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颤振抑制中的测量点和压电驱动器的分布(英文)

Distribution of Measuring Points and Piezoelectric Actuators in Flutter Suppression
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摘要 Single input/single output (SISO), single input/multi output(SIMO) multi input/ multi output (SIMO) control laws for activeflutter suppression are designed and realized wind tun- nel tests.Reasonable agreement between analytical and tested results isachieved. Based on these re- sults, the distribution of responsemeasuring points and piezoelectric actuators is investigated. Single input/single output (SISO), single input/multi output(SIMO) multi input/ multi output (SIMO) control laws for activeflutter suppression are designed and realized wind tun- nel tests.Reasonable agreement between analytical and tested results isachieved. Based on these re- sults, the distribution of responsemeasuring points and piezoelectric actuators is investigated.
作者 陈伟民 管德 李敏 诸德超
机构地区 Dept. of Mechanics and Engineering Science Dept. of Flight Vehicle Design and Applied Mechanics The State Key Lab. of Nonlinear Mechanics
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2002年第1期33-37,共5页 中国航空学报（英文版）
基金 NationalNatureScienceFoundationofChina(60 0 3 40 10 ) PostDoctorScienceFoundationofChina
关键词 FLUTTER wind tunnel PIEZOELECTRIC flutter wind tunnel piezoelectric
分类号 V215.34 [航空宇航科学与技术—航空宇航推进理论与工程]
  • 相关文献

参考文献3

  • 1管德,陈伟民,李敏,诸德超.FLUTTER SUPPRESSION USING DISTRIBUTED PIEZOELECTRIC ACTUATORS[J].Chinese Journal of Aeronautics,2000,13(4):211-215. 被引量：2
  • 2Moore B C.Principal component analysis in linear system:controllability,observability and model reduction[J].IEEE Transaction on Automatic Control,1981,AC-26(1),17-31.
  • 3Anderson L R.Order reduction of meroelastic models through LK transformation and riecati iteration[R].AIAA 93-3795 CP,1993.

二级参考文献8

  • 1[6] Hwang W S, Park H. C. Finite element modeling of piezoelectric sensors and actuators[J]. AIAA Journal, 1993, 31(5): 930～937.
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  • 4[1] Heeg J. Analytical and experimental investigation of flutter suppression by piezoelectric actuation[R]. NASA TP 3241, 1993.
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共引文献1

Chinese Journal of Aeronautics
2002年 第1期

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