Path: FormationFlying/Transformation
% Compute geometric goals given Frenet frame state and orbit info
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Form:
[g,D] = FFEccFrenet2Goals( e, nu, xF, n );
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Inputs
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e (1,1) Eccentricity
nu (1,1) True anomaly [rad]
xF (6,1) Frenet frame state at nu (time-domain)
n (1,1) Mean orbit rate [rad/s] (optional)
* uses time-derivatives if provided
* uses nu-derivatives if NOT provided
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Outputs
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g (.) Data structure of geometric goals
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Copyright (c) 2007 Princeton Satellite Systems, Inc.
All rights reserved.
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Since version 7.
2019.1 Fixed bug in second path
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FormationFlying: EccDynamics/FFEccDH FormationFlying: EccDynamics/FFEccGoals FormationFlying: EccDynamics/FFEccProp FormationFlying: EccDynamics/FFEccRMat FormationFlying: EccDynamics/FFEccXExt FormationFlying: EccDynamics/FFEccYExt FormationFlying: EccDynamics/FFEccZExt EccDynamics: Derivatives/FFEccDDX EccDynamics: Derivatives/FFEccDDY EccDynamics: Derivatives/FFEccDDZ EccDynamics: Derivatives/FFEccDX EccDynamics: Derivatives/FFEccDY EccDynamics: Derivatives/FFEccDZ FormationFlying: Transformation/FFEccHills2Goals FormationFlying: Transformation/Frenet2Hills FormationFlying: Utility/NuDot FormationFlying: Utility/Time2NuDomain FormationFlying: Visual/FFEccAnalyzeShape Common: Transform/RotMat Math: Linear/Cross Math: Linear/DupVect Math: Linear/Mag Math: Solvers/NewtRaph Math: Trigonometry/WrapPhase
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