DocumentCode :
3436439
Title :
Notice of Retraction
Failure modes and effect analysis on the gyroscope of the INS on the spaceflight tracking ship
Author :
Feng Zhang ; Fan Zhang ; Yibin Ren
Author_Institution :
Maritime Tracking & Control Dept., China Satellite, Jiangyin, China
fYear :
2013
fDate :
15-18 July 2013
Firstpage :
388
Lastpage :
390
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, the structure of gyroscope is described, and then reliability analysis and modeling of gyroscope is carried out. Specific to one of the gyroscope failures, the failure tree model is built and analyzed. Finally, the failure type is counted up and the corresponding reason is analyzed.
Keywords :
fault trees; gyroscopes; inertial navigation; space vehicles; FMEA; INS; failure mode and effect analysis; failure tree model; gyroscope failures; gyroscope modeling; gyroscope structure; reliability analysis; spaceflight tracking ship; Gyroscopes; Integrated circuit reliability; Marine vehicles; Reliability engineering; Sealing materials; Wires; failure tree; failure type; gyroscope; 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.2013.6625608
Filename :
6625608
Link To Document :
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