DocumentCode
1683255
Title
Attitude guidance and control of land-survey mini-satellite
Author
Somov, Yevgeny ; Butyrin, Sergey ; Somov, Sergey ; Salmin, Vadim
Author_Institution
Samara State Tech. Univ., Samara, Russia
fYear
2015
Firstpage
759
Lastpage
764
Abstract
Contemporary land-survey mini-satellites have general mass up to 500 kg and are placed onto the orbit altitudes up to 800 km. For such spacecraft some principle problems on optimal attitude guidance and robust control are considered and elaborated methods are presented for their solving.
Keywords
artificial satellites; attitude control; optimal control; robust control; attitude control; contemporary land-survey minisatellites; optimal attitude guidance; robust control; spacecraft; Arrays; Attitude control; Azimuth; Optimization; Position measurement; Quaternions; Torque; attitude control; guidance; mini-satellite;
fLanguage
English
Publisher
ieee
Conference_Titel
Recent Advances in Space Technologies (RAST), 2015 7th International Conference on
Conference_Location
Istanbul
Print_ISBN
978-1-4673-7760-7
Type
conf
DOI
10.1109/RAST.2015.7208442
Filename
7208442
Link To Document