Path: SpacecraftEstimation/StellarEphem
% Adjust the vector u for aberration.
Since version 3.
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Form:
uC = StellAbr( u, v, abType )
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Inputs
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u (3,1) Unit position vector
v (3,1) Velocity vector divided by the speed of
light
abType (1,1) Type of computation 'n' (Newtonian) or 's'
(special-relativistic)
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Outputs
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uC Corrected u
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References: Siedelmann, P., ed. (1992). Explanatory Supplement to the
Astronomical Almanac, University Science Books,
Mill Valley, CA, 129.
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