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非对称受损飞机多变量模型参考自适应控制

杨凌宇 冷宁 张晶 申功璋

杨凌宇, 冷宁, 张晶, 等 . 非对称受损飞机多变量模型参考自适应控制[J]. 北京航空航天大学学报, 2013, 39(11): 1509-1514.
引用本文: 杨凌宇, 冷宁, 张晶, 等 . 非对称受损飞机多变量模型参考自适应控制[J]. 北京航空航天大学学报, 2013, 39(11): 1509-1514.
Yang Lingyu, Leng Ning, Zhang Jing, et al. Multivariable model reference adaptive control of aircraft with asymmetric damage[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(11): 1509-1514. (in Chinese)
Citation: Yang Lingyu, Leng Ning, Zhang Jing, et al. Multivariable model reference adaptive control of aircraft with asymmetric damage[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(11): 1509-1514. (in Chinese)

非对称受损飞机多变量模型参考自适应控制

基金项目: 国家自然科学基金资助项目(61273099)
详细信息
  • 中图分类号: V249.122

Multivariable model reference adaptive control of aircraft with asymmetric damage

  • 摘要: 针对非对称受损的常规布局飞机,对其自适应控制设计方法与适用条件进行了研究.建立了非对称结构受损飞机的非线性模型,详细讨论了模型的线性化过程以及受损造成的纵、横向间动态耦合项;结合常规布局非对称结构受损飞机的物理特性,对多变量模型参考自适应控制器设计的关键条件:关联矩阵和高频增益矩阵顺序主子式符号的不变性做出了证明,确立了该方法在非对称结构受损飞机上应用的理论可行性;通过仿真验证了MRAC(Model Reference Adaptive Control)方法对非对称结构受损飞机控制的有效性.

     

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    [2] Nguyen.N, Krishnakumar K, Kaneshige J.Dynamics and adaptive control for stability recovery of damaged asymmetric aircraft[R].AIAA-2006-6049, 2006
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    [7] Guo Jiaxing, Tao Gang.A multivariable MRAC scheme applied to the NASA GTM with damage[R].AIAA 2010-8014, 2010
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  • 被引次数: 0
出版历程
  • 收稿日期:  2012-12-16
  • 刊出日期:  2013-11-30

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