Paper Info
Title
Periodic H-2 Synthesis For Spacecraft Attitude Control With Magnetorquers And Reaction Wheels
Abstract
Particularly attractive for small satellites, the use of magnetic torquers for attitude control is still a difficult problem. Indeed, equations are naturally time-varying and suffers from controllability issues. In this paper, a generic model, taking different kinds of pointing and different kinds of actuators into account, is proposed, linearized and then discretized. Recent studies demonstrate how combining magnetorquers and reaction wheels is attractive. Following this line, latest LMI synthesis techniques for static periodic controller are applied in this paper to the attitude control problem of a spacecraft equipped with both actuation systems. Simulation results are provided, showing the performance of the obtained control law.
Year
Venue
DocType
2011
2011 50TH IEEE CONFERENCE ON DECISION AND CONTROL AND EUROPEAN CONTROL CONFERENCE (CDC-ECC)
Conference
ISSN
Citations 
PageRank 
0743-1546
5
0.56
References 
Authors
7
6
Name
Order
Citations
PageRank
Jean-Francois Tregouet1315.88
Denis Arzelier227926.58
Dimitri Peaucelle330931.56
Yoshio Ebihara416419.52
Christelle Pittet5274.58
Alexandre Falcoz6151.53