| 变结构控制在导弹制导中的应用综述 |
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| 引用本文： | GU Wen-jin,顾文锦,赵红超,杨智勇. 变结构控制在导弹制导中的应用综述[J]. 飞行力学, 2005, 23(1): 1-4 |
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| 作者姓名： | GU Wen-jin 顾文锦 赵红超 杨智勇 |
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| 作者单位： | 海军航空工程学院,自动控制系,山东,烟台,264001 |
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| 摘 要： | 简要介绍了变结构控制理论和导弹制导律，对基于变结构控制的导弹制导律进行了比较详细的研究。重点介绍了各种制导律中滑模面的选择和制导律的设计，并给出了一些仿真结果。研究表明，由于变结构控制的应用．使得制导律具有很强的鲁棒性，比传统的比例导引律有更多的优越性。
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| 关 键 词： | 变结构控制 制导律 滑模面 鲁棒性 |
| 文章编号： | 1002-0853(2005)01-0001-04 |
| 修稿时间： | 2003-12-09 |
Application of Variable Structure Control in Missiles Guidance |
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| GU Wen-jin. Application of Variable Structure Control in Missiles Guidance[J]. Flight Dynamics, 2005, 23(1): 1-4 |
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| Authors: | GU Wen-jin |
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| Abstract: | The theory of variable structure control and guidance laws of missiles is simply introduced. The guidance laws based on variable structure control are researched in detail. The paper emphasizes on the selection of sliding-mode surface and the design of guidance laws in all kinds of guidance laws, and gives some simulation results. Research shows because of the application of variable structure control, the guidance laws have strong robustness and more advantages over the conventional proportional navigation guidance law. Therefore, the variable structure guidance laws have good prospects of application. |
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| Keywords: | variable structure control guidance law sliding-mode surface robustness |
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