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Volume 37 Issue 5
May  2011
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Journal of Beijing University of Aeronautics and Astronautics  > 2011  >  37(5): 560-563.
Huang Xiyuan, Wang Qing, Dong Chaoyanget al. Robust adaptive control for hypersonic vehicle based on dynamic inversion[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(5): 560-563. (in Chinese)
Citation: Huang Xiyuan, Wang Qing, Dong Chaoyanget al. Robust adaptive control for hypersonic vehicle based on dynamic inversion[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(5): 560-563. (in Chinese)
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Robust adaptive control for hypersonic vehicle based on dynamic inversion

  • 1.

    School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • 2. School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 01 Mar 2010
  • Publish Date: 30 May 2011
    Abstract
  • For the feature that hypersonic vehicle motion model is highly nonlinear, multivariable coupled and includes uncertain parameters, a robust adaptive control strategy based on nonlinear dynamic inversion for the hypersonic vehicle was proposed. By decomposing the vehicle motion equations into two subsystems, namely, a velocity subsystem and an altitude subsystem, and incorporating the design of virtual control commands and nonlinear dynamic inversion technology, the stable velocity and altitude tracking were achieved. To eliminate the effect of the model uncertainties and external disturbances, the robust adaptive sliding mode control method was adopted. Simulation results show that the proposed method not only satisfies the velocity and altitude tracking performance requirements, but also is robust to model uncertainties and external disturbances.

     

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  • [1] 吴宏鑫,孟斌.高超声速飞行器控制研究综述[J].力学进展,2009,39(6):756-765 Wu Hongxin,Meng Bin.Review on the control of hypersonic flight vehicles[J].Advances In Mechanics,2009,39(6):756-765(in Chinese) [2] Fidan B,Mirmirani M,Ioannou P A.Flight dynamics and control of air-breathing hypersonic vehicle:review and new directions // AIAA International Space Planes and Hypersonic Systems and Technologies.Norfolk,Virginia:AIAA,2003-7081 [3] Xu H,Mirmirani M,Ioannou P.Adaptive sliding mode control design for a hypersonic flight vehicle[J].Journal of Guidance,Control,and Dynamics,2004,27(5):829-838 [4] Wang Q,Stengel R F.Robust nonlinear control of a hypersonic aircraft[J].Journal of Guidance,Control,and Dynamics,2000,23(4):577-585 [5] 刘燕斌,陆宇平.基于反步法的高超音速飞机纵向逆飞行控制[J].控制与决策,2007,22(3):313-317 Liu Yanbin,Lu Yuping.Longitudinal inversion flight control based on backstepping for hypersonic vehicle[J].Control and Decision,2007,22(3):313-317(in Chinese) [6] Parker J T,Serrani A,Yurkovich S,et al.Control-oriented modeling of an air-breathing hypersonic vehicle[J].Journal of Guidance,Control,and Dynamics,2007,30(3):856-869
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