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. --------------------------------------------------------------------------
FormationFlying: EccDynamics/FFEccDH FormationFlying: EccDynamics/FFEccGoals FormationFlying: EccDynamics/FFEccProp FormationFlying: EccDynamics/FFEccRMat FormationFlying: EccDynamics/FFEccYExt EccDynamics: Derivatives/FFEccDDX EccDynamics: Derivatives/FFEccDDY EccDynamics: Derivatives/FFEccDX EccDynamics: Derivatives/FFEccDY FormationFlying: Visual/FFEccAnalyzeShape Math: Linear/Mag Math: Solvers/NewtRaph Math: Trigonometry/WrapPhase
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