DocumentCode
1311340
Title
Attitude Coordination Control for a Group of Spacecraft Without Velocity Measurements
Author
Zou, An-Min ; Kumar, Krishna Dev ; Hou, Zeng-Guang
Author_Institution
Dept. of Aerosp. Eng., Ryerson Univ., Toronto, ON, Canada
Volume
20
Issue
5
fYear
2012
Firstpage
1160
Lastpage
1174
Abstract
This paper investigates the problem of velocity-free attitude coordination control for a group of spacecraft with attitude represented by modified Rodrigues parameters. The communication flow among neighbor spacecraft is described by an undirected connected graph. Two velocity-free attitude coordination control schemes are proposed. By employing linear reduced-order observers, robust control and Chebyshev neural networks, the first velocity-free control scheme allows a group of spacecraft to simultaneously align their attitude and track a time-varying reference attitude even in the presence of unknown mass moment of inertia matrix and external disturbances, where all spacecraft have access to the common reference attitude. The second control law guarantees a group of spacecraft to track a time-varying reference attitude without requiring velocity measurements even when the common reference attitude is available only to a subset of the group members. Furthermore, the stability of the overall closed-loop system for both control laws is guaranteed by a Lyapunov-based approach. Finally, numerical simulations are presented to demonstrate the performance of the proposed controllers.
Keywords
Lyapunov methods; attitude control; closed loop systems; neural nets; observers; robust control; space vehicles; time-varying systems; velocity control; Chebyshev neural networks; Lyapunov-based approach; communication flow; external disturbances; inertia matrix; linear reduced-order observers; modified Rodrigues parameters; overall closed-loop system; robust control; second control law; spacecraft; time-varying reference attitude; undirected connected graph; velocity-free attitude coordination control; velocity-free control scheme; Attitude control; Chebyshev approximation; Control systems; Observers; Space vehicles; Symmetric matrices; Velocity measurement; Adaptive control; Chebyshev neural networks (CNNs); attitude coordination; spacecraft formation flying (SFF); without velocity measurements;
fLanguage
English
Journal_Title
Control Systems Technology, IEEE Transactions on
Publisher
ieee
ISSN
1063-6536
Type
jour
DOI
10.1109/TCST.2011.2163312
Filename
6006556
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