GroundStation:

Path: SpacecraftEstimation/OrbitEstimation

% Generate the ECI coordinates of an Earth-fixed position at a given time

   Type GroundStation for a demo.

   Since version 8.
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   Usage:
     [r, v] = GroundStation( t, omega, rEF );
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   ------
   Inputs
   ------
   t          (1)   Mean sidereal time (sec) 
   omega      (1)   Planet angular rate (rad/s)
   rEF       (3,1)  Earth-fixed position (km)

   -------
   Outputs
   -------
   r         (3,1)  Earth-Centered Inertial position (km)
   v         (3,1)  Earth-Centered Inertial velocity (km/s)

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Children:

Math: Linear/Cross

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