Fault diagnosis of an intelligent hydraulic pump based on a nonlinear unknown input observer

被引:71
作者
Ma, Zhonghai [1 ]
Wang, Shaoping [1 ]
Shi, Jian [1 ]
Li, Tongyang [1 ]
Wang, Xingjian [1 ]
机构
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100083, Peoples R China
基金
中国国家自然科学基金;
关键词
Fault diagnosis; Hydraulic piston pump; Model-based; Nonlinear unknown input observer (NUIO); Residual error; SYSTEMS; DESIGN;
D O I
10.1016/j.cja.2017.05.004
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Hydraulic piston pumps are commonly used in aircraft. In order to improve the viability of aircraft and energy efficiency, intelligent variable pressure pump systems have been used in aircraft hydraulic systems more and more widely. Efficient fault diagnosis plays an important role in improving the reliability and performance of hydraulic systems. In this paper, a fault diagnosis method of an intelligent hydraulic pump system (IHPS) based on a nonlinear unknown input observer (NUIO) is proposed. Different from factors of a full-order Luenberger-type unknown input observer, nonlinear factors of the IHPS are considered in the NUIO. Firstly, a new type of intelligent pump is presented, the mathematical model of which is established to describe the IHPS. Taking into account the real-time requirements of the IHPS and the special structure of the pump, the mechanism of the intelligent pump and failure modes are analyzed and two typical failure modes are obtained. Furthermore, a NUIO of the IHPS is performed based on the output pressure and swash-plate angle signals. With the residual error signals produced by the NUIO, online intelligent pump failure occurring in real-time can be detected. Lastly, through analysis and simulation, it is confirmed that this diagnostic method could accurately diagnose and isolate those typical failure modes of the nonlinear IHPS. The method proposed in this paper is of great significance in improving the reliability of the IHPS. (C) 2017 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd.
引用
收藏
页码:385 / 394
页数:10
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