Title :
Spacecraft guidance and robust attitude control with precise pointing the flexible antennas
Author :
Somov, Ye.I. ; Butyrin, S.A. ; Somov, S.Ye.
Author_Institution :
Samara Sci. Center, Russian Acad. of Sci. (RAS), Samara, Russia
Abstract :
New approach for modelling a physical hysteresis damping the flexible spacecraft structure oscillations, is developed. New results on spacecraft attitude guidance and digital robust control with precise pointing the large-scale flexible antennas, are presented.
Keywords :
antennas; attitude control; robust control; space vehicles; digital robust control; flexible antennas; physical hysteresis damping; robust attitude control; spacecraft guidance; spacecraft structure oscillations; Attitude control; Control systems; Damping; Differential equations; Friction; Hysteresis; Large-scale systems; Mathematical model; Robust control; Space vehicles;
Conference_Titel :
Control Applications, (CCA) & Intelligent Control, (ISIC), 2009 IEEE
Conference_Location :
St. Petersburg
Print_ISBN :
978-1-4244-4601-8
Electronic_ISBN :
978-1-4244-4602-5
DOI :
10.1109/CCA.2009.5281102
