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.20 *
******************************************************************************* * FDLNCOOR43 * * THIS PROGRAM PLOTS THE RESULTS OF *.E*IN AND *.E*OUT FOUR TO A PAGE. * *******************************************************************************
PROGRAM FDLNCOOR43
PARAMETER (NB=50,NN=1500) REAL XYZ(6),X(NB,NN),Y(NB,NN) INTEGER NC,NPT(NB),NP CHARACTER*72 FNAME,TITLE,XLAB,YLAB
WRITE(6,*) 'ENTER NP:,NOS.OR PLOTS ON A PAGE' READ (5,*) NP
WRITE(6,*) 'ENTER THE TITLE' WRITE(6,'(A,$)') ' --> ' READ(5,'(A)') TITLE
DO NC=1,NP
WRITE(6,5) NC READ(5,10) FNAME C WRITE(6,*) 'ENTER INTEGERS FOR HORIZONTOL AND VERTICAL AXES:' C WRITE(6,12) C READ (5,*) Ho,Vo Ho = 1 Vo = 2 OPEN (UNIT=1,STATUS='OLD',FILE=FNAME) READ (1,*) 2 NPOINT = 0 READ(1,*,END=70) NLN WRITE(6,*) NLN 3 READ(1,19,ERR=2) (XYZ(M),M=1,2) D WRITE (6,*) XYZ(1),XYZ(2) NPOINT = NPOINT+1 X(NLN,NPOINT) = (XYZ(Ho)) Y(NLN,NPOINT) = (XYZ(Vo)) D WRITE(6,*) X(NLN,NPOINT),Y(NLN,NPOINT)
NPT(NLN) = NPOINT GO TO 3 70 CLOSE(1) PRINT *,'NLN: ',NLN D DO I = 1,NLN D WRITE(6,*) NPT(I) D END DO C WRITE(6,*) 'ENTER THE X-LABEL' C WRITE(6,'(A,$)') '--> ' C READ (5,'(A)') XLAB XLAB = 'THETA' C WRITE(6,*) 'ENTER THE Y-LABEL' C WRITE(6,'(A,$)') '--> ' C READ (5,'(A)') YLAB YLAB = 'PHI' C WRITE(6,*) 'ENTER LNPT,LNK' C READ(5,*) LNPT,LNK LNPT = 1 LNK = 4 WRITE(6,*) NLN WRITE(6,*) NLN WRITE(6,*) NLN WRITE(6,*) NLN D DO J = 1,NLN D WRITE(6,*) X(NLN,J),Y(NLN,J) D END DO
CALL PLOTR4(NC,X,Y,NPT,NLN,TITLE,XLAB,YLAB,LNPT,LNK) END DO C-----------------------------------------------------------
CALL FLUSH
5 FORMAT(X,'ENTER THE NAME OF THE FILE: ',I3) 10 FORMAT(A72) 12 FORMAT(X,'X---1',/, ' Y---2',/,' Z---3') c 19 FORMAT(3(X,f9.6)) 19 FORMAT(2(X,F9.3)) 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