DocumentCode
3436641
Title
Notice of Retraction
Mission reliability assessment of military helicopter based on state
Author
Jun Shen ; Jian Li ; Zongyuan Li ; Yanda Gao ; Yong Yue
Author_Institution
Army Aviation Res. Inst., Beijing, China
fYear
2013
fDate
15-18 July 2013
Firstpage
419
Lastpage
422
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.
According to the typical mission profile of military helicopter, a mission reliability evaluation model is formulated. Firstly, by task decomposition to determine relevant functional units, D-S evidence theory is employed to assess the technical state of the task-related functional units. Then combining with the specific mission profile and technology state assessment results, the reliability of the typical tasks for military helicopter is evaluated. Finally, application of one example shows the effectiveness of the method.
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.
According to the typical mission profile of military helicopter, a mission reliability evaluation model is formulated. Firstly, by task decomposition to determine relevant functional units, D-S evidence theory is employed to assess the technical state of the task-related functional units. Then combining with the specific mission profile and technology state assessment results, the reliability of the typical tasks for military helicopter is evaluated. Finally, application of one example shows the effectiveness of the method.
Keywords
helicopters; inference mechanisms; military vehicles; reliability; D-S evidence theory; military helicopter; mission reliability assessment; mission reliability evaluation model; specific mission profile; task decomposition; task-related functional units; technology state assessment; Availability; Gears; Helicopters; Military aircraft; Reliability theory; Uncertainty; D-S evidence theory; military helicopter; mission reliability assesment; task-related functional units;
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.2013.6625616
Filename
6625616
Link To Document