DocumentCode :
3438422
Title :
Notice of Retraction
Research on heading sensitive drift storage behavior of inertial platform system under the influence of temperature
Author :
Xiaokai Huang ; Yunxia Chen ; Rui Kang
Author_Institution :
Sch. of Reliability & Syst. Eng., Beihang Univ., Beijing, China
fYear :
2013
fDate :
15-18 July 2013
Firstpage :
878
Lastpage :
884
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.

For the missile inertial platform system with the characteristic of long-term storage and onetime use, temperature is a key factor that affects the long-term storage behavior of the heading sensitive drift, which is a major parameter of the missile inertial platform system. Based on the gyro´s movement principle in the coordinate system of inertial platform system, the principle and expression of the heading sensitive drift caused by storage temperature was derived in this paper. Then, the storage characteristics of various drift parameters in the expression under the long-term influence of temperature were thoroughly analyzed, and the storage behavioral model of the heading sensitive drift under the influence of storage temperature was obtained. Finally, the long-term drift feature, the acceleration feature and the storage stability of the heading sensitive drift based on behavioral model was analyzed with the actual storage profile. The results indicate that the heading sensitive drift features no acceleration with the current storage temperature profile, but the influence of long-term temperature is obvious, which provides a basis for reasoned resource allocation for the calibration and maintenance in inertial platform system.
Keywords :
aerospace instrumentation; gyroscopes; inertial systems; missiles; behavioral model; gyros movement principle; heading sensitive drift storage behavior; inertial platform system; inertial platform system calibration; long-term storage behavior; missile inertial platform system; storage temperature; temperature influence; Aerodynamics; Damping; Rotors; Servomotors; Temperature; Temperature sensors; Torque; heading sensitive drift; inertial platform system; storage behavioral; temperature;
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.2013.6625709
Filename :
6625709
Link To Document :
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