| 基于线性模型跟随的重构飞行控制律设计 |
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| 引用本文： | 齐晓慧,杨志军.基于线性模型跟随的重构飞行控制律设计[J].军械工程学院学报,2008,20(1):24-26. |
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| 作者姓名： | 齐晓慧 杨志军 |
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| 作者单位： | 齐晓慧（军械工程学院光学与电子工程系,河北,石家庄,050003）;杨志军（军械工程学院光学与电子工程系,河北,石家庄,050003） |
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| 摘 要： | 线性模型跟随控制是一种传统的控制方法，通过对增益的调整，使实际受控系统的输出跟随参考模型的输出，以达到理想的静态、动态特性。将线性模型跟随控制引入自修复飞行控制系统的重构控制中，针对发生舵面故障的飞行控制系统，设计模型跟随控制律，给出仿真实例。结果表明，该方法具有可行性和有效性。
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| 关 键 词： | 线性模型跟随 重构控制 飞行控制律 飞行控制系统 |
| 文章编号： | 1008-2956(2008)01-0024-03 |
| 修稿时间： | 2007年10月26 |
Design of Reconfigurable Flight Control Based on Linear Model Following |
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| QI Xiao-hui,YANG Zhi-jun.Design of Reconfigurable Flight Control Based on Linear Model Following[J].Journal of Ordnance Engineering College,2008,20(1):24-26. |
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| Authors: | QI Xiao-hui YANG Zhi-jun |
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| Institution: | (Department of Optics and Electronics Engineering, Ordnance Engineering College, Shijiazhuang 050003, China) |
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| Abstract: | Linear model following is one of the classical control methods in which a control system is designed so that the output of the system follows the output of a reference model to adjust gain matrices. In this paper the method is introduced to reconfigurable flight control. The control law is designed against actuator faults, and a simulation example is presented to demonstrate the effectiveness and feasibility of the proposed control law. |
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| Keywords: | LMF reconfigurable control flight control law flight control system |
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