[1]吴振东,王青,董朝阳,等.高超声速飞行器多回路抗饱和鲁棒切换控制[J].哈尔滨工程大学学报,2013,(08):1028-1034.[doi:10.3969/j.issn.10067043.201210079]
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高超声速飞行器多回路抗饱和鲁棒切换控制(/HTML)
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《哈尔滨工程大学学报》[ISSN:1006-6977/CN:61-1281/TN]

卷:
期数:
2013年08期
页码:
1028-1034
栏目:
出版日期:
2013-08-25

文章信息/Info

文章编号:
10067043(2013)08102806
作者:
吴振东1 王青1 董朝阳2 莫华东1
(1.北京航空航天大学 自动化科学与电气工程学院,北京 100191; 2.北京航空航天大学 航空科学与工程学院,北京 100191)
关键词:
高超声速飞行器切换系统鲁棒控制稳定性分析执行器饱和
分类号:
V249
DOI:
10.3969/j.issn.10067043.201210079
文献标志码:
A
摘要:
针对执行机构饱和的高超声速飞行器姿态控制器设计问题,提出一种多回路抗饱和鲁棒切换控制方案.首先针对运动模态在频率上表现出显著的分离特性,将高超声速飞行器的状态变量分回路设计,对受执行机构饱和影响明显的状态设计参考切换系统,从而降低切换系统和控制器参数设计的复杂性;然后将导致执行机构饱和的事件视作切换信号,选定参考切换模型及鲁棒控制器,使得系统输出能够鲁棒地跟踪参考模型的输出,并保证控制输入不达到饱和状态;最后通过多Lyapunov函数和线性矩阵不等式分析了控制器的稳定性.仿真对比结果表明控制方案的有效性,在存在执行机构失效故障和干扰的情况下,系统状态可良好地跟踪参考状态且输入小于执行机构限幅.

参考文献/References:

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备注/Memo

备注/Memo:
基金项目:国家自然科学基金资助项目(60974014, 61273083).
作者简介:吴振东(1987), 男, 博士研究生.
王青(1968), 女, 教授, 博士生导师.
更新日期/Last Update: 2013-10-11