Practical Finite-Time Control of Missiles–A Terminal Sliding Mode Approach

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• 英文论文题名：Practical Finite-Time Control of Missiles–A Terminal Sliding Mode Approach
• 论文作者：Mingzhe Hou ; Shitao Wang ; Guangren Duan ; Feng Tan ; Yang Liu
• 英文论文作者：Mingzhe Hou ; Shitao Wang ; Guangren Duan ; Feng Tan ; Yang Liu ; Harbin Institute of Technology
• 年：2017
• 作者机构：Harbin Institute of Technology;
• 英文论文关键词：missile control ; terminal sliding mode ; finite-time ; robust control
• 会议召开时间：2017-07-26
• 会议录名称：第36届中国控制会议论文集（A）
• 英文会议录名称：Proceedings of the 36th Chinese Control Conference（A）
• 语种：英文
• 分类号：TJ765
• 学会代码：KZLL
• 会议名称：第36届中国控制会议
• 会议地点：中国辽宁大连
• 主办单位：中国自动化学会控制理论专业委员会
• 学会名称：中国自动化学会控制理论专业委员会
• 页数：5
• 文件大小：243k
• 原文格式：D
• 会议级别：全国

摘要

This paper investigates the missile attitude control problem. The model used in this paper is with respect to the Euler attitude angles and their derivatives which can be measured and computed easily. A robust practical finite-time control algorithm is proposed based on the terminal sliding mode approach. It is proved that all of the signals in the closed-loop system are bounded and the tracking error can be driven into a given small neighborhood of the origin in the pre-specified time. The simulation results show the effectiveness of the proposed results.
This paper investigates the missile attitude control problem. The model used in this paper is with respect to the Euler attitude angles and their derivatives which can be measured and computed easily. A robust practical finite-time control algorithm is proposed based on the terminal sliding mode approach. It is proved that all of the signals in the closed-loop system are bounded and the tracking error can be driven into a given small neighborhood of the origin in the pre-specified time. The simulation results show the effectiveness of the proposed results.

引文

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