Path: FormationFlying/EccDynamics
% Compute extreme x-values and associated true anomalies for given relative motion. Since version 7. -------------------------------------------------------------------------- Form: [x,nu] = FFEccXExt( e, D, dH, epsilon, nMax ); -------------------------------------------------------------------------- ------ Inputs ------ e (1) Eccentricity D (6,1) Integration constants computed from i.c.'s dH (1) Integration constant found by setting H = 0 at nu0 epsilon (1) Angular tolerance [rad] nMax (1) Maximum number of iterations ------- Outputs ------- x (1,#) Extreme values of radial oscillation [km] nu (1,#) True anomaly where extreme values occur [rad] -------------------------------------------------------------------------- Copyright 2004 Princeton Satellite Systems, Inc. All rights reserved. --------------------------------------------------------------------------