Morphing aircraft can adaptively alter configuration according to the different flight conditions or a variety of missions to ensure the optimal aerodynamic performance in flight. A class of variable-span morphing aircraft were considered,and the controller design synthesis for linear parameter varying( LPV) systems with non-affine parameter dependent configuration was researched. Jacobian linearization approach,as well as exact fitting method,was used on multiple balance points to transform the nonlinear m...
网络出版地址:www.cnki.net/kcms/detail/11.2625.V.20170213.1026.002.html引用格式:温暖,刘正华,祝令谱,等.非仿射参数依赖LPV模型的变体飞行器H∞控制[J].北京航空航天大学学报,2017,43(10):2073-2080.WEN N,LIU Z H,ZHU L P,et al.H∞control for morphing aircraft via no
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