Distributed adaptive output feedback control design and application to a formation flight experiment

Date

2005-01-01

Author

Kutay, Ali Türker
Calise, Anthony J.
D'Andrea, Raffaello

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This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

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An approach for augmenting existing distributed controller designs for large-scale interconnected systems with neural network based adaptive elements is proposed. It is assumed that the controllers are interconnected in the same way as the plant and based on the available measurements, a single hidden layer neural network is introduced for each subsystem to partially cancel the effects of the sub-system interconnections and modeling errors on tracking performance. Boundedness of error signals is shown through Lyapunov's direct method. Effectiveness of the approach is demonstrated on a wind tunnel experiment representing aerial vehicles flying in a highly aerodynamically coupled formation. Copyright © 2005 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.

URI

https://hdl.handle.net/11511/57926

DOI

https://doi.org/10.2514/6.2005-6368

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

A. T. Kutay, A. J. Calise, and R. D’Andrea, “Distributed adaptive output feedback control design and application to a formation flight experiment,” 2005, vol. 7, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/57926.