Global optimum spacecraft orbit control subject to bounded thrust in presence of nonlinear and random disturbances in a low earth orbit

The primary objective of this work is to develop an effective spacecraft orbit control algorithm suitable for spacecraft orbital maneuver and/or rendezvous. The actual governing equation of a spacecraft orbiting the earth is merely nonlinear. Disturbance forces resulting from aerodynamic drag, oblat...

Full description

Bibliographic Details

Published in:	The Egyptian journal of remote sensing and space sciences Vol. 15; no. 1; pp. 1 - 8
Main Author:	Habib, Tamer Mekky Ahmed
Format:	Journal Article
Language:	English
Published:	Elsevier B.V 01.06.2012 Elsevier
Subjects:	Drag Earth oblateness Orbit control Random disturbance Real coded genetic algorithms Orbit control Random disturbance Real coded genetic algorithms Drag Earth oblateness
ISSN:	1110-9823, 2090-2476
Online Access:	Get full text
Tags:	Add Tag No Tags, Be the first to tag this record!