Spacecraft attitude maneuvers using composite adaptive control with invariant sliding manifold

Dando, Aaron (2009). Spacecraft attitude maneuvers using composite adaptive control with invariant sliding manifold. In: Proceedings of the 48th IEEE Conference on Decision and Control (CDC) held jointly with 2009 28th Chinese Control Conference. 2009 CDC/CCC: The combined 48th IEEE Conference on Decision and Control and 28th Chinese Control Conference, Shanghai, China, (4535-4540). 15-18 December, 2009. doi:10.1109/CDC.2009.5400350


Author Dando, Aaron
Title of paper Spacecraft attitude maneuvers using composite adaptive control with invariant sliding manifold
Conference name 2009 CDC/CCC: The combined 48th IEEE Conference on Decision and Control and 28th Chinese Control Conference
Conference location Shanghai, China
Conference dates 15-18 December, 2009
Proceedings title Proceedings of the 48th IEEE Conference on Decision and Control (CDC) held jointly with 2009 28th Chinese Control Conference   Check publisher's open access policy
Journal name Proceedings of the IEEE Conference on Decision and Control   Check publisher's open access policy
Place of Publication Piscataway, NJ, United States
Publisher Institute of Electrical and Electronics Engineers
Publication Year 2009
Sub-type Fully published paper
DOI 10.1109/CDC.2009.5400350
Open Access Status
ISBN 9781424438716
9781424438723
ISSN 0191-2216
Start page 4535
End page 4540
Total pages 6
Language eng
Formatted Abstract/Summary
An adaptive control strategy is developed for spacecraft attitude tracking maneuvers, in the presence of structured uncertainty in the spacecraft inertia parameters. The proposed strategy incorporates a composite parameter update law, which guarantees global asymptotic stability of the overall closed-loop system. A stability analysis is performed using Lyapunov's direct method, in conjunction with Bar-balat's lemma. The asymptotic convergence results provided by this control strategy require persistently exciting reference trajectory commands. Simulation results are provided which demonstrate the performance of the proposed adaptive control design for a rigid spacecraft tracking a time-varying reference trajectory.
Subjects 2207 Control and Systems Engineering
2606 Control and Optimization
2611 Modelling and Simulation
Q-Index Code E1
Q-Index Status Provisional Code
Institutional Status UQ

Document type: Conference Paper
Collection: School of Mechanical & Mining Engineering Publications
 
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