FFEccInitDemo:

Path: FormationFlying/Eccentric

% Demonstrate how relative motion changes when the same relative state is initialized at different true anomalies.

   Since version 7.
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 References: Inalhan, Tillerson, How, "Relative Dynamics and Control of
 Spacecraft Formations in Eccentric Orbits", Journal of Guidance,
 Control & Dynamics, Vol.25, No.1, Jan-Feb 2002.%
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  See also FFEccLawdensEqns
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%
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	Copyright 2004 Princeton Satellite Systems, Inc.
   All rights reserved.
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Children:

FormationFlying: EccDynamics/FFEccIntConst
FormationFlying: EccDynamics/FFEccLawdensEqns
FormationFlying: EccDynamics/FFEccRMat
FormationFlying: Utility/Nu2TimeDomain
FormationFlying: Utility/NuDot
FormationFlying: Utility/Time2NuDomain
Common: Graphics/NewFig

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