Path: Orbit/RHSOrbit
% Computes the right-hand-side of the orbit equations about a mass point with options for cartesian, spherical, or cylindrical coordinates. Since version 1. -------------------------------------------------------------------------- Form: xDot = FOrb( x, t, fType, a, mu ) -------------------------------------------------------------------------- ------ Inputs ------ x (6,1) The state vector [r;v] t Time fType Type of equations 'car','sph','cyl' a (3,1) External acceleration* mu Gravitational parameter* *Optional ------- Outputs ------- xDot (6,1) The derivative of the state vector --------------------------------------------------------------------------
Orbit: OrbitMechanics/CylOrb Orbit: OrbitMechanics/SphOrb SC: BasicOrbit/FOrbCart
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