Path: Orbit/Interplanetary
% Computes planet heliocentric states for a range of dates.
The data structure is from Planets.
Since version 2014.1
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Form:
x = SolarSysState( d, jD )
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Inputs
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d (.) Data structure
.iv (n,2) Inclination wrt ecliptic plane (rad)
.Wv (n,2) Longitude of ascending node wrt vernal equinox (rad)
.wv (n,2) Argument of perhelion (rad)
.av (n,2) Mean distance (au)
.ev (n,2) Eccentricity
.Lv (n,3) Mean longitude (rad)
.name (n,:) Name of planet
.jdref (1,1) Reference Julian date
.T (1,:) Julian centuries from J2000.0 (centuries)
jD (1,:) Julian date
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Outputs
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x (6,:,:) [state,date,planet]
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SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: Ephem/Planets SC: Ephem/SolarSys Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT 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
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