留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

飞机机翼故障的动态飞行包线估算方法

刘小雄 孙逊 唐强 章卫国

刘小雄, 孙逊, 唐强, 等 . 飞机机翼故障的动态飞行包线估算方法[J]. 北京航空航天大学学报, 2013, 39(11): 1515-1519.
引用本文: 刘小雄, 孙逊, 唐强, 等 . 飞机机翼故障的动态飞行包线估算方法[J]. 北京航空航天大学学报, 2013, 39(11): 1515-1519.
Liu Xiaoxiong, Sun Xun, Tang Qian, et al. Method of dynamic flight envelop assessment for aircraft wing damages[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(11): 1515-1519. (in Chinese)
Citation: Liu Xiaoxiong, Sun Xun, Tang Qian, et al. Method of dynamic flight envelop assessment for aircraft wing damages[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(11): 1515-1519. (in Chinese)

飞机机翼故障的动态飞行包线估算方法

基金项目: 航空科学基金资助项目(20100753009)
详细信息
  • 中图分类号: V249

Method of dynamic flight envelop assessment for aircraft wing damages

  • 摘要: 进行机翼故障情况下的飞行包线估算可为驾驶员正确操纵和包线保护控制提供必要的信息.考虑到飞机机翼故障的动力学特点,提出一种动态飞行包线估算方法.建立故障参数模型,应用最小二乘辨识算法进行气动参数辨识与故障诊断;基于参数辨识结果估算飞行包线;根据故障特点,分别对系统进行配平计算,在每个配平点建立飞行包线数据库,根据故障诊断结果实时调用包线库中的数据,形成当前时刻的飞行包线.

     

  • [1] Bacon B J, Gregory I M.General equations of motion for a damaged asymmetric aircraft[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit.Hilton Head, South Carolina:, 2007:1-13
    [2] Shah G H.Aerodynamic effects and modeling of damage to transport aircraft[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit.Honolulu, Hawai:, 2008:1-13
    [3] Urnes J M, Reichenbach E Y Sr, Smith T A.Dynamic flight envelope assessment and prediction[C]//AIAA Guidance, Navigation and Control Conference and Exhibit.Honolulu, Hawaii:, 2008:1-10
    [4] Tang Liang, Roemer M, Bharadwaj S.An integrated health assessment and fault contingency management system for aircraft[C]//AIAA Guidance, Navigation and Control Conference and Exhibit.Honolulu, Hawaii:, 2008:1-9
    [5] Tang Liang, Roemer M, Ge Jianhua.Methodologies for adaptive flight envelope estimation and protection[C]//AIAA Guidance, Navigation, and Control Conference.Chicago, Illinois:, 2009:1-14
    [6] Goman M G, Khramtsovsky A V, Kolesnikov E N.Evaluation of aircraft performance and maneuverability by computation of attainable equilibrium sets[J].Journal of Guidance, Control, and Dynamics, 2008, 31 (2):329-339
    [7] Pandita R, Chakraborty A, Seiler P.Reachability and region of attraction analysis applied to GTM dynamic flight envelope assessment[C]//AIAA Guidance, Navigation, and Control Conference.Chicago, Illinois:, 2009:1-21
    [8] Keller1 J D, McKillip R M, JrKim S.Aircraft flight envelope determination using upset detection and physical modeling methods[C]//AIAA Guidance, Navigation, and Control Conference.Chicago, Illinois:, 2009, 1-21
    [9] Moncayo H, Perhinschi M G, Davis J.Artificial-immune-system-based aircraft failure evaluation over extended flight envelope[J].Journal of Guidance, Control, and Dynamics, 2011, 34 (4):989-1002
    [10] Morelli E A, Smith M S.Real-time dynamic modeling-data information requirements and flight test results[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit.2008
    [11] 黄成涛, 王立新.多操纵面飞翼构型飞机舵面故障在线诊断方法[J].航空学报, 2011, 32 (1):58-66 Huang Chengtao, Wang Lixin.On-line fault diagnosis for control surface of multi-control effector flying wings[J].Acta Aeronautica et Astronautica Sinica, 2011, 32 (1):58-66 (in Chinese)
    [12] 方振平.飞机飞行动力学[M].北京:北京航空航天大学出版社, 2008:25-45 Fang Zhenping.Aircraft flight dynamic[M].Beijing:Beijing University of Aeronautics and Astronautics Press, 2008:25-45 (in Chinese)
  • 加载中
计量
  • 文章访问数:  948
  • HTML全文浏览量:  7
  • PDF下载量:  568
  • 被引次数: 0
出版历程
  • 收稿日期:  2012-12-24
  • 刊出日期:  2013-11-30

目录

    /

    返回文章
    返回
    常见问答