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导弹控制系统的容错控制研究
引用本文:刘湘崇, 梁彦, 程咏梅, 潘泉, 张洪才.导弹控制系统的容错控制研究[J].控制与决策,2006,21(10):1185-1189.
作者姓名:刘湘崇  梁彦  程咏梅  潘泉  张洪才
作者单位:西北工业大学,自动化学院,西安,710072
基金项目:国家自然科学基金项目(60404011,60372085).
摘    要:为了提高导弹姿态控制系统的可靠性,防止由于传感器失效而引起导弹自毁,提出基于信号重构的容错控制方法.为了对姿态控制系统中的传感器进行信号重构,首先考虑弹体弹性振动的影响,分析了弹体弹性振动与姿态角之间的关系;然后分析了传感器输出信号之间的关系;最后,通过解析冗余方法,用正常工作的传感器输出信号重构出现故障的传感器的正常信号.仿真实验表明了该方法的有效性.

关 键 词:弹性振动  容错控制  惯性传感器  振型斜率
文章编号:1001-0920(2006)10-1185-05
收稿时间:2005-07-21
修稿时间:2005-09-26

On Fault-tolerant Control of Missile Control Systems
LIU Xiang-chong,LIANG Yan,CHENG Yong-mei,PAN Quan,ZHANG Hong-cai.On Fault-tolerant Control of Missile Control Systems[J].Control and Decision,2006,21(10):1185-1189.
Authors:LIU Xiang-chong  LIANG Yan  CHENG Yong-mei  PAN Quan  ZHANG Hong-cai
Abstract:To enhance the reliability of missile attitude control systems and prevent the self-destruction caused by failed inertia sensors, an approach of fault-tolerant control based on signal reconfiguration is proposed. To reconfigure signals of the sensors in the missile attitude control system, the impact of elastic oscillation of the missile body is considered, and the relationship between the elastic oscillation of the missile body and the attitude angles is analyzed. The relationship among the sensors is also analyzed. The normal signal of a failed sensor is reconfigured with other normally working sensors via analytical redundancy. The simulation result shows the effectiveness of the approach.
Keywords:Elastic oscillation  Fault-tolerant control  Inertia sensor  Oscillation mode slope
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