Hugo Lhachemi, David Saussié and Guchuan Zhu
Article (2019)
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Open Access to the full text of this document Accepted Version Terms of Use: All rights reserved Download (297kB) |
Abstract
This note deals with the boundary control problem of a nonhomogeneous flexible wing evolving under unsteady aerodynamic loads. The wing is actuated at its tip by flaps and is modeled by a distributed parameter system consisting of two coupled partial differential equations. Based on the proposed boundary control law, the well-posedness of the underlying Cauchy problem is first investigated by resorting to the semigroup theory. Then, a Lyapunov-based approach is employed to assess the stability of the closed-loop system in the presence of bounded input disturbances.
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| Department: | Department of Electrical Engineering |
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| PolyPublie URL: | https://publications.polymtl.ca/3745/ |
| Journal Title: | IEEE Transactions on Automatic Control (vol. 64, no. 2) |
| Publisher: | IEEE |
| DOI: | 10.1109/tac.2018.2838040 |
| Official URL: | https://doi.org/10.1109/tac.2018.2838040 |
| Date Deposited: | 15 Jan 2019 12:07 |
| Last Modified: | 09 Apr 2025 09:32 |
| Cite in APA 7: | Lhachemi, H., Saussié, D., & Zhu, G. (2019). Boundary Control of a Nonhomogeneous Flexible Wing with Bounded Input Disturbances. IEEE Transactions on Automatic Control, 64(2), 854-861. https://doi.org/10.1109/tac.2018.2838040 |
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