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.1 *
****************************************************************************** * TRAJ6PT * * THIS IS THE MAIN TRAJECTORY PROGRAM. ALL VARIABLES AND PARAMETERS ARE * * DEFINED IN THE COMMENTS FOUND ON PAGE 65 OF SHODHAN'S THESIS. * ******************************************************************************
PROGRAM TRAJ1PHI IMPLICIT NONE CHARACTER*72 FNAME,FNAME1,FNAME2,FNAME3,FNAME4 INTEGER I,I1,IHLF,J,MAXE,NCOUNT,NDIM,NHIT,NPHI,NTHETA,NU INTEGER NXK,NYK,NZK,MAXSURF PARAMETER (MAXE=100) REAL*8 C,CON,ERRWT PARAMETER (CON=2.540005D0,NDIM=6) REAL*8 STEPHI,STEPTHETA,EK,ENEK,PHIMIN,EVELO, & PHI,QMC,QMCP, & THETA,THETAMAX,THETAMID,V,VX,VY,VZ REAL*8 AUX(16,NDIM),DERY(NDIM),PRMT(5),X0,Y(NDIM),Y0,Z0 REAL CPUTIME,TIMER,ZTIM0
INCLUDE 'PASS5.CMN' COMMON /QMC/QMC COMMON /NCOUNT/NCOUNT,/NU/NU,/NHIT/NHIT C COMMON /FNAME/FNAME COMMON /FNAME4/FNAME4 COMMON /FNAME1/FNAME1 COMMON /FNAME2/FNAME2,FNAME3 DATA C/2.998D0/,QMCP/0.175602D0/ EXTERNAL FCT,OUTP ZTIM0=TIMER() CALL GEOM
C 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(-10000.0D0*X0) NYK=IDINT(-10000.0D0*Y0) NZK=IDINT(10000.0D0*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)
ENCODE (23,125,FNAME4)NXK,NYK,NZK,IDINT(ENEK) OPEN(UNIT=3,STATUS='NEW',ACCESS='SEQUENTIAL',FILE=FNAME4)
V = EVELO(EK) !COMPUTE V FOR THIS ENERGY OF e QMC = -QMCP*DSQRT(1 - (V/C)**2)
WRITE (6,*) 'ENTER MID. THETA,THETAMAX,DEL THETA' READ (5,*) THETAMID,THETAMAX,STEPTHETA
WRITE (6,*) 'ENTER MIN. PHI,NO. OF STEPS,DEL PHI' READ (5,*) PHIMIN,NPHI,STEPHI
WRITE (8,70) EK,V WRITE (8,80) THETAMID,THETAMAX,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 (1,*) (1) WRITE (2,140) WRITE (2,*) (1) WRITE (3,150)
C TO CONVERT FROM INCHES TO CMS. X0 = X0 * CON Y0 = Y0 * CON Z0 = Z0 * CON
WRITE (8,100) X0,Y0,Z0 WRITE (8,*)
NPAS=0
DO I=1,NPHI
PHI=PHIMIN + DFLOAT(I-1)*STEPHI
DO J=-1,1,2 IF (J .EQ. -1) THEN THETA=THETAMID ELSE THETA=THETAMID + DFLOAT(J)*STEPTHETA END IF NHIT=2 DO WHILE (NHIT .EQ. 2 .AND. THETA .LT. THETAMAX)
C ENCODE (23,50,FNAME)NXK,NYK,NZK,IDINT(ENEK), C & IDINT(THETA),IDINT(PHI) C OPEN(UNIT=4,STATUS='NEW',ACCESS='SEQUENTIAL',FILE=FNAME)
NCOUNT = 0 NU = 1
C WRITE(7,05) I C WRITE(7,10) EK,V,THETA(J),PHI(I) C WRITE(7,20) PRMT(1),PRMT(2),PRMT(3),PRMT(4) C WRITE(7,30) C WRITE(6,*) J
C TO COMPUTE THE VELOCITY PROJECTIONS Vx,Vy,Vz CALL VELOPROJ(V,VX,VY,VZ,THETA,PHI)
WRITE(6,*) ' THETA ',THETA,' PHI ',PHI
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 PAS(NPAS,2) = PHI END IF
WRITE(6,*) WRITE(6,*) ' IHLF NO. OF BISECTIONS OF STEP: ',IHLF WRITE(6,*) 'TOTAL NO. OF POINTS IN THE TRAJECTORY: ',NU-1
IF ((THETA.LT.140).AND.(THETA.GT.40)) NHIT = 2 THETA = THETA+DFLOAT(J)*STEPTHETA
END DO 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,'MIDDLE THETA(in deg.)',F10.2,2X,'MAX.THETA', & F10.2,2X,'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') 125 FORMAT (I3,I3,I4,'.E',I5,'OUTVEL') 130 FORMAT(1X,'POLAR & AZIMUTHAL ANGLES AT THE DETECTOR') 140 FORMAT(1X,'POLAR & AZIMUTHAL ANGLES AT THE APERTURE') 150 FORMAT(1X,'POLAR & AZIMUTHAL ANGLES AT THE APERTURE FROM VEL.') CLOSE(1) CLOSE(2) CLOSE(3) END
C----------------------------------------------------------------------------- C-----------------------------------------------------------------------------
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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