DocumentCode :
3435667
Title :
Notice of Retraction
Reliability model of missile with disturbance-dependence
Author :
Yunxia Chen ; Dan Xu ; Jieping Gao ; Rui Kang
Author_Institution :
Sch. of Reliability & Syst. Eng., Beihang Univ., Beijing, China
fYear :
2013
fDate :
15-18 July 2013
Firstpage :
226
Lastpage :
232
Abstract :
Notice of Retraction

After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.

We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.

The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.

In this paper, firstly, considering the mechanism of disturbance factors which have effect on missile´s reliability, three types of correlations is proposed with definitions and descriptions. Then specific reliability model formissile with each type of the correlations is developed. Furthermore, the synthetical reliability model for missile with each type isformulated by synthesizing and modifying these three aforementioned reliability models. Detailed steps of reliability calculationis given. Finally, the correctness and feasibility of the classification of correlation and the reliability model proposed in this paper is verified by taking a missile as a typical case.
Keywords :
correlation methods; missiles; reliability; correlations; disturbance factors; disturbance-dependence; missile; reliability model; Aerodynamics; Automotive components; Correlation; Missiles; Modeling; Reliability theory; correlation; disturbance factors; missile; reliability;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Quality, Reliability, Risk, Maintenance, and Safety Engineering (QR2MSE), 2013 International Conference on
Conference_Location :
Chengdu
Print_ISBN :
978-1-4799-1014-4
Type :
conf
DOI :
10.1109/QR2MSE.2013.6625571
Filename :
6625571
Link To Document :
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