DocumentCode
3174899
Title
Control of Large Angle Attitude Maneuvers for Rigid Bodies Using Sum of Squares
Author
Gollu, Narendra ; Rodrigues, Luis
Author_Institution
Concordia Univ., Montreal
fYear
2007
fDate
9-13 July 2007
Firstpage
3156
Lastpage
3161
Abstract
The main contribution of this paper is the development of a two step integrated and systematic approach for modeling and control of large angle maneuvers of a rigid body through convex optimization. In the first step, the attitude dynamics of the rigid body are represented by modified Rodriguez parameters (MRP). In the second step, a Lyapunov- based controller synthesis is performed based on the Sum of Squares (SOS) technique. The key observation that makes rigid body control amenable to an efficient (convex) design technique such as SOS is that both quaternions and modified Rodriguez parameters enable the representation of the attitude dynamics of a rigid body by polynomial vector fields. The model proposed in this paper will use MRP instead of quaternions to represent the rigid body attitude to yield a minimal parameterization. The effectiveness of the proposed control technique is shown in simulations for a large angle maneuver corresponding to a satellite rotation about a fixed axis.
Keywords
Lyapunov methods; artificial satellites; attitude control; control system synthesis; Lyapunov-based controller synthesis; convex optimization; large angle attitude maneuvers; modified Rodriguez parameters; rigid-body attitude control; satellite rotation; sum of squares; Angular velocity; Attitude control; Control system synthesis; Lyapunov method; Materials requirements planning; Quaternions; Satellites; Sliding mode control; Space vehicles; Vehicle dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2007. ACC '07
Conference_Location
New York, NY
ISSN
0743-1619
Print_ISBN
1-4244-0988-8
Electronic_ISBN
0743-1619
Type
conf
DOI
10.1109/ACC.2007.4283054
Filename
4283054
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