| 引用本文: | 薛文超,黄朝东,黄一.飞行制导控制一体化设计方法综述[J].控制理论与应用,2013,30(12):1511~1522.[点击复制] |
| XUE Wen-chao,HUANG Chao-dong,HUANG Yi.Design methods for the integrated guidance and control system[J].Control Theory and Technology,2013,30(12):1511~1522.[点击复制] |
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| 飞行制导控制一体化设计方法综述 |
| Design methods for the integrated guidance and control system |
| 摘要点击 4713 全文点击 3875 投稿时间：2013-09-18 修订日期：2013-11-04 |
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| DOI编号 10.7641/CTA.2013.30988 |
| 2013,30(12):1511-1522 |
| 中文关键词 制导控制一体化 不确定系统 自抗扰控制 |
| 英文关键词 integrated guidance and control uncertain systems active disturbance rejection control |
| 基金项目 国家数学与交叉科学中心课题资助项目 |
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| 中文摘要 |
| 从系统模型和控制设计方法两个方面综述了飞行器制导控制一体化设计方法的研究现状. 论述了制导控制一体化设计中的关键问题, 即系统具有较高的阶数和系统存在大量不确定性. 提出了基于自抗扰控制的三维制导控制一体化设计方法. 该控制方法具有简明的线性结构, 并且可以对飞行控制系统中的非线性时变不确定性进行实时估计和补偿. 仿真结果表明该方法可以对付大范围的不确定性, 具有很好的鲁棒性. |
| 英文摘要 |
| The design methods for guidance control systems are overviewed from the aspects of modeling and control. Key problems of high system order and high uncertainties are discussed. For a 3-D system, we propose an integrated guidance and control approach with active disturbance rejection control (ADRC). The controller is featured with simple structure and with online estimation and compensation for the nonlinear time-varying uncertainties in the flight control system. Simulation results show the effectiveness of the proposed approach for dealing with large uncertainties in the integrated system. |