Path: Orbit/OrbitMechanics
% Variational Keplerian equations with the acceleration in tangential coordinates. Computes the right hand side of the variational equations based on the Gauss formulation with the acceleration in tangential coordinates. These equations are singular when i = 0. Since version 1. -------------------------------------------------------------------------- Form: dElDt = VarGausT( el, aD, tol, mu ) -------------------------------------------------------------------------- ------ Inputs ------ el Elements vector [a,i,W,w,e,M] aD Disturbance vector [tangent,normal,z] tol Tolerance for Kepler's equation solver mu Gravitational parameter ------- Outputs ------- dElDt Derivative to the elements -------------------------------------------------------------------------- References: Battin, R.H., An Introduction to the Methods and Mathematics of Astrodynamics, AIAA, New York, 1987, pp. 484-490. --------------------------------------------------------------------------
SC: BasicOrbit/E2Nu SC: BasicOrbit/M2EEl
Back to the Orbit Module page