ULYSSES
Ulysses HISCALE Data Analysis Handbook
Appendix 9 Geometric Factor Study for the Deflected and Unscattered Electrons of HISCALE (Buckley MS Thesis)
A9.13 Appendix: Computer Programs
* PROGRAM I.11 *
****************************************************************************** * TRAJ2PT * * THIS IS THE MODIFICATION TO THE MAIN PROGRAM NEEDED TO DO TRAJECTORY PLOTS.* * PRIMARY DIFFERENCES BETWEEN THIS AND TRAJ6PT ARE EXPLAINED ON PAGE 108 OF * * SHODHAN'S THESIS. * ******************************************************************************
PROGRAM TRAJ1PHI
IMPLICIT NONE CHARACTER*72 FNAME,FNAME1,FNAME2,FNAME3 INTEGER I,I1,IHLF,J,MAXE,NCOUNT,NDIM,NHIT,NPAS,NPHI,NU,NTHETA INTEGER NXK,NYK,NZK,NTRAJ PARAMETER (MAXE=100) REAL*8 C,CON,ERRWT,QMCP REAL*8 STEPHI,STEPTHETA,EK,ENEK,PHIMIN,PHIMAX,EVELO,PHI(MAXE),QMC,QMCP, & V,VX,VY,VZ,THETA(MAXE),THETAMIN
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/ PARAMETER (CON=2.540005D0,NDIM=6) REAL*8 AUX(16,NDIM),DERY(NDIM),PRMT(5),X0,Y(NDIM),Y0,Z0 REAL CPUTIME,TIMER,ZTIM0
EXTERNAL FCT,OUTP ZTIM0=TIMER()
CALL GEOM
C OPEN(UNIT=3,FILE='TRAJ.DAT',ACCESS='SEQUENTIAL',STATUS='NEW') C OPEN(UNIT=4,FILE='TRAJCO.DAT',ACCESS='SEQUENTIAL',STATUS='NEW') OPEN(UNIT=7,FILE='TRAJSH.DAT',ACCESS='SEQUENTIAL',STATUS='NEW') C OPEN(UNIT=8,FILE='PASS.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(10000.0D0*abs(X0)) NYK=IDINT(10000.0D0*abs(Y0)) NZK=IDINT(10000.0D0*abs(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)
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 + (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,*) WRITE(4,05) (I+49) WRITE(4,*)
C TO COMPUTE THE VELOCITY PROJECTIONS Vx,Vy,Vz CALL VELOPROJ(V,VX,VY,VZ,THETA(J),PHI(I))
C WRITE(6,*) ' X: ',X0,' Y: ',Y0,' Z: ',Z0 C WRITE(6,*) 'ENERGY (in mev) ',EK,' V ',V,' QMC ',QMC WRITE(6,*) ' THETA( ',J,')',THETA(J),' PHI( ',I,')',PHI(I) C WRITE(6,*) ' VX ',VX,' VY ',VY,' VZ ',VZ
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) C WRITE(3,40) WRITE(4,40) WRITE(6,*) C WRITE(6,*) ' Y ',(Y(I1),I1=1,NDIM) 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',F10.2,2X,'NO. OF STEPS', & I5,2X,'DEL THETA',F10.2) 90 FORMAT (1X,'INITIAL PHI',F10.2,2X,'NO. OF STEPS', & I5,2X,'DEL PHI',F10.2) 95 FORMAT (1X,'STARTING POSITION(INCHES)',2X,'X(+02)',D14.7, & 2X,'Y(+02)',D14.7,2X,'Z(+02)',D14.7) 100 FORMAT (1X,'STARTING POSITION(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 & AZIM ANGLES AT DETECTOR') 140 FORMAT (1X,'POLAR & AZIM ANGLES AT THE APERATURE')
CLOSE(1) CLOSE(2) CLOSE(7) CLOSE(4) CLOSE(8) STOP END
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Updated 8/8/19, Cameron Crane
QUICK FACTS
Manufacturer:
ESA provided the Ulysses spacecraft, NASA provided the power
supply, and various others provided its instruments.
Mission End Date: June 30, 2009
Destination: The inner heliosphere of the sun away from the ecliptic plane
Orbit: Elliptical orbit transversing the polar regions of the sun outside of the ecliptic plane
Mission End Date: June 30, 2009
Destination: The inner heliosphere of the sun away from the ecliptic plane
Orbit: Elliptical orbit transversing the polar regions of the sun outside of the ecliptic plane