHICH ARE PASSED INTO THE ROUTINE *
* DHPCG THAT SOLVES THE SYSTEM OF DIFFERENTIAL EQUATIONS. *
* SUBROUTINES: *
* FCT : CALCULATES THE RIGHT HAND SIDE OF THE DIFFERENTIAL EQUATIONS *
* OUTP : EVERY OUTPUT POINT IN THE INTEGRATION PROCESS IS HANDED ONTO THI*
* -S ROUTINE BY THE DIFFERENTIAL EQUATION SOLVER DHPCG. THIS OUTPUT*
* POINT IS A POINT IN THE LINE-SEGMENT OF THE TRAJECTORY WHICH IS *
* THEN TESTED AGAINST THE VARIOUS SURFACES BY CALLING THE ROUTINE *
* 'CHECHIT' TO DETERMINE WHETHER THE PARTICLE HITS ANY OF THE SURFA*
* -CES AND LOST OR ESCAPED. TRAJECTORY CALCULATION CONTINUES UNTIL *
* THE FATE OF THE PARTICLE IS DETERMINED. *
**************************************************************************
SUBROUTINE FCT(X,Y,DERY)
* PURPOSE : TO COMPUTE THE RIGHT HAND SIDE DERY OF THE SYSTEM AT THE *
* GIVEN VALUES OF X & Y. *
**************************************************************************
IMPLICIT NONE
INTEGER NDIM
PARAMETER (NDIM=6)
REAL*8 BX,BY,BZ,DERY(NDIM),FAC,QMC,X,X00,Y(NDIM),Y00,Z00
COMMON /QMC/QMC
C COMMON /BX/BX,BY,BZ,/X00/X00,Y00,Z00
PARAMETER (FAC=0.02540005D0)
X00 = Y(1)/FAC
Y00 = Y(2)/FAC
Z00 = Y(3)/FAC
CALL FDMOD(X00,Y00,Z00,BX,BY,BZ)
D PRINT *,' QMC ',QMC
D PRINT *,' X00 ',X00,' Y00 ',Y00,' Z00 ',Z00
D PRINT *,' BX ',BX,' BY ',BY,' BZ ',BZ
DERY(1) = Y(4)
DERY(2) = Y(5)
DERY(3) = Y(6)
DERY(4) = QMC * (Y(5)*BZ - Y(6)*BY)
DERY(5) = QMC * (Y(6)*BX - Y(4)*BZ)
DERY(6) = QMC * (Y(4)*BY - Y(5)*BX)
RETURN
END
C----------------------------------------------------------------------
C----------------------------------------------------------------------
SUBROUTINE OUTP(X,Y,DERY,IHLF,NDIM,PRMT,HIT)
* PURPOSE : THIS IS A ROUTINE THAT IS DECLARED EXTERNAL IN THE MAIN *
* ROUTINE. IT PRINTS THE OUTPUT VALUES OBTAINED FROM THE ROUTINE *
* DHPCG - WHICH SOLVES THE SYSTEM OF DIFF. EQUATIONS. *
***********************************************************************
IMPLICIT NONE
CHARACTER*72 FNAME
INTEGER HIT,I,IHLF,MULC,MULC1,NCOUNT,NDIM,NSURF,NU
REAL*8 DERY(NDIM),PRMT(5),X,Y(NDIM),TLN(2,3),TOTV,BX,BY,BZ,B,
& X00,Y00,Z00,FAC,PASVEL(10000,2)
REAL*8 FPHI,DIST,X1,Y1,Z1
PARAMETER (FAC=0.02540005D0)
COMMON /NCOUNT/NCOUNT
COMMON /TLN/TLN,/NU/NU
COMMON /PASVEL/PASVEL
INCLUDE 'PASS5.CMN'
DATA MULC/40/,MULC1/10/
TOTV=DSQRT(Y(4)*Y(4) + Y(5)*Y(5) + Y(6)*Y(6))
NCOUNT = NCOUNT + 1
D B = DSQRT(BX*BX + BY*BY + BZ*BZ)
IF (NU .EQ. 1) THEN
DO I=1,3
TLN(2,I)=Y(I)/FAC
END DO
ELSE
DO I=1,3
TLN(1,I)=TLN(2,I)
TLN(2,I)=Y(I)/FAC
END DO
CALL CHECKHIT(HIT,NSURF)
!HIT=0 :CONTINUE WITH TRAJECTORY CALCULATION
! =1 :HIT THE NSURF(NTH SURFACE), LOST
! =2 :SUCCESSFULLY ESCAPED FROM THE SENSOR
IF (HIT .EQ. 2) THEN
NPAS=NPAS+1
C COMPUTE THE POLAR & THE AZIMUTHAL ANGLES OF THIS ESCAPING
C PARTICLE
X1=TLN(2,1)-TLN(1,1)
Y1=TLN(2,2)-TLN(1,2)
Z1=TLN(2,3)-TLN(1,3)
DIST=DSQRT(X1*X1 + Y1*Y1 + Z1*Z1)
PAS(NPAS,3)=DACOS(Z1/DIST)
PAS(NPAS,4)=FPHI(X1,Y1)
PASVEL(NPAS,1)=DACOS(Y(6)/TOTV)
PASVEL(NPAS,2)=FPHI(Y(4),Y(5))
DO I=1,6
PAS(NPAS,I+4)=Y(I)
END DO
END IF
END IF
NU=NU+1
15 FORMAT (1X,D14.7,6(1X,D15.8),1X,D21.14)
20 FORMAT(3(X,F13.6))
RETURN
END
C----------------------------------------------------------------------- C-----------------------------------------------------------------------
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LECP Data Analysis Handbook Table of Contents.
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Technologies Home Page.
Updated 8/9/19, Cameron Crane
VOYAGER 1 ELAPSED TIME
--:--:--:--
Days: Hours:
Minutes: Seconds
*Since official launch
September 5, 1977, 12:56:00:00 UTC
*Since official launch
September 5, 1977, 12:56:00:00 UTC
VOYAGER 2 ELAPSED TIME
--:--:--:--
Days: Hours:
Minutes: Seconds
*Since official launch
August 20, 1977, 14:29:00:00 UTC
*Since official launch
August 20, 1977, 14:29:00:00 UTC
QUICK FACTS
Manufacturer:
Voyagers 1 and 2 were built in the Jet Propulsion
Laboratory in Southern California.
Mission Duration: 40+ years have elapsed for both Voyager 1 and Voyager 2 (both are ongoing).
Destination: Their original destinations were Saturn and Jupiter. Their current destination is interstellar space.
Mission Duration: 40+ years have elapsed for both Voyager 1 and Voyager 2 (both are ongoing).
Destination: Their original destinations were Saturn and Jupiter. Their current destination is interstellar space.

