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.
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