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Path: Orbit/OrbitMechanics
% Right-hand-side of the cylindrical orbit equations about a mass point. See also SphOrb and FOrb. Since version 1. -------------------------------------------------------------------------- Form: xDot = CylOrb( x, a, mu ) -------------------------------------------------------------------------- ------ Inputs ------ x (6,1) state [r;theta;z;dr/dt;dtheta/dt;dz/dt] a (3,1) acceleration vector mu gravitational parameter ------- Outputs ------- xDot (6,1) state derivative --------------------------------------------------------------------------
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