VOYAGER
Voyager LECP Data Analysis Handbook
Instrument Modeling Reports
by Sheela Shodhan
E.11 TRAJ2PT
**************************************************************************** * PROGRAM TRAJ1PHI * * PURPOSE : THIS IS THE MAIN PROGRAM IN A SET OF ROUTINES TO FOLLOW THE * * PARTICLE TRAJECTORIES INSIDE THE SENSOR SUBSYSTEM, IDENTIFY THE* * IMPACT ON SURFACES AND COUNT THOSE THAT ESCAPE THE SENSOR SUB * * -SYSTEM. * * ROUTINES TO BE LINKED : TRAJ2PT,CHECHITSEN1,FDMOD1,TIMER,TRACKSUB1, * * TRAJRT2BDET * * DESCRIPTION :(1)TRAJ2PT:THIS IS THE MAIN ROUTINE MAINLY USED TO PLOT THE * * PARTICLE TRAJECTORIES INSIDE THE SENSOR SUBSYSTEM. IT LOOPS * * OVER THE USER SPECIFIED POLAR ANGLE (THETA) AND THE AZIMUTHAL * * ANGLE (PHI). * * FOR DETAILED EXPLANATIONS, PLEASE SEE THE COMMENTS IN THE ROUTINES THEMSE* * -LVES. * * (2)CHECHITSEN1:THIS CONTAINS THE SET OF ROUTINES TO DETERMINE WHE* * -THER THE LINE-SEGMENT HAS HIT ANY OF THE POLYGON SURFACES OF * * THE SENSOR OR NOT. * * (3)FDMOD1:CALCULATES THE MAGNETIC FIELD AT THE GIVEN POINT IN SPA* * -CE. * * (4)TIMER:SHORT ROUTINE TO DETERMINE THE C.P.U. TIME REQUIRED TO * * RUN THIS PROGRAM. * * (5)TRACKSUB1:CONTAINS A SET OF ROUTINES TO PERFORM VARIOUS TASKS.* * (6)TRAJRT2BDET:CONTAINS THE DIFFERENTIAL EQUATION SOLVER DHPCG * * AND A SET OF ROUTINES THAT ARE NEEDED BY IT. * * VARIABLES : * * INPUT : * * X0,Y0,Z0 : INITIAL POSITION OF THE PARTICLE (* 10**2 INCHES). * * EK : INCIDENT ELECTRON ENERGY (MEV). * * NPHI,NTHETA : THE NUMBER OF PHIs AND THETAs TO BE SCANNED. * * PHIMIN : THE MINIMUM AZIMUTHAL ANGLE AT WHICH SCANNING STARTS(DEGREES). * * PRMT : 1-D ARRAY THAT IS TO BE PASSED TO THE ROUTINE DHPCG * * (1) INITIAL TIME, (2) FINAL TIME, (3)TIME STEP, (4) ERROR BOUND. * * (* 10**-8 SECONDS). * * STEPHI,STEPTHETA : INTERVALS AT WHICH AZIMUTHAL AND POLAR ANGLES ARE SCAN* * -NED RESPECTIVELY (DEGREES). * * THETAMIN : (DEGREES)MINIMUM POLAR ANGLE AT WHICH THETAs ARE SCANNED. * * OUTPUT: * * NPAS : NUMBER OF PARTICLES THAT PASS THE SENSOR SUBSYSTEM. * * *.E* : FILE THAT RECORDS THE ANGLES AT THE DETECTOR,AND ANGLES,POSITIONS * * AND VELOCITIES AT THE APERTURE, OF THE ESCAPING TRAJECTORIES. * * *.E*IN, *.E*OUT, *.E*OUTVEL : FILES OF ANGLES AT THE DETECTOR,APERTURE * * AND ANGLES COMPUTED FROM Vx,Vy and Vz AT THE APERTURE RESPECTIVELY. * * *.E*** : FILE FOR EACH PARTICLE CONTAINING ITS POSITION COORDINATES AT * * EVERY POINT IN THE TRAJECTORY. THIS FILE CAN BE USED TO PLOT THE * * TRAJECTORY OF THE PARTICLE INSIDE THE SENSOR SUBSYSTEM. * * OTHERS: * * NHIT : INDICATES WHETHER THE PARTICLE IS LOST OR NOT-THETAs ARE SCANNED * * UNITL THE PARTICLE ESCAPES FROM THE SENSOR SUBSYSTEM (NHIT=2). * * PAS : 1-D ARRAY, (1)-(4)POLAR & AZIMUTHAL ANGLES AT THE DETECTOR AND AT * * THE APERTURE,(5)-(10) x,y,z,Vx,Vy,Vz OF THE ESCAPING PARTICLE. * * QMC : q/mc CONSTANT (C.G.S. UNITS). * * QMCP : QMC * sqrt(1 - (v/c)^2) TO TAKE CARE OF THE RELATIVITIC MASS. * * PHI,THETA : INITIAL AZIMUTHAL AND POLAR ANGLE AT THE DETECTOR SURFACE. * * V : VELOCITY OF THE PARTICLE FOR GIVEN ENERGY EK. * * Y : 1-D ARRAY TO BE PASSSED TO THE ROUTINE DHPCG * * (1)-(3) POSITION COORDINATES, (4)-(6) VELOCITY COMPONENTS. * * PLEASE NOTE : (1)ROUTINES TRACKSUB1 AND TRACKSUB5 ARE BASICALLY THE SAME * * EXCEPT THAT THE SUBROUTINE 'PASSOUTPUT' IN TRACKSUB5 INCLUDES PASS5.CMN * * WHILST 'PASSOUTPUT' IN TRACKSUB1 INCLUDES PASS.CMN. BESIDES, 'PASSOUTPUT'* * IN TRACKSUB5 ALSO WRITES IN THE FILE *.E*OUTVEL, POLAR ANGLES AND AZIMUTH* * AL ANGLES AT THE APERTURE OF THE ESCAPING PARTICLE CALULATED FROM THE VEL* * -OCITY COMPONENTS Vx,Vy AND Vz OF THE PARTICLE. * * THE DIFFERENCE BETWEEN PASS5.CMN AND PASS.CMN IS THAT IN THE FORMER THE * * DIMENSION OF THE ARRAY 'PAS' IS MUCH LARGER. * * (2)DIFFERENCES BETWEEN TRAJRT2BDET AND TRAJRT2BDET5 ARE: * * AT EVERY FEW STEPS OF THE TRAJECTORY, FORMER WRITES THE POSITION COORDINA* * -TES IN THE FILE *.E***, SO THAT THE TRAJECTORY CAN BE PLOTTED. * * FORMER INCLUDES DIFFERENTIAL EQUATION SOLVER DHPCG WHILE THE LATTER DOES * * NOT. FORMER WRITES THE POSITION AND VELOCITY COMPONENTS AT EVERY FEW STEP* * -S IN A FILE 'TRAJSH.DAT' WHILE THE LATTER DOES NOT. LATTER ALSO COMPUTES* * THE OUTGOING ANGLES FROM THE VELOCITY COMPONENTS OF THE PARTICLE AS IT * * ESCAPES THE APERTURE, THE FORMER DOES NOT. TRAJRT2BDET INCLUDES FILE * * 'PASS.CMN' WHILE TRAJRT2BDET5 INCLUDES FILE 'PASS5.CMN'. * * (3) THUS, TRAJ2PT IS MAINLY SUITED FOR PLOTTING THE TRAJECTORIES OF THE * * PARTICLES AND FOR SHORT SCANS OVER THE ANGLES WHILST TRAJ6PT IS FOR LONG * * SCANS, TO COUNT THE NUMBER OF PARTICLES THAT PASS IN ORDER TO COMPUTE THE* * GEOMETRIC FACTOR FOR VARIOUS ENERGIES. * ****************************************************************************
PROGRAM TRAJ1PHI
IMPLICIT NONE
CHARACTER*72 FNAME,FNAME1,FNAME2,FNAME3
INTEGER I,I1,IHLF,J,MAXE,NCOUNT,NDIM,NHIT,NPHI,NTHETA,NU
INTEGER NXK,NYK,NZK
PARAMETER (MAXE=100)
REAL*8 C,CON,ERRWT
PARAMETER (CON=2.540005D0,NDIM=6)
REAL*8 STEPHI,STEPTHETA,EK,ENEK,PHIMIN,EVELO,PHI(MAXE),
& QMC,QMCP,
& THETA(MAXE),THETAMIN,V,VX,VY,VZ
REAL*8 AUX(16,NDIM),DERY(NDIM),PRMT(5),X0,Y(NDIM),Y0,Z0
REAL CPUTIME,TIMER,ZTIM0
INCLUDE 'PASS.CMN'
COMMON /QMC/QMC
COMMON /NCOUNT/NCOUNT,/NU/NU,/FNAME/FNAME,/NHIT/NHIT
COMMON /FNAME1/FNAME1
COMMON /FNAME2/FNAME2,FNAME3
DATA C/2.998D0/,QMCP/0.175602D0/
EXTERNAL FCT,OUTP
ZTIM0=TIMER()
CALL GEOM
OPEN(UNIT=7,FILE='TRAJSH.DAT',ACCESS='SEQUENTIAL',STATUS='NEW')
WRITE(6,*) 'ENTER THE INITIAL COORDINATES OF THE e IN INCHES'
READ(5,*) X0,Y0,Z0
C TO ENTER QUANTITIES FOR PRMT
WRITE(6,*) 'ENTER LOWER BOUND ON TIME (t=0)'
READ(5,*) PRMT(1)
WRITE(6,*) 'ENTER THE UPPER BOUND ON TIME'
READ(5,*) PRMT(2)
WRITE(6,*) 'ENTER THE TIME STEP'
READ(5,*) PRMT(3)
WRITE(6,*) 'ENTER THE ERROR BOUND'
READ(5,*) PRMT(4)
WRITE(6,*) 'ENTER THE ENERGY OF THE PARTICLE IN MEV'
READ(5,*) EK
ENEK=IDINT(1000.0D0*EK)
NXK=IDINT(-100000.0D0*X0)
NYK=IDINT(-100000.0D0*Y0)
NZK=IDINT(100000.0D0*Z0)
ENCODE (17,60,FNAME1)NXK,NYK,NZK,IDINT(ENEK)
OPEN(UNIT=8,STATUS='NEW',ACCESS='SEQUENTIAL',FILE=FNAME1)
ENCODE (19,110,FNAME2)NXK,NYK,NZK,IDINT(ENEK)
OPEN(UNIT=1,STATUS='NEW',ACCESS='SEQUENTIAL',FILE=FNAME2)
ENCODE (20,120,FNAME3)NXK,NYK,NZK,IDINT(ENEK)
OPEN(UNIT=2,STATUS='NEW',ACCESS='SEQUENTIAL',FILE=FNAME3)
V = EVELO(EK) !COMPUTE V FOR THIS ENERGY OF e
QMC = -QMCP*DSQRT(1 - (V/C)**2)
WRITE (6,*) 'ENTER MIN. THETA,NO. OF STEPS,DEL THETA'
READ (5,*) THETAMIN,NTHETA,STEPTHETA
WRITE (6,*) 'ENTER MIN. PHI,NO. OF STEPS,DEL PHI'
READ (5,*) PHIMIN,NPHI,STEPHI
WRITE (8,70) EK,V
WRITE (8,80) THETAMIN,NTHETA,STEPTHETA
WRITE (8,90) PHIMIN,NPHI,STEPHI
WRITE (8,20) PRMT(1),PRMT(2),PRMT(3),PRMT(4)
WRITE (8,*)
WRITE (8,95) X0,Y0,Z0
WRITE (1,130)
WRITE (2,140)
C TO CONVERT FROM INCHES TO CMS.
X0 = X0 * CON
Y0 = Y0 * CON
Z0 = Z0 * CON
WRITE (8,100) X0,Y0,Z0
WRITE (8,*)
DO I=1,NTHETA
THETA(I)=THETAMIN + DFLOAT(I-1)*STEPTHETA
END DO
DO I=1,NPHI
PHI(I)=PHIMIN + DFLOAT(I-1)*STEPHI
END DO
NPAS=0
DO J=1,NTHETA
DO I=1,NPHI
ENCODE (23,50,FNAME)NXK,NYK,NZK,IDINT(ENEK),
& IDINT(THETA(J)),IDINT(PHI(I))
OPEN(UNIT=4,STATUS='NEW',ACCESS='SEQUENTIAL',FILE=FNAME)
NCOUNT = 0
NU = 1
WRITE(7,05) I
WRITE(7,10) EK,V,THETA(J),PHI(I)
WRITE(7,20) PRMT(1),PRMT(2),PRMT(3),PRMT(4)
WRITE(7,30)
WRITE(4,05) I
C TO COMPUTE THE VELOCITY PROJECTIONS Vx,Vy,Vz
CALL VELOPROJ(V,VX,VY,VZ,THETA(J),PHI(I))
WRITE(6,*) ' THETA( ',J,')',THETA(J),' PHI( ',I,')',PHI(I)
C TO INITIALISE THE INITIAL VALUES
Y(1) = X0
Y(2) = Y0
Y(3) = Z0
Y(4) = VX
Y(5) = VY
Y(6) = VZ
ERRWT = 1.0D0/6.0D0
DO I1=1,NDIM
DERY(I1) = ERRWT
END DO
CALL DHPCG(PRMT,Y,DERY,NDIM,IHLF,FCT,OUTP,AUX)
IF (NHIT .EQ. 2) THEN
PAS(NPAS,1) = THETA(J)
PAS(NPAS,2) = PHI(I)
END IF
WRITE(7,40)
WRITE(4,40)
WRITE(6,*)
WRITE(6,*) ' IHLF NO. OF BISECTIONS OF STEP: ',IHLF
WRITE(6,*) 'TOTAL NO. OF POINTS IN THE TRAJECTORY: ',NU-1
END DO
END DO
CALL PASSOUTPUT
WRITE(6,*) 'NPAS:',NPAS
CPUTIME=TIMER()-ZTIM0
WRITE(6,*) 'C.P.U. TIME: ',CPUTIME
WRITE(1,40)
WRITE(2,40)
05 FORMAT(1X,I3)
10 FORMAT(1X,'ENERGY(in mev)',D10.3,2X,'VELOCITY(*10+10)',F12.5,2X,
& 'THETA(in deg.)',F10.3,2X,'PHI(in deg.)',F10.3)
20 FORMAT(1X,'INITIAL TIME(*10-08)',F12.6,2X,'FINAL TIME(*10-08)',
& F12.6,2X,'INITIAL STEP(*10-08)',F14.8,1X,'ERROR BOUND',F19.12)
30 FORMAT(4X,'T(-08)',10X,'X(+02)',10X,'Y(+02)',10X,'Z(+02)',10X,
& 'VX(+10)',10X,'VY(+10)',10X,'VZ(+10)',10X,'(V+10)')
40 FORMAT(X,'---*---*---*--- END OF ENERGY ---*---*---*---')
50 FORMAT (I3,I3,I4,'.E',I5,I3,I3)
60 FORMAT (I3,I3,I4,'.E',I5)
70 FORMAT (1X,'ENERGY(in mev)',D10.3,2X,'VELOCITY(*10+10)',F12.5)
80 FORMAT (1X,'INITIAL THETA(in deg.)',F10.2,2X,'NO. OF STEPS',
& I5,2X,'DEL THETA',F10.2)
90 FORMAT (1X,'INITIAL PHI (in deg.)',F10.2,2X,'NO. OF STEPS',
& I5,2X,'DEL PHI ',F10.2)
95 FORMAT (1X,'STARTING POSITION(in in.)',2X,'X(+02)',D14.7,
& 2X,'Y(+02)',D14.7,2X,'Z(+02)',D14.7)
100 FORMAT (1X,'STARTING POSITION(in cm.)',2X,'X(+02)',D14.7,
& 2X,'Y(+02)',D14.7,2X,'Z(+02)',D14.7)
110 FORMAT (I3,I3,I4,'.E',I5,'IN')
120 FORMAT (I3,I3,I4,'.E',I5,'OUT')
130 FORMAT(1X,'POLAR & AZIMUTHAL ANGLES AT THE DETECTOR')
140 FORMAT(1X,'POLAR & AZIMUTHAL ANGLES AT THE APERTURE')
CLOSE(1)
CLOSE(2)
CLOSE(7)
CLOSE(4)
CLOSE(8)
STOP
END
C-----------------------------------------------------------------------------
C-----------------------------------------------------------------------------
Return to thesis table of contents.
Return to Voyager
LECP Data Analysis Handbook Table of Contents.
Return to Fundamental
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.