Path: Orbit/OrbitCoord
% Converts tangential accelerations into radial using the elements vector.
Since version 1.
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Form:
ar = CT2REl( el, at, mu )
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Inputs
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el Keplerian Elements [a,i,W,w,e,M]
at Tangential vector [tangent;normal;out-of-plane]
mu Gravitational parameter
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Outputs
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ar Radial vector or transformation matrix
[radial;circumferential;out-of-plane]
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References: Battin, R.H., An Introduction to the Methods and Mathematics
of Astrodynamics, AIAA, New York, 1987, pp. 489.
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Orbit: OrbitCoord/SLR 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/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Math: Linear/DupVect
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