Path: SC/Visualization
% Plot planets and a trajectory in the heliocentric frame.
It uses PlanetPosJPL for the planetary ephemerides. Can handle
any number of spacecraft [r1;r2;r3...]
--------------------------------------------------------------------------
Form:
HelioPlot( p, duration, jD0, r, rName )
--------------------------------------------------------------------------
------
Inputs
------
p (1,:) Planets 1-9
duration (1,1) Duration of the study (years)
jD0 (1,1) Julian date to start computation or date array
r (3*m,:) Spacecraft trajectory [r1;r2;r3...] (km)
rName {m} Names objects in r
-------
Outputs
-------
None.
--------------------------------------------------------------------------
AC: ACData/ACTConstants Orbit: OrbitCoord/SLR Orbit: OrbitMechanics/RVOrbGen SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: Ephem/CEcl2Eq SC: Ephem/InterpolateState SC: Ephem/PlanetPosJPL SC: SCData/bin2000 SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeBlankLT Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Math: Linear/DupVect
Back to the SC Module page