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Path: SCPro/DynamicalModels
% Analytical eigenvalues for gravity gradient stabilization. r is along -z. This is only valid for a circular orbit. -------------------------------------------------------------------------- Form: [e, a] = GravityGradientAnalytical( n, iXX, iYY, iZZ ) -------------------------------------------------------------------------- ------ Inputs ------ n (1,1) Orbit rate iXX (1,1) Ixx inertia term iYY (1,1) Iyy inertia term iZZ (1,1) Izz inertia term ------- Outputs ------- e (6,1) Eigenvalues a (6,6) State matrix --------------------------------------------------------------------------
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