Path: Orbit/ThreeBody
% Compute the Jacobi constant for a state in the CRTBP system. Centered at the barycenter. -------------------------------------------------------------------------- Form: C = CRTBPJacobi( x, mu ) -------------------------------------------------------------------------- ------ Inputs ------ x (6,1) The state vector [r;v] mu (1,1) Non-dimensional mass parameter. Smaller mass divided by total mass of system. ------- Outputs ------- C (1,1) Jacobi constant of integration --------------------------------------------------------------------------
Back to the Orbit Module page