DocumentCode
1869087
Title
Adaptive attitude control of a flexible satellite
Author
Bahrami, M. ; Nezhad, R. Kalantari
Author_Institution
Dept. of Mech. Eng., Amir Kabir Univ. of Technol., Tehran
fYear
2006
fDate
19-21 Jan. 2006
Lastpage
1333
Abstract
Dynamics model of a satellite with two solar panels is derived. It is assumed that solar panels are connected to central rigid body by two torsional flexible rods. A model reference adaptive controller is designed and its stability is proven by Lyapunov method. Capability of controller in an attitude maneuver by a numerical simulation is shown
Keywords
Lyapunov methods; adaptive control; attitude control; Lyapunov method; attitude control; attitude maneuver; flexible satellite; model reference adaptive controller; rigid body; solar panels; stability; torsional flexible rods; Adaptive control; Attitude control; Centralized control; Control systems; Gravity; Open loop systems; Parameter estimation; Programmable control; Satellites; Stability;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aerospace and Astronautics, 2006. ISSCAA 2006. 1st International Symposium on
Conference_Location
Harbin
Print_ISBN
0-7803-9395-3
Type
conf
DOI
10.1109/ISSCAA.2006.1627532
Filename
1627532
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