The Stark problem applied to astrodynamics is a two body Keplerian model plus a constant perturbation acceleration.

This coefficient files and a basic wrapper for solving the Stark or Kepler problems using the F&G series approach along with a generalized Sundman Transformation: link

 

Details are found here:


Pellegrini, E., Russell, R.P., Vittaldev, V., F and G Taylor Series Solutions to the Stark and Kepler Problems with Sundman Transformations,
Celestial Mechanics and Dynamical Astronomy, (accepted: Jan 2014), published on-line March 2014, DOI 10.1007/s10569-014-9538-7.

 

 

F&G Stark and Kepler Series

WELCOME!

 

Last updated:
December 5, 2016

 

 

Orbital Mechanics Discipline Area

research group of:
Ryan P. Russell

Associate Professor, Ph.D

ryan.russell@utexas.edu

 


Department of Aerospace Engineering and Engineering Mechanics