Reliability Assessment of Aircraft Power and Actuation System Based on Three-axis Control

被引：0

作者：

Cui, Xiaoyu ^{[1
]}

Wang, Shaoping ^{[1
]}

Li, Qian ^{[1
]}

Shi, Jian ^{[1
]}

机构：

[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing, Peoples R China

来源：

2015 IEEE/ASME INTERNATIONAL CONFERENCE ON ADVANCED INTELLIGENT MECHATRONICS (AIM) | 2015年

关键词：

reliability assessment; power and actuation system; three-axis control; dissimilar redundancy;

D O I：

暂无

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

As a key subsystem in aircraft, electro-hydraulic power and actuation system embodies performance and reliability that is crucial to aircraft safety, maneuverability and flight quality. The substantially increased system redundancy and high volume of dissimilar redundancy further complicate the aircraft electro-hydraulic control and actuation system. This paper presents the reliability model based on three-axis control as well as the reliability assessment method considering the function and performance. Application in several structures of aircraft power and actuation system indicates that the results of proposed method are closer to the actual situation.

引用

页码：382 / 387

页数：6

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