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结构受损飞机动力学模型与飞行控制方法

钟友武 倪少波 杨凌宇 申功璋

钟友武, 倪少波, 杨凌宇, 等 . 结构受损飞机动力学模型与飞行控制方法[J]. 北京航空航天大学学报, 2013, 39(2): 154-158.
引用本文: 钟友武, 倪少波, 杨凌宇, 等 . 结构受损飞机动力学模型与飞行控制方法[J]. 北京航空航天大学学报, 2013, 39(2): 154-158.
Zhong Youwu, Ni Shaobo, Yang Lingyu, et al. Dynamic model and flight control method for structure damaged aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(2): 154-158. (in Chinese)
Citation: Zhong Youwu, Ni Shaobo, Yang Lingyu, et al. Dynamic model and flight control method for structure damaged aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(2): 154-158. (in Chinese)

结构受损飞机动力学模型与飞行控制方法

基金项目: 国家自然科学基金资助项目(60804007)
详细信息
  • 中图分类号: V249.1

Dynamic model and flight control method for structure damaged aircraft

  • 摘要: 为实现对结构部分受损飞机的安全控制,建立了其动力学模型,通过分析将结构受损飞机的旋转运动分解为正常飞机旋转运动和由于受损引起的扰动运动,将结构受损飞机的控制转化为对扰动等不确定性因素的抑制问题.提出了一种基于扩张状态观测器的轨迹线性化控制方法进行飞行控制律设计,使系统具有较强的鲁棒性.仿真结果表明:当飞机右侧机翼缺损15%半翼展长时,控制系统能实现结构受损飞机的解耦控制,角速度响应能较好地跟踪指令,有效抑制了结构受损带来的不确定性和扰动.

     

  • [1] Wolff M.Missile strike:a damaged A300 lands with thrust only[J].Flight Safety Australia,2004,8(6):22-24
    [2] Bramesfeld G,Maughmer M,Willits S.Piloting strategies for controlling a transport aircraft after vertical-tail loss [J].Journal of Aircraft,2006,43(1):216-225
    [3] Shah G H.Aerodynamic effects and modeling of damage to transport aircraft .AIAA 2008-6203,2008
    [4] Nguyen N,Krishnakumar K.Hybrid intelligent flight control with adaptive learning parameter estimation [J].Journal of Aerospace Computing, Information, and Communication, 2009,6(2):171-185
    [5] Campbell S F, Nguyen N T, Kaneshige J, et al. Parameter estimation for a hybrid adaptive flight controller[R].AIAA 2009-1803,2009
    [6] Nguyen N, Krishnakumar K, Kaneshige J, et al. Flight dynamics and hybrid adaptive control of damaged aircraft[J].Journal of Guidance, Control, and Dynamics, 2008, 31(3):751-764
    [7] Nguyen N T, Bakhtiari N M.Hybrid adaptive flight control with bounded linear stability analysis[R].AIAA 2007-6422, 2007
    [8] 钟友武.先进布局飞机非线性容错飞行控制方法研究 [D].北京:北京航空航天大学自动化科学与电气工程学院,2010 Zhong Youwu. Research on nonlinear fault-tolerant flight control Approach for the advanced configuration aircraft[D].Beijing:School of Automation Science and Electrical Engineering,Beijing University of Aeronautics and Astronautics,2010(in Chinese)
    [9] Zhu J J. Nonlinear tracking and decoupling by trajectory linearization[R].NASA Marshall Space Flight Center,1998
    [10] Zhu J J, Huizenga A B.A type two trajectory linearization controller for a reusable launch vehicle-a singular perturbation approach[R].AIAA 2004-5184,2004
    [11] Liu Y.Neural adaptive nonlinear tracking using trajectory linearization[D]. Ohio,USA:Ohio University,2007
    [12] 韩京清.自抗扰控制技术 [M].北京:国防工业出版社,2008:197-206 Han Jingqing.Active Disturbance rejection control technique [M].Beijing:National Defence Industry Press,2008:197-206(in Chinese)
    [13] Huang Yi ,Han Jingqing. Analysis and design for the second order nonlinear continuous extended states observer [J].Chinese Science Bulletin,2000,45(21):1938-1944
    [14] Yang Lingyu,Shen Gongzhang.A new optimal control allocation method for aircraft with multiple control effectors[R].AIAA 2007-1052,2007
    [15] Yang Lingyu,Zhong Youwu,Shen Gongzhang. Control allocation and management for aircraft with multiple effectors[C]//Williamson D A.2009 IEEE Aerospace Conference Proceedings.Montana:Institute of Electrical and Electronics Engineers,2009:1-8
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出版历程
  • 收稿日期:  2011-11-30
  • 网络出版日期:  2013-02-28

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