| 飞行制导控制一体化设计方法综述 |
| |
| 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. |
| |
| 作者姓名： | 薛文超 黄朝东 黄一 |
| |
| 作者单位： | 中国科学院数学与系统科学研究院,北京航天长征飞行器研究所,中国科学院数学与系统科学研究院 |
| |
| 基金项目： | 国家数学与交叉科学中心课题资助项目 |
| |
| 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.
|
| 关 键 词： | 制导控制一体化 不确定系统 自抗扰控制 |
| 收稿时间： | 2013/9/18 0:00:00 |
| 修稿时间： | 2013/11/4 0:00:00 |
Design methods for the integrated guidance and control system |
| |
| XUE Wen-chao,HUANG Chao-dong and HUANG Yi.Design methods for the integrated guidance and control system[J].Control Theory & Applications,2013,30(12):1511-1522. |
| |
| Authors: | XUE Wen-chao HUANG Chao-dong and HUANG Yi |
| |
| Affiliation: | Academy of Mathematics and Systems Science, Chinese Academy of Sciences,Beijing Institute of Space Long March Vehicle,Academy of Mathematics and Systems Science, Chinese Academy of Sciences |
| |
| Abstract: | 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. |
| |
| Keywords: | integrated guidance and control uncertain systems active disturbance rejection control |
|
| 点击此处可从《控制理论与应用》浏览原始摘要信息 |
|
点击此处可从《控制理论与应用》下载全文 |
