| 对传感器失效具有完整性的运载火箭控制器设计 |
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| 引用本文： | 胡昌华,许化龙,陈新海.对传感器失效具有完整性的运载火箭控制器设计[J].系统工程与电子技术,1996(8). |
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| 作者姓名： | 胡昌华 许化龙 陈新海 |
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| 作者单位： | 西北工业大学航天工程学院８０３室 |
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| 摘 要： | 基于观测器理论和Ｈ００控制，导出了一种对传感器失效具有Ｈ００性能指标的容错控制器设计律，并成功地应用于某运载火箭姿态控制系统传感器失效容错控制中，理论分析和实例设计论证了该方法的正确性和有效性。
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| 关 键 词： | 航天器传感器，失效分析，容错技术，运载火箭 |
A Controller Design Method for Carrier Rocket with Integrity to Sensor Failures |
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| Hu Changhua, Xu Hualong and Chen Xinhai.A Controller Design Method for Carrier Rocket with Integrity to Sensor Failures[J].System Engineering and Electronics,1996(8). |
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| Authors: | Hu Changhua Xu Hualong and Chen Xinhai |
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| Abstract: | This paper. based on observer theory and H00 control. suggests a design procedure for fault-tolerant control. The control system designed by this procedure can simultaneously stabilize the normal system and the system with sensor failure. keep the H00 norm bound of the close-loop system's performance. The authors employ the procedure to design a fault-tolerant control system for the attitude control of certain carrier rocket with possible sensor failure. The theorical analysis and the practical design prove the procedure's validity. |
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| Keywords: | H_(00) control Fault-tolerant control Carrier rocket |
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