Computer Engineering and Applications ›› 2010, Vol. 46 ›› Issue (29): 76-79.DOI: 10.3778/j.issn.1002-8331.2010.29.021
• 研发、设计、测试 • Previous Articles Next Articles
XIAO Jia-wei1,XI Qing-biao1,2,LIU Hui-xia2
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肖佳伟1,席庆彪1,2,刘慧霞2
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Abstract: Aiming at resolving the problem of fault detection mistake under the noise environment in aerial vehicle dynamic process,a new-style observer is constructed,which is based on the method of LMI.This observer is applied as residual generator,which uses[H∞]norm to describe the robustness of the residual against external disturbance in fault detecting.The actuator fault can be detected accurately by restraining the noise effect and the solution of the robust observer estate matrices is deduced.A failure aerial vehicle’s longitudinal model is applied in the simulation.The experimental results show that the design of this paper can check out the fault promptly and accurately and suppress noise effectively.
摘要: 针对飞机动态过程中由于噪声干扰造成故障检测误报的问题,构造一种新的基于LMI(Linear Matrix Inequality)的观测器。将此观测器作为残差产生器,利用[H∞]范数来衡量残差对于外界干扰的鲁棒性,通过抑制噪声对残差的影响来实现故障的准确检测,给出了鲁棒观测器各状态矩阵的求解方法。采用某型歼击机发生故障的纵向运动模型进行仿真验证,实验结果证明提出的方法能在噪声环境下及时准确地检测出故障,对噪声干扰具有一定的鲁棒性。
CLC Number:
TP277
XIAO Jia-wei1,XI Qing-biao1,2,LIU Hui-xia2. LMI based H∞ design approach for robust fault observer[J]. Computer Engineering and Applications, 2010, 46(29): 76-79.
肖佳伟1,席庆彪1,2,刘慧霞2. 基于LMI的H∞鲁棒故障观测器的设计[J]. 计算机工程与应用, 2010, 46(29): 76-79.
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URL: http://cea.ceaj.org/EN/10.3778/j.issn.1002-8331.2010.29.021
http://cea.ceaj.org/EN/Y2010/V46/I29/76