Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
5472913 | Aerospace Science and Technology | 2017 | 9 Pages |
Abstract
This paper proposes a controller design method for preventing pilot-induced-oscillation (PIO) based on nonlinear optimal output regulation theory and center stable manifold method. The type of PIO considered is due to actuator rate limiting and the proposed controller assures Câ handling quality by the optimal control when actuator works in the linear region. The simulation result shows that the proposed nonlinear controller has better tracking performance in comparison with the linear optimal output regulation controller. The robustness of the designed controller against parametrization error, noise and time-delay is also verified.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Anh Tuan Tran, Noboru Sakamoto, Yoshimitsu Kikuchi, Koichi Mori,