Path: Orbit/Interplanetary
% Computes the heliocentric orbital elements after an Earth escape spiral.
Performs a simulation of the spiral out from Earth using ode113 and
FCRTBPRHS, and stops once the sun gravity acceleration dominates that
of Earth.
Since version 2014.1
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Form:
[elHelio, rSEMI, vSEMI, t1, mass] = EarthOrbToHelioOrb( jD0, elEarth, SCParams)
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Inputs
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jD0 (1,:) Julian Date
elEarth (1,6) Initial orbital elements in the ECI frame
SCParams (.) Design parameters for the spacecraft
.mass0 Mass (kg)
.thrust Thrust (kN)
.Isp Specific impulse (sec)
.uE Exhaust velocity (km/s)
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Outputs
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elHelio (:,6) Orbital elements in the heliocentric frame
rSEMI (3,:) Position vector in the heliocentric frame
vSEMI (3,:) Velocity vector in the heliocentric frame
t1 (1,:) Time vector
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See also SunEarthMoonSystemConstants, TransformECIToSEMR,
CRTBPRHS, FCRTBPRHS, LowThrustCRTBP_StopFcn, SEMRToSEMI
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AC: ACData/ACTConstants Orbit: OrbitCoord/SEMIToSEMR Orbit: OrbitCoord/SEMRToSEMI Orbit: OrbitCoord/TransformECIToSEMR Orbit: OrbitData/SunEarthMoonSystemConstants Orbit: ThreeBody/CRTBPRHS Orbit: ThreeBody/FCRTBPRHS Orbit: ThreeBody/LowThrustCRTBP_StopFcn SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/El2RV SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/RV2El SC: BasicOrbit/RVFromKepler SC: Ephem/CEcl2Eq 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/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/Plot3D 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/Cross Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit
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