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
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;
Conference_Titel :
Recent Advances in Space Technologies (RAST), 2015 7th International Conference on
Conference_Location :
Istanbul
Print_ISBN :
978-1-4673-7760-7
DOI :
10.1109/RAST.2015.7208442
