Gain self-scheduled H control for morphing aircraft in the wing transition process based on an LPV model

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Abstract

This article investigates gain self-scheduled H robust control system design for a tailless folding-wing morphing aircraft in the wing shape varying process. During the wing morphing phase, the aircraft’s dynamic response will be governed by time-varying aerodynamic forces and moments. Nonlinear dynamic equations of the morphing aircraft are linearized by using Jacobian linearization approach, and a linear parameter varying (LPV) model of the morphing aircraft in wing folding is obtained. A multi-loop controller for the morphing aircraft is formulated to guarantee stability for the wing shape transition process. The proposed controller uses a set of inner-loop gains to provide stability using classical techniques, whereas a gain self-scheduled H outer-loop controller is devised to guarantee a specific level of robust stability and performance for the time-varying dynamics. The closed-loop simulations show that speed and altitude vary slightly during the whole wing folding process, and they converge rapidly after the process ends. This proves that the gain self-scheduled H robust controller can guarantee a satisfactory dynamic performance for the morphing aircraft during the whole wing shape transition process. Finally, the flight control system’s robustness for the wing folding process is verified according to uncertainties of the aerodynamic parameters in the nonlinear model.

Keywords

Gain self-scheduled
H robust control
Linear parameter varying
Morphing aircraft
Wing transition

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Yue Ting is a postdoctor at School of Aeronautic Science and Engineering, Beihang University. He received the B.S., M.S. and Ph.D. degrees in aircraft design from Beihang University in 2004, 2006 and 2010 respectively. His main research interest is aircraft flight dynamics and control.

Wang Lixin is a professor in Beihang University. His main research interest lies in aircraft design, flight dynamics and flight control.

Ai Junqiang is a researcher in The First Aircraft Design Institute of AVIC. His main research interest lies in aircraft design.

Peer review under responsibility of Editorial Committee of CJA.

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