Path: FormationFlying/Eccentric
% Demonstrate how relative motion changes when the same relative state is initialized at different true anomalies. Since version 7. ------------------------------------------------------------------------- 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.% ------------------------------------------------------------------------- See also FFEccLawdensEqns ------------------------------------------------------------------------- % -------------------------------------------------------------------------- Copyright 2004 Princeton Satellite Systems, Inc. All rights reserved. --------------------------------------------------------------------------
FormationFlying: EccDynamics/FFEccIntConst FormationFlying: EccDynamics/FFEccLawdensEqns FormationFlying: EccDynamics/FFEccRMat FormationFlying: Utility/Nu2TimeDomain FormationFlying: Utility/NuDot FormationFlying: Utility/Time2NuDomain Common: Graphics/NewFig
Back to the FormationFlying Module page