DocumentCode
1795443
Title
Reliability modeling analysis for hydraulic/electro-hydrostatic dual redundant actuation system
Author
Qian Li ; Shaoping Wang ; Jian Shi ; Xingjian Wang ; Zongxia Jiao
Author_Institution
Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
fYear
2014
fDate
8-10 Aug. 2014
Firstpage
2757
Lastpage
2762
Abstract
To ensure the reliability and safety, hydraulic/electro-hydrostatic dissimilar dual redundant actuation system is widely used in advanced civil aircraft. Considering the change of dynamic performance of hydraulic actuator (HA) and electro-hydrostatic actuator (EHA), this paper establishes performance reliability model based on parameter drift model, and presents the calculation methods of performance reliability. In order to achieve the comprehensive reliability evaluation of the dual redundant actuation system, this paper combines the performance reliability model with function reliability model. The results indicate that the evaluation method based on integrated reliability model can describe reliability index of dynamic system more accurately.
Keywords
actuators; aircraft control; reliability; EHA; HA; civil aircraft; dissimilar dual redundant actuation system; electro-hydrostatic dual redundant actuation system; function reliability model; hydraulic dual redundant actuation system; parameter drift model; performance reliability model; reliability modeling analysis; Analytical models; Atmospheric modeling; Degradation; Pistons; Reliability; Servomotors; Valves;
fLanguage
English
Publisher
ieee
Conference_Titel
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location
Yantai
Print_ISBN
978-1-4799-4700-3
Type
conf
DOI
10.1109/CGNCC.2014.7007601
Filename
7007601
Link To Document