DocumentCode
3154352
Title
Application of fault tolerant and federated strong tracking Kalman algorithm in integrated navigation system
Author
Yun-feng, Ma
Author_Institution
Inf. & Control Eng. Coll., Weifang Univ., Weifang, China
fYear
2011
fDate
16-18 April 2011
Firstpage
3946
Lastpage
3949
Abstract
An improved federated strong tracking Kalman filter has been proposed creatively and has been used in loose coupling MSINS/GPS integrated navigation system. Adopting three-layer fault tolerant structure, it can effectively check the errors of data outlier, GPS´s velocity jump and the malfunction of the filter state estimate. When the system fault has been diagnosed, it can be insulated in real time, which can make this system have better ability of tolerant the faults. The simulation results show that this approach can resolve the problem of the correlation of GPS´s position and velocity measurement data, GPS´s velocity jump and the system´s sensitivity to initial values. Thus, the real time character, Robust and the ability of tolerating faults of the system has been improved.
Keywords
Global Positioning System; Kalman filters; correlation methods; inertial navigation; position measurement; velocity measurement; Kalman filter; MSINS/GPS integrated navigation system; federated strong tracking Kalman algorithm; position measurement; three layer fault tolerant structure; velocity measurement; Fault tolerance; Fault tolerant systems; Global Positioning System; Information filters; Kalman filters; Fault Tolerant; Federated Filter; Global Position System(GPS); Integrated Navigation System; Kalman Filter; Strapdown Inertial Navigation System(SINS); Strong Tracking;
fLanguage
English
Publisher
ieee
Conference_Titel
Consumer Electronics, Communications and Networks (CECNet), 2011 International Conference on
Conference_Location
XianNing
Print_ISBN
978-1-61284-458-9
Type
conf
DOI
10.1109/CECNET.2011.5768545
Filename
5768545
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