Missile guidance law based on extended state observer

Zheng Zhu; Dong Xu; Jingmeng Liu; Yuanqing Xia

doi:10.1109/TIE.2012.2232254

Missile guidance law based on extended state observer

Zheng Zhu, Dong Xu, Jingmeng Liu, Yuanqing Xia

自动化学院

科研成果: 期刊稿件 › 文章 › 同行评审

174 引用（Scopus）

摘要

The problem of missile interception is investigated in this paper. Sliding-mode controllers with finite-time convergence are proposed for the design of guidance laws. In particular, the control design consists of the estimation of the target acceleration by the extended state observer (ESO), and thus, it achieves the decrease of undesired chattering effectively. Also, simulation results are presented to illustrate the effectiveness of the control strategies.

源语言	英语
文章编号	6374675
页（从-至）	5882-5891
页数	10
期刊	IEEE Transactions on Industrial Electronics
卷	60
期	12
DOI	https://doi.org/10.1109/TIE.2012.2232254
出版状态	已出版 - 2013

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Zhu, Z., Xu, D., Liu, J., & Xia, Y. (2013). Missile guidance law based on extended state observer. IEEE Transactions on Industrial Electronics, 60(12), 5882-5891. 文章 6374675. https://doi.org/10.1109/TIE.2012.2232254

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abstract = "The problem of missile interception is investigated in this paper. Sliding-mode controllers with finite-time convergence are proposed for the design of guidance laws. In particular, the control design consists of the estimation of the target acceleration by the extended state observer (ESO), and thus, it achieves the decrease of undesired chattering effectively. Also, simulation results are presented to illustrate the effectiveness of the control strategies.",

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KW - Extended state observer (ESO)

KW - finite-time control

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Missile guidance law based on extended state observer

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