Path: Orbit/OrbitCoord
% Converts tangential accelerations into radial using equinoctial elements.
Since version 1.
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Form:
aR = CT2REq( eq, aT, mu )
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Inputs
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eq Equinoctial elements
aT Tangential vector
mu Gravitational parameter
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Outputs
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aR Radial vector or transformation matrix
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References: Battin, R.H., An Introduction to the Methods and Mathematics
of Astrodynamics, AIAA, New York, 1987, pp. 490.
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Orbit: OrbitCoord/K2L Orbit: OrbitCoord/ML2K Orbit: OrbitCoord/ML2KApp Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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