Junruoyu Zheng
Active stall flutter suppression for a revised Leishman-Beddoes Model
Zheng, Junruoyu; Pontillo, Alessandro; Chen, Lejun; Whidborne, James F.
Authors
Dr Alessandro Pontillo Alessandro.Pontillo@uwe.ac.uk
Lecturer in Aerospace Sytems
Lejun Chen
James F. Whidborne
Abstract
This paper proposes a nonlinear disturbance observer (NDO)-based sliding mode control (SMC) method to the problem of stall flutter suppression for a revised Leishman-Beddoes (L-B) model. To capture accurate aerodynamic characteristics whilst reducing the plant model mismatch, the dynamics of the separation point and the shift of the aerodynamic center are analyzed to improve the structure of the L-B model. Based on this revised L-B model, an active flutter suppression problem that includes aerodynamic disturbances and actuator dynamics is addressed. The inclusion of the actuator dynamics means that the aerodynamic disturbance from the flow separation, induced by the revised L-B model, is considered as an "unmatched"disturbance. To counteract the effect of unmatched disturbances, an NDO-based sliding mode control scheme is applied to suppress stall flutter and to ensure rapid reference tracking performance in both steady and unsteady flow conditions. Simulation results show the improvements of the proposed revised L-B model via a comparative analysis. In addition, the efficacy of the proposed stall flutter suppression scheme is demonstrated.
Journal Article Type | Article |
---|---|
Acceptance Date | Oct 11, 2023 |
Online Publication Date | Oct 11, 2023 |
Publication Date | Oct 11, 2023 |
Deposit Date | Apr 22, 2024 |
Journal | Journal of Aerospace Engineering |
Print ISSN | 0893-1321 |
Electronic ISSN | 1943-5525 |
Publisher | American Society of Civil Engineers |
Peer Reviewed | Peer Reviewed |
Volume | 37 |
Issue | 1 |
DOI | https://doi.org/10.1061/JAEEEZ.ASENG-5003 |
Public URL | https://uwe-repository.worktribe.com/output/11886207 |
You might also like
Flight dynamic modelling and simulation of large flexible aircraft
(2018)
Book Chapter
Verification of a low fidelity fast simulation framework through RANS simulations
(2019)
Journal Article
A benchtop flight control demonstrator
(2019)
Journal Article
Investigating pitching moment stall through dynamic wind tunnel test
(2019)
Journal Article
Aeroelastic damping estimation for a flexible high-aspect-ratio wing
(2021)
Journal Article
Downloadable Citations
About UWE Bristol Research Repository
Administrator e-mail: repository@uwe.ac.uk
This application uses the following open-source libraries:
SheetJS Community Edition
Apache License Version 2.0 (http://www.apache.org/licenses/)
PDF.js
Apache License Version 2.0 (http://www.apache.org/licenses/)
Font Awesome
SIL OFL 1.1 (http://scripts.sil.org/OFL)
MIT License (http://opensource.org/licenses/mit-license.html)
CC BY 3.0 ( http://creativecommons.org/licenses/by/3.0/)
Powered by Worktribe © 2025
Advanced Search