DocumentCode :
1989252
Title :
An enhancement of integrity algorithm for GPS/SINS tightly coupled system
Author :
Huang, Guorong ; Peng, Xingzhao ; Liu, Huawei ; Jiang, Zhengyong ; Xu, Yayi
Author_Institution :
Air Force Eng. Univ., Xi´´an, China
fYear :
2011
fDate :
16-18 Sept. 2011
Firstpage :
1961
Lastpage :
1964
Abstract :
Integrity is a critical performance for GPS/SINS tightly coupled system, as the failure presented in GPS satellites must be detected and excluded before it contaminates the integrated system. To shorten the failure detection time, an innovation extrapolation method was proposed in this paper, and the algorithm´s failure detection performance in the case of outliers, stair errors, slowing growing errors (SGEs) was simulated, the simulation results show that the proposed algorithm has a great improvement against the traditional innovation test method, especially in detecting SGEs. And the failure exclusion was realized by dint of a series of kalman filters.
Keywords :
Global Positioning System; Kalman filters; extrapolation; GPS satellites; GPS/SINS; Kalman filters; coupled system; failure detection performance; failure detection time; failure exclusion; innovation extrapolation method; integrity algorithm; Extrapolation; Global Positioning System; Kalman filters; Satellites; Silicon compounds; Technological innovation; failure detection; failure exclusion; innovation extrapolation method; integrity; tightly coupled;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electrical and Control Engineering (ICECE), 2011 International Conference on
Conference_Location :
Yichang
Print_ISBN :
978-1-4244-8162-0
Type :
conf
DOI :
10.1109/ICECENG.2011.6057812
Filename :
6057812
Link To Document :
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