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Journal of Projectiles, Rockets, Missiles and Guidance >

2015 , Vol. 35 >Issue 5: 1 - 4

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2015.05.001

MISSILES AND GUIDANCE TECHNOLOGY

Characteristic Model Based Attitude Control Method for Hypersonic Vehicle

  • WANG Liqi ,
  • ZHOU Jun ,
  • LIN Peng
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  • Institute of Precision Guidance and Control, Northwestern Polytechnical University, Xi'an 710072, China

Received date: 2015-07-14

  Online published: 2025-05-28

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Abstract

Since that hypersonic vehicle has time-varying parameter and uncertainty of model, an online control method based on characteristic model was proposed. First, the input space was divided into many local subspaces by clustery analysis, and then the control-orient model was combined by characteristic model which was identified in those local subspaces. Secondly, the variable structure controller was designed. Finally, simulation results proved the capability of online controller and guaranteed the robustness of system, besides it can be implemented easily in engineering.

Key words： hypersonic vehicle; characteristic model; data clustering; control-oriented modeling; variable structure control

Cite this article

WANG Liqi , ZHOU Jun , LIN Peng . Characteristic Model Based Attitude Control Method for Hypersonic Vehicle[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(5) : 1 -4 . DOI: 10.15892/j.cnki.djzdxb.2015.05.001

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