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变体飞行器LPV建模与鲁棒增益调度控制 被引量:23
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作者 殷明 陆宇平 何真 《南京航空航天大学学报》 EI CAS CSCD 北大核心 2013年第2期202-208,共7页
以可变翼展的变体飞行器为对象,研究了一类变体飞行器的建模与控制问题。分析了飞行器纵向气动参数与翼展变形的关系,构建了气动参数函数。用Jacobian线性化方法,建立了飞行器的线性变参数(Linear pa-rameter varying,LPV)模型,分析了... 以可变翼展的变体飞行器为对象,研究了一类变体飞行器的建模与控制问题。分析了飞行器纵向气动参数与翼展变形的关系,构建了气动参数函数。用Jacobian线性化方法,建立了飞行器的线性变参数(Linear pa-rameter varying,LPV)模型,分析了变体过程中飞行器特征的变化。为保证变体过程的稳定,采用鲁棒增益调度控制方法设计了全局控制器,其设计条件具有线性矩阵不等式(Linear matrix inequality,LMI)的形式。对采用所设计控制器的变体飞行器进行了仿真验证。结果表明:翼展变形对飞行器气动参数有明确的影响,能够直接改变飞行器的系统特征;设计的鲁棒增益调度控制器能实现预期的运动过程,并保证变体过程的全局稳定。 展开更多
关键词 变体飞行器 气动参数函数 线性变参数 鲁棒增益调度 线性矩阵不等式
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Three-dimensional aerodynamic optimization design of high-speed train nose based on GA-GRNN 被引量:24
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作者 YAO ShuanBao GUO DiLong YANG GuoWei 《Science China(Technological Sciences)》 SCIE EI CAS 2012年第11期3118-3130,共13页
With the speed upgrade of the high-speed train,the aerodynamic drag becomes one of the key factors to restrain the train speed and energy saving.In order to reduce the aerodynamic drag of train head,a new parametric a... With the speed upgrade of the high-speed train,the aerodynamic drag becomes one of the key factors to restrain the train speed and energy saving.In order to reduce the aerodynamic drag of train head,a new parametric approach called local shape function(LSF) was adopted based on the free form surface deformation(FFD) method and a new efficient optimization method based on the response surface method(RSM) of GA-GRNN.The optimization results show that the parametric method can control the large deformation with a few design parameters,and can ensure the deformation zones smoothness and smooth transition of different deformation regions.With the same sample points for training,GA-GRNN performs better than GRNN to get the global optimal solution.As an example,the aerodynamic drag for a simplified shape with head + one carriage + tail train is reduced by 8.7%.The proposed optimization method is efficient for the engineering design of high-speed train. 展开更多
关键词 aerodynamic drag GA-GRNN PARAMETRIC high-speed trains
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