Advanced Search
Volume 39 Issue 2
Feb.  2013
Turn off MathJax
Article Contents
Journal of Beijing University of Aeronautics and Astronautics  > 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)
shu

Dynamic model and flight control method for structure damaged aircraft

  • 1.

    Beijing Aerospace Automatic Control Institute, Beijing 100854, China

  • 2. Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 30 Nov 2011
  • Publish Date: 28 Feb 2013
    Abstract
  • The dynamic model of a structure damaged aircraft was presented, for designing flight control law to ensure flight safety when the aircraft structure damaged partially. After analyzing the dynamic model, the rotational motion of structure damaged aircraft could be decomposed to normal aircraft rotational motion and disturbance motion by structural damage. The control of structure damaged aircraft could be translated to suppress the disturbance motion and uncertainties. A trajectory linearization control method based on extended state observer was proposed to design the robust flight control law. The simulation results indicate that, the flight control system can achieve the decouple control of the aircraft when the right wing lost 15%. And the attitude rate response follows the command well. The control system can endure the uncertainties and disturbance because of structure damage.

     

    • FullText(HTML)
  • loading
    • References(15)
  • [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
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(2114) PDF downloads(755) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return