DocumentCode :
631214
Title :
Economical attitude and orbit control of information satellites by electromechanical, magnetic and plasma drivers
Author :
Somov, Yevgeny ; Buryrin, Sergey ; Somov, Sergey
Author_Institution :
Dept. of the GNC, Samara State Tech. Univ., Samara, Russia
fYear :
2013
fDate :
12-14 June 2013
Firstpage :
1109
Lastpage :
1114
Abstract :
Methods for attitude & orbit control of the information satellites with economical expending of the onboard energy and fuel resources are presented. We consider small information spacecraft with an orbit altitude from 550 up to 1500 km when its lifetime must be up to 10 years and economical control is actual problem.
Keywords :
Earth orbit; artificial satellites; attitude control; driver circuits; fuel; plasma devices; space vehicle electronics; attitude control; economical attitude; economical control; economical expending; electromechanical driver; fuel resources; information satellites; information spacecraft; magnetic driver; onboard energy; orbit altitude; orbit control; plasma driver; Attitude control; Digital control; Orbits; Quaternions; Space vehicles; Torque; Vectors; economical control; guidance; information spacecraft;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Recent Advances in Space Technologies (RAST), 2013 6th International Conference on
Conference_Location :
Istanbul
Print_ISBN :
978-1-4673-6395-2
Type :
conf
DOI :
10.1109/RAST.2013.6581169
Filename :
6581169
Link To Document :
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