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基于控制分配的一类变体飞行器容错控制

江未来 董朝阳 王通 王青

江未来, 董朝阳, 王通, 等 . 基于控制分配的一类变体飞行器容错控制[J]. 北京航空航天大学学报, 2014, 40(3): 355-359. doi: 10.13700/j.bh.1001-5965.2013.0255
引用本文: 江未来, 董朝阳, 王通, 等 . 基于控制分配的一类变体飞行器容错控制[J]. 北京航空航天大学学报, 2014, 40(3): 355-359. doi: 10.13700/j.bh.1001-5965.2013.0255
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)

基于控制分配的一类变体飞行器容错控制

doi: 10.13700/j.bh.1001-5965.2013.0255
基金项目: 国家自然科学基金资助项目(61273083,61074027);国防预研基金资助项目(9140C48020212HK0101)
详细信息
  • 中图分类号: V249.1

Fault tolerant control based on control allocation for morphing aircraft model

  • 摘要: 针对一类含有执行器故障的新型操纵面变体飞行器的容错控制问题,将控制分配方法和整数规划理论相结合,提出了一种基于控制分配的容错控制方法.首先设计虚拟控制律,使飞行器的状态变量跟踪参考模型.然后通过执行阵列重构将执行器的概率性故障及饱和约束转化为整数规划中的决策变量的约束,进而将控制分配问题转换成一类决策变量概率可变的整数规划问题.为保证解算的有效性及收敛性,运用改进的遗传算法进行求解.仿真结果表明,飞行器在执行器发生故障的情形下,仍具有良好的跟踪性能.

     

  • [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)
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出版历程
  • 收稿日期:  2013-05-13
  • 刊出日期:  2014-03-20

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