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基于不变流形的高超声速飞行器动态面控制

后德龙 陈彬 王青 董朝阳

后德龙, 陈彬, 王青, 等 . 基于不变流形的高超声速飞行器动态面控制[J]. 北京航空航天大学学报, 2014, 40(11): 1595-1601. doi: 10.13700/j.bh.1001-5965.2013.0673
引用本文: 后德龙, 陈彬, 王青, 等 . 基于不变流形的高超声速飞行器动态面控制[J]. 北京航空航天大学学报, 2014, 40(11): 1595-1601. doi: 10.13700/j.bh.1001-5965.2013.0673
Hou Delong, Chen Bin, Wang Qing, et al. Dynamic surface control for hypersonic vehicle based on invariant manifold[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(11): 1595-1601. doi: 10.13700/j.bh.1001-5965.2013.0673(in Chinese)
Citation: Hou Delong, Chen Bin, Wang Qing, et al. Dynamic surface control for hypersonic vehicle based on invariant manifold[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(11): 1595-1601. doi: 10.13700/j.bh.1001-5965.2013.0673(in Chinese)

基于不变流形的高超声速飞行器动态面控制

doi: 10.13700/j.bh.1001-5965.2013.0673
基金项目: 国家自然科学基金资助项目(61273083)
详细信息
    作者简介:

    后德龙(1988-),男,安徽芜湖人,博士生,dlh8855@163.com.

  • 中图分类号: TP249;V448.22

Dynamic surface control for hypersonic vehicle based on invariant manifold

  • 摘要: 针对存在未知气动参数的吸气式高超声速飞行器纵向运动控制问题,提出一种基于不变流形的自适应动态面控制方法.通过合理假设将高超声速飞行器纵向模型分解为弹道倾角回路和速度回路,分别实现对弹道倾角和速度参考指令的跟踪.弹道倾角回路被表达为严反馈形式进行控制器设计.采用基于不变流形的自适应方法实现了对未知参数的估计.所提出的自适应动态面控制方案能保证未知参数估计误差全局一致稳定和闭环系统全局有界稳定,且估计器和控制器设计不存在耦合,因此参数设计更加容易.仿真结果验证了该控制方法在参数估计方面的显著优势和良好的闭环系统性能.

     

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出版历程
  • 收稿日期:  2013-11-21
  • 网络出版日期:  2014-11-20

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