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
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;
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
DOI :
10.1109/ISSCAA.2006.1627532
