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.16 *
******************************************************************************* * FACTOR * * THIS IS THE PROGRAM THAT READS THE INPUT ANGLES OF THE ESCAPING * * TRAJECTORIES AND COMPUTES G FOR A GIVEN ENERGY. IT HAS TO LOOP THROUGH * * ALL DETECTOR AREA ELEMENTS, AS WELL AS EACH ESCAPING TRAJECTORY. NOTE * * THAT FOR MY SITUATION, I USED DELPHI = 2 DEGREES, AND DELTHETA = 2 DEGREES. * * NOTE ALSO THAT I RENAMED THE *.E*IN FILES 1.DAT, 2.DAT,...ETC. * *******************************************************************************
program factor
real*8 G,theta,omega real*8 area(13) integer int,n,npas,j character*2 fname parameter (delth = .0349066,delphi = .0349066)
G = 0. do n=1,13 int = n write (fname,'(i2)') int write (6,*) fname open (unit=1,status='old',access='sequential',file=fname) read (1,*) area(n) write (6,*) area(n) read (1,*) npas write (6,*) npas omega = 0. do j=1,npas read (1,*) theta c write (6,*) theta theta = theta*.0174533 omega = omega + delth*delphi*sin(theta + delth/2) c write (6,*) 'omega',omega end do if (n.lt.6) then G = G + area(n)*omega else G = G + 2*area(n)*omega end if close (1) end do write (6,*) 'G=',G 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