[1] YUE T,ZHANG X Y,WANG L X,et al.Flight dynamic modeling and control for a telescopic wing morphing aircraft via asymmetric wing morphing[J].Aerospace Science & Technology,2017,70:328-338.
[2] JIANG W L,DONG C Y,WANG Q.A systematic method of smooth switching LPV controllers design for a morphing aircraft[J].Chinese Journal of Aeronautics,2015,28(6):1640-1649.
[3] 殷明,陆宇平,何真.变体飞行器LPV建模与鲁棒增益调度控制[J].南京航空航天大学学报,2013,45(2):202-208.YIN M,LU Y P,HE Z.LPV Modeling and robust gain scheduling control of morphing aircraft[J].Journal of Nanjing University of Aeronautics and Astronautics,2013,45(2):202-208(in Chinese).
[4] AFONSO F,VALE J,LAU F,et al.Performance based multidisciplinary design optimization of morphing aircraft[J].Aerospace Science and Technology,2017,67:1-12.
[5] AJAJ R M,BEAVERSTOCK C M,FRISWELL M I.Morphing aircraft:The need for a new design philosophy[J].Aerospace Science and Technology,2016,49:154-166.
[6] SU H Q, HUANG Z, BAO X X,et al.Morphing process research of UAV with PID controller[J].Procedia Engineering,2015,99:873-877.
[7] WU Z H,LU J C,ZHOU Q,et al.Modified adaptive neural dynamic surface control for morphing aircraft with input and output constraints[J].Nonlinear Dynamics,2016,87(4):2367-2383.
[8] WANG L,LIU C S,GONG H J.A novel robust controller with command filter for uncertain morphing aircraft[J].International Journal of Computer and Electrical Engineering,2018,10(1):523-523.
[9] AHMADI A A,PARRILO P A.Sum of squares certificates for stability of planar, homogeneous, and switched systems[J].IEEE Transaction on Automatic Control,2017,62(10):5269-5273.
[10] YUAN S,SCHUTTER B D,BALDI S.Robust adaptive tracking control of uncertain slowly switched linear systems[J].Nonlinear Analysis Hybrid Systems,2018,27:1-12.
[11] WANG R H,XING J C,XIANG Z R.Finite-time stability and stabilization of switched nonlinear systems with asynchronous switching[J].Applied Mathematics and Computation,2018,316(1):229-244.
[12] ZHAO X D,SHI P,YIN Y F,et al.New results on stability of slowly switched systems:A multiple discontinuous Lyapunov function approach[J].IEEE Transaction on Automatic Control,2016,62(7):3502-3509.
[13] HE X,ZHAO J.Multiple Lyapunov functions with blending for induced l2-norm control of switched LPV systems and its application to an F-16 aircraft model[J].Asian Journal of Control,2014,16(1):149-161.
[14] 王青,王通,后德龙,等.基于速度线性化的变体飞行器鲁棒LPV控制[J].系统工程与电子技术,2014,36(6):1130-1136.WANG Q,WANG T,HOU D L,et al.Robust LPV control for morphing vehicles via velocity-based linearization[J].System Engineering and Electronics,2014,36(6):1130-1136(in Chinese).
[15] CHENG H Y, DONG C Y, JIANG W L,et al. Non-fragile switched H∞ control for morphing aircraft with asynchronous switching[J].Chinese Journal of Aeronautics,2017,30(3):1127-1139.
[16] 江未来, 董朝阳, 王通,等. 变体飞行器平滑切换LPV鲁棒控制[J]. 控制与决策, 2016, 31(1):66-72.JIANG W L, DONG C Y, WANG T,et al. Smooth switching LPV robust control for morphing aircraft[J].Control and Decision,2016,31(1):66-72(in Chinese).
[17] SEIGLER T M. Dynamics and control of morphing aircraft[D]. Charlottesville:Virginia Polytechnic Institute and State University, 2005:30-55
[18] ZHAO X D, YIN S, LI H Y,et al.Switching stabilization for a class of slowly switched systems[J].IEEE Transactions on Automatic Control,2014,60(1):221-226.
[19] XU S Y, CHEN T W.Robust H∞ control for uncertain stochastic systems with state delay[J].IEEE Transactions on Automatic Control,2002,47(12):2089-2094.
[20] TAO G.Multivariable adaptive control:A survey[J].Automatica,2014, 50(11):2737-2764. |