Path: Orbit/Interplanetary
% Initialize a heliocentric orbit from a planet centered orbit. xP is in the ECI planet centered frame. Type HelioFromPlanetInit for a demo of an equatorial 7000 km circular earth orbit. This only works with the planets (including Pluto). Since version 2014.1 -------------------------------------------------------------------------- Forms: xH = HelioFromPlanetInit( planet, xP, jD ) -------------------------------------------------------------------------- ------ Inputs ------ name (1,1) Planet name xP (6,1) State in the planet centered ECI frame jD (1,1) Julian date ------- Outputs ------- xH (6,1) State in the heliocentric frame --------------------------------------------------------------------------
AC: ACData/ACTConstants SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: Ephem/CEcl2Eq SC: Ephem/Planets SC: Ephem/SolarSys 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/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TextS Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2T Math: Linear/DupVect
Back to the Orbit Module page