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Volume 38 Issue 2
Feb.  2012
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Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  (2): 160-165.
Wang Pengbo, Zhou Yinqing, Chen Jie, et al. Imaging algorithm for high-resolution space-borne spotlight SAR data based on two dimension deramp processing[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(01): 72-75. (in Chinese)
Citation: Li Huifeng, Xiao Jin, Zhang Ranet al. Hypersonic vehicle rigid/elastic coupled dynamic modeling[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (2): 160-165. (in Chinese)
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Hypersonic vehicle rigid/elastic coupled dynamic modeling

  • School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 14 Oct 2010
  • Publish Date: 29 Feb 2012
    Abstract
  • Extensive use of lifting body, wave-rider aerodynamic layout and other composite materials, thin-walled structures, lead the frequency of structural vibration and rigid body motion very close. This yields a great challenge to the vehicle control system design. Taking into account the transverse displacement, a specific simplification which treats the vehicle body as two mass center fixed cantilever beams was adopted. And the hypersonic aircraft-s rigid body/elastic coupling model was derived based on the principle of virtual work and Lagrange equations. After comparing the open-looped poles of new coupling model and traditional rigid body model, a conclusion that the short-period vibration mode and the structures vibration mode tightly coupled with each other was made. The centrifugal force affected the height and long-period mode, and the effect on the flight path can not be ignored. Finally, changes in flight speed and structural damping on the dynamic performance of coupled model were analyzed. Results show that flight speeds significantly affect the rigid body motion modes, while the structural damping mainly changes in elastic mode.

     

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    • References(6)
  • [1]
    杨超,许赟,谢长川.高超声速飞行器气动弹性力学研究综述[J].航空学报,2010,31(1):1-11 Yang Chao,Xu Yun,Xie Changchuan.Review of studies on aeroelasticity of hypersonic vehicles[J].ACTA Aeronautica et Astronautica sinica,2010,31(1):1-11(in Chinese)
    [2]
    Waszak M R,Schmit D K.On the flight dynamics of aeroelastic vehicles .AIAA-1986-2077-388,1986
    [3]
    Bolender M A,Doman D B.A non-linear model for the longitudinal dynamics of a hypersonic air-breathing vehicle .AIAA-2005-6255,2005
    [4]
    Parker J T,Bolender M A,Doman D B.Control-oriented modeling of an air-breathing hypersonic vehicle .AIAA-27830-611,2007
    [5]
    Clark A D,Mirmirani M D,et al.An aero-propulsion integrated elastic model of a generic air-breathing hypersonic vehicle .AIAA-2006-6560,2006
    [6]
    Rodriguez A A,Dickeson J J,Sridharan S,et al.Control relevant modeling,analysis,and design for scramjet-powered hypersonic vehicles .AIAA-2009-7287-980,2009
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