Volume 40 Issue 3
Mar.  2014
Turn off MathJax
Article Contents
Jiang Weilai, Dong Chaoyang, Wang Tong, et al. Fault tolerant control based on control allocation for morphing aircraft model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(3): 355-359. doi: 10.13700/j.bh.1001-5965.2013.0255(in Chinese)
Citation: Jiang Weilai, Dong Chaoyang, Wang Tong, et al. Fault tolerant control based on control allocation for morphing aircraft model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(3): 355-359. doi: 10.13700/j.bh.1001-5965.2013.0255(in Chinese)

Fault tolerant control based on control allocation for morphing aircraft model

doi: 10.13700/j.bh.1001-5965.2013.0255
  • Received Date: 13 May 2013
  • Publish Date: 20 Mar 2014
  • To cope with the fault tolerant control problem of innovative control effectors (ICE) morphing aircraft with actuator fault, employing control allocation method and theory of integer programming, a fault tolerant control scheme based on control allocation was proposed. Firstly, virtual control law was designed to assure that the ICE aircraft can track a desired reference model. Afterwards, the probabilistic fault and saturation constraint of actuators were translated into decision variables constraint of integer programming by the reconfiguration of distributed shape-change effector arrays. In this way, the problem of control allocation was considered as a class of integer programming problem with probabilistic decision variables. To ensure availability and convergence, optimized genetic algorithm was used to solve the problem. Simulation results shows that ICE aircraft with actuator fault also has good tracking performance.

     

  • loading
  • [1]
    Raney D L,Montgomery R C,Green L L.Flight control using distributed shape-change effector arrays [C]//41st AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference and Exhibit.Reston.VA,United States:AIAA, 2000:1560-1-1560-12
    [2]
    Davidson J B,Lallman F J,Bundick W T.Real-time adaptive control allocation applied to a high performance aircraft [C]//5th SIAM Conference on Control & Its Applications.United States:NASA Langley Technical Report Server,2001:1211-1229
    [3]
    吴俊,陆宇平,何真.基于微系统阵列的变形翼的控制研究 [J].传感器与微系统,2009,28(2):38-41 Wu Jun,Lu Yuping,He Zhen.Study on control of morphing wings based on microsystems arrays [J].Transducer and Microsystem Technologies,2009,28(2):38-41(in Chinese)
    [4]
    Liu C S,Zhang S J.Novel robust control framework for morphing aircraft [J].Journal of Systems Engineering and Electronics,2013,24(2):281-287
    [5]
    Liu C S,Li C T,He Z.Adaptive control of a morphing aircraft through updating the number of actuators [C]//AIAA Guidance,Navigation,and Control Conference.Reston,VA,United States:AIAA,2012:4446-1-4446-9
    [6]
    Gang T,Chen S H,Fei J T,et al.An adaptive actuator failure compensation scheme for controlling a morphing aircraft model [C]//Proceedings of the 42nd IEEE Conference and Decision and Control.Maui,HI,United States:IEEE,2003,5: 4926-4931
    [7]
    Ataei-Esfahani A,Wang Q.Robust failure compensation for a morphing aircraft model using a probabilistic approach [J].IEEE Transactions on Control Systems Technology,2007, 15(2):324-331
    [8]
    何光宇,周军,呼卫军.基于遗传算法的多执行机构控制分配策略 [J].西北工业大学学报,2010,28(1):23-26 He Guangyu,Zhou Jun,Hu Weijun.A novel control allocation algorithm based on genetic algorithm (GA) and quadratic programming [J].Journal of Northwestem Polytechnical University,2010,28(1):23-26(in Chinese)
    [9]
    Michael A B,David B D.Nonlinear control allocation using piecewise linear functions [J].Journal of Guidance Control and Dynamics,2004,27(6):1017-1027
    [10]
    宁伟华,陈绍顺,王凤山.求解整数规划的混合遗传算法 [J].空军工程大学学报,2004,5(6):80-83 Ning Weihua,Chen Shaoshun,Wang Fengshan.A hybrid genetic algorithm for solving integer programming [J].Journal of Air Force Engineering University:Natural Science Edition,2004, 5(6):80-83(in Chinese)
  • 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

    Article Metrics

    Article views(1164) PDF downloads(619) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return