DocumentCode
2644133
Title
The optimal orbital control of the dive and ascent earth observing satellite
Author
Fu, Tianshuang ; Imado, Fumiaki
Author_Institution
Shinshu Univ., Nagano
fYear
2007
fDate
17-20 Sept. 2007
Firstpage
2625
Lastpage
2632
Abstract
In this paper, we propose observing the particular area which is in the emergency situation or suffered by a natural disaster with the Dive and Ascent earth observing Satellite (DAS). We selected the forces of the thrusters fixed to the satellite body three axes as the control variables, and obtained the optimal thrust patterns by using the Steepest Descent Method (SDM). Some of new ideas and study results are presented.
Keywords
artificial satellites; matrix algebra; optimal control; ascent earth observing satellite; dive earth observing satellite; natural disaster; optimal orbital control; optimal thrust patterns; steepest descent method; Control systems; Drag; Earth; Force control; Mathematical model; Mechanical systems; Optimal control; Satellites; Systems engineering and theory; Velocity control; Dive and ascent satellite; Optimal orbital control; Steepest descent method;
fLanguage
English
Publisher
ieee
Conference_Titel
SICE, 2007 Annual Conference
Conference_Location
Takamatsu
Print_ISBN
978-4-907764-27-2
Electronic_ISBN
978-4-907764-27-2
Type
conf
DOI
10.1109/SICE.2007.4421435
Filename
4421435
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