Article ID Journal Published Year Pages File Type
5472913 Aerospace Science and Technology 2017 9 Pages PDF
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 C⁎ 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
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