Conference
Trajectory accuracy assessment during intrack thrusting using energy integrals
Abstract
The paper aims to address questions on intrack thrusting and to test variation of parameters (VOP) fourth order Runge-Kutta integration in equinoctial orbit elements with significant intrack thrust accelerations.
Authors
Wright JR
Volume
87
Pagination
pp. 321-335
Publication Date
January 1, 1994
Conference proceedings
Advances in the Astronautical Sciences
Issue
1
ISSN
0065-3438