| 飞航导弹分层滑动模控制 |
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| 引用本文： | 韦峰,张福恩,顾文锦,姚洪.飞航导弹分层滑动模控制[J].航空学报,1999,20(5):475-477. |
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| 作者姓名： | 韦峰 张福恩 顾文锦 姚洪 |
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| 作者单位： | 1. 哈尔滨工业大学控制工程系, 黑龙江哈尔滨 150001;2. 海军航空工程学院, 山东烟台 264001 |
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| 摘 要： | 对 １ 个二层的非线性模型进行了仿射型化，使块对角结构具有分层仿射型特点，提出了滑动模块对角控制器的设计方法，实现了飞航导弹的非线性控制系统的设计。仿真结果表明，这种设计方法对模型参数变化具有很强的鲁棒性。
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| 关 键 词： | 飞航导弹 控制系统 块对角模型 分层滑动模控制 |
| 文章编号： | 1000-6893(1999)05-0475-03 |
| 收稿时间： | 1998-09-09 |
| 修稿时间： | 1998-09-09 |
LAYERED SLIDING MODEL CONTROL OF THE AERODYNAMIC MISSILE |
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| WEI Feng,ZHANG Fu-en,GU Wen-jing,YAO Hong.LAYERED SLIDING MODEL CONTROL OF THE AERODYNAMIC MISSILE[J].Acta Aeronautica et Astronautica Sinica,1999,20(5):475-477. |
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| Authors: | WEI Feng ZHANG Fu-en GU Wen-jing YAO Hong |
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| Institution: | 1. Department of Automatic Control, Harbin Institute of Technology, Harbin 150001, China;2. Department of Automatic Control, Naval Aerodynamic Engineering Academy, Yantai 264001, China |
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| Abstract: | The model of the areodynamic missile can be described as a block diagonal construction with four layers.After getting an affine form of 1 st and 2 nd layers,an affine form with four layers of the missile is gotten in this paper.By using the form , this paper develops a procedure called sliding model block diagonal controller , which realizes a design of a nonlinear system of a missile. The simulation shows that the procedure has a powerful robustness for the model. |
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| Keywords: | areodynamic missile control system block diagonal layered sliding model control |
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