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Control-Oriented Modeling and Simulation on Rigid-Aeroelasticity Coupling for Hypersonic Vehicle

Xiao Liping Zhang Yong Lu Yuping

南京航空航天大学学报(英文版)2015,Vol.32Issue(1):70-80,11.
南京航空航天大学学报(英文版)2015,Vol.32Issue(1):70-80,11.

Control-Oriented Modeling and Simulation on Rigid-Aeroelasticity Coupling for Hypersonic Vehicle

Control-Oriented Modeling and Simulation on Rigid-Aeroelasticity Coupling for Hypersonic Vehicle

Xiao Liping 1Zhang Yong 1Lu Yuping2

作者信息

  • 1. UAV Research Institute, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, P.R.China
  • 2. School of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, P.R.China
  • 折叠

摘要

关键词

hypersonic vehicle/wave-rider/aeroelasticity/modeling/dynamic properties

Key words

hypersonic vehicle/wave-rider/aeroelasticity/modeling/dynamic properties

分类

航空航天

引用本文复制引用

Xiao Liping,Zhang Yong,Lu Yuping..Control-Oriented Modeling and Simulation on Rigid-Aeroelasticity Coupling for Hypersonic Vehicle[J].南京航空航天大学学报(英文版),2015,32(1):70-80,11.

南京航空航天大学学报(英文版)

OACSCDCSTPCD

1005-1120

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