Quasi-LPV Modeling and Parameter-dependent Optimal Control of Morphing Wing Aircraft
31st Congress of the International Council of the Aeronautical Sciences (ICAS), Belo Horizonte, Brazil, Sep. 2018
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A near-optimal gain-scheduling strategy for the morphing aircraft flight control design is proposed. Nonlinear parameter-dependent dynamics of the morphing aircraft is transformed into a quasi-linear parameter-varying form. Assuming that the morphing parameters are determined in an outer-loop to meet system requirements, an inner-loop controller is designed by optimal control scheme. An algebraic Riccati equation using the parameter-dependent coefficient matrices is solved to design a near-optimal controller. Numerical simulation is performed to demonstrate the effectiveness of the proposed scheme.
https://icas.org/ICAS_ARCHIVE/ICAS2018/data/papers/ICAS2018_0218_paper.pdfBibTeX@inproceedings{Lee2018,
title = {Quasi-LPV Modeling and Parameter-dependent Optimal Control of Morphing Wing Aircraft},
author = {Jihoon Lee and Youdan Kim},
year = {2018},
booktitle = {31st Congress of the International Council of the Aeronautical Sciences (ICAS), Belo Horizonte, Brazil, Sep. 2018},
}