StellAbr:

Path: SpacecraftEstimation/StellarEphem

% Adjust the vector u for aberration.

   Since version 3.
------------------------------------------------------------------------
   Form:
   uC = StellAbr( u, v, abType )
------------------------------------------------------------------------

   ------
   Inputs
   ------
   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) 
   

   -------
   Outputs
   -------
   uC                       Corrected u

------------------------------------------------------------------------
   References: Siedelmann, P., ed. (1992). Explanatory Supplement to the
               Astronomical Almanac, University Science Books,
               Mill Valley, CA, 129. 
------------------------------------------------------------------------

Back to the SpacecraftEstimation Module page