Path: Orbit/OrbitCoord
% Computes the orbit radius and the parameter from Keplerian elements.
Since version 1.
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Form:
[r, p] = REl( el )
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Inputs
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el Elements vector [a,i,W,w,e,M] where a is perigee
radius for a parabola
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Outputs
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r Radius
p Parameter
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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 Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/DupVect
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