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航天器姿态跟踪有限时间饱和控制

DOI: 10.13195/j.kzyjc.2014.1436, PP. 2004-2008

Keywords: 姿态控制,有限时间稳定,输入饱和,修正罗德里格参数

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Abstract:

针对卫星姿态跟踪系统,在无扰动和有扰动的情况下,利用双曲正切函数和辅助系统设计两个有限时间饱和控制器.双曲正切函数可以严格地保证卫星姿态跟踪系统的控制输入是有界的.通过李雅普诺夫理论可以证明,系统在两个控制器的作用下既是渐近稳定的又是有限时间稳定的,系统可以快速收敛到平衡点.数值仿真进一步表明了所提出的有限时间控制器的有效性.

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