DocumentCode :
2668774
Title :
High dynamic GPS/INS integrated navigation fusion algorithm assisted by neural network
Author :
Minhu, Zhang ; Zhang, Ren
Author_Institution :
Sch. of Autom. Sci. & Electr. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing
fYear :
2008
fDate :
16-18 July 2008
Firstpage :
721
Lastpage :
724
Abstract :
The phenomena of the disconvergency of Kalman filter occurs in case of lock-lose or absence in GPS (global positioning system) navigation based on carrier phases in the high dynamic environment. We propose a new method to enhance the performance of GPS/INS (intertial navigation system) integrated navigation system during the GPS signal loss. The method is based on using a ANN (artificial neural netwok) to intelligently aid the GPS/INS integrated navigation system in the absence of GPS signal. The ANN is trained in every filter period during the GPS signal on; When the GPS is off, The output of the previously trained ANN is as the input of the same Kalman filter.The proposed enhanced GPS/INS can be used in the high dynamic environment of a autonomous carrier. A simulation indicates that the method is valid.
Keywords :
Global Positioning System; Kalman filters; navigation; neural nets; GPS signal loss; INS integrated navigation fusion; Kalman filter; artificial neural netwok; autonomous carrier; carrier phases; global positioning system; high dynamic GPS; high dynamic environment; integrated navigation system; intertial navigation system; neural network; Aerodynamics; Artificial neural networks; Automation; Electronic mail; Equations; Global Positioning System; Kalman filters; Navigation; Neural networks; Performance loss; BP neural network; High dynamic; Integrated navigation; Kalman filter;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference, 2008. CCC 2008. 27th Chinese
Conference_Location :
Kunming
Print_ISBN :
978-7-900719-70-6
Electronic_ISBN :
978-7-900719-70-6
Type :
conf
DOI :
10.1109/CHICC.2008.4605661
Filename :
4605661
Link To Document :
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