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...

Celý popis

Podrobná bibliografia

Vydané v:	The Egyptian journal of remote sensing and space sciences Ročník 15; číslo 1; s. 1 - 8
Hlavný autor:	Habib, Tamer Mekky Ahmed
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	Elsevier B.V 01.06.2012 Elsevier
Predmet:	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
On-line prístup:	Získať plný text
Tagy:	Pridať tag Žiadne tagy, Buďte prvý, kto otaguje tento záznam!