| 引用本文: | 李 清,沈春林,郭锁凤.控制可重构飞机多变量鲁棒控制器设计[J].控制理论与应用,2000,17(1):133~135.[点击复制] |
| LI Qing,SHEN Chun-lin,GUO Suo-feng.Robust Multivariable Controller Design for the Control Reconfigurable Aircraft[J].Control Theory and Technology,2000,17(1):133~135.[点击复制] |
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| 控制可重构飞机多变量鲁棒控制器设计 |
| Robust Multivariable Controller Design for the Control Reconfigurable Aircraft |
| 摘要点击 1758 全文点击 830 投稿时间：1997-09-08 修订日期：1999-10-14 |
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| DOI编号 10.7641/j.issn.1000-8152.2000.1.033 |
| 2000,17(1):133-135 |
| 中文关键词 故障 飞行控制 鲁棒 自修复系统 |
| 英文关键词 failure flight control robust self repairing system |
| 基金项目 |
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| 中文摘要 |
| 控制可重构飞机要求其基本飞行控制系统对舵面部分缺损故障具有强的鲁棒特性, 在故障发生后保证飞机的稳定性, 提供足够的时间进行故障的检测和隔离, 为控制系统重构提供条件. 本文采用高速采样PI控制器设计输出反馈跟随系统, 给出了控制器的设计方法, 并分析了它对于控制舵面部分缺损故障的鲁棒特性. 仿真结果表明, 这种控制器具有好的鲁棒特性. |
| 英文摘要 |
| The control reconfigurable aircraft with multi surfaces needs robust basic flight control system to support enough time for failure detection and isolation.When partial surface loses,it can keep the damaged aircraft stable.In this paper,multivariable output feedback digital control laws are designed for the Control Reconfigurable Aircraft (CRA).The method uses fast sampling digital PI controllers to design digital flight control tracking system.This paper gives the way to design the controller and analyze its robustness characteristics.The simulation results indicate that the controller is very robust and the output responses are fully satisfactory. |
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