DocumentCode :
2329020
Title :
Design and Reliability Analysis on Tri-redundancy Servo Actuator System
Author :
Zhang, Peng ; Wang, Jing
Author_Institution :
Eng. & Technol. Training Center, Civil Aviation Univ. of China, Tianjin, China
Volume :
2
fYear :
2011
fDate :
28-30 Oct. 2011
Firstpage :
262
Lastpage :
265
Abstract :
Reliability is one of the most important target in airplane designing, the redundancy technology is universally used in servo-actuator system of civil aircraft´s Fly-by-Wire System (FBWS). In order to attain a high reliability, firstly the system structure is designed and redundancy allocation is given, accordingly the redundant management strategy and realization are described in detail. Based on Markov process reliability model is established. Taking fault coverage percentage of the first time and the second into account, reliability of the system is analyzed. The simulation result shows that the system has a high reliability.
Keywords :
Markov processes; actuators; aerospace control; aircraft; reliability; servomechanisms; steering systems; FBWS; Markov process reliability model; airplane design; design analysis; fly-by-wire system; redundant management strategy; reliability analysis; triredundancy servo actuator system; Circuit faults; Monitoring; Redundancy; Sensors; Servomotors; Synchronization; markov model; redundancy; reliability; servo system;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computational Intelligence and Design (ISCID), 2011 Fourth International Symposium on
Conference_Location :
Hangzhou
Print_ISBN :
978-1-4577-1085-8
Type :
conf
DOI :
10.1109/ISCID.2011.168
Filename :
6079788
Link To Document :
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