TransECIToHills:

% Two orbits are initialized with a small inclination difference. The orbits
   are propagated with Kepler's equations using RVOrbGen. The ECI position 
   and velocity of each orbit is then transformed into the relative Hills frame.

   Since version 7.
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  See also Constant, Plot2D, ECI2Hills, RVOrbGen
  ------------------------------------------------------------------------
%
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   Copyright (c) 2002 Princeton Satellite Systems, Inc. All rights reserved.
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Children:

Common: Database/Constant
Common: Graphics/Plot2D
FormationFlying: Transformation/ECI2Hills
Orbit: OrbitMechanics/RVOrbGen