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

• Published in: Chinese journal of aeronautics 2013-08, Vol.26 (4), p.909-917
• Main Authors: Yue, Ting, Wang, Lixin, Ai, Junqiang
• Format: Article
• Language: English
• Subjects: Gain self-scheduled; H∞ robust control; Linear parameter varying; Morphing aircraft; V模型; Wing transition; 变形控制; 多回路控制器; 线性化方法; 过渡过程; 非线性动力学方程; 飞机机翼; 鲁棒稳定性
• ISSN: 1000-9361
• DOI: 10.1016/j.cja.2013.06.004

This article investigates gain self-scheduled H 1 robust control system design for a tailless fold- ing-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 1 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 1 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.