DocumentCode :
2635812
Title :
Application of evolutionary neural networks in integrated navigation system
Author :
Jian-juan, Lill
Author_Institution :
Dept. of Electr. Eng., Henan Univ. of Technol., Zhengzhou
fYear :
2008
fDate :
10-12 Dec. 2008
Firstpage :
1
Lastpage :
5
Abstract :
Performance of conventional Kalman filter, which is used in integrated navigation system, depends on precise system model and accurate observation data. Inaccuracy system model or truseless observation data will cause low precision of Kalman filter, and even lead to divergence. So a new adaptive Kalman filter based on evolutionary artificial neural networks is used in this system. The algorithm is tested by simulations, and the results indicated that the algorithm proposed in this paper can efficiently overcome the shortcomings of conventional Kalman filter with better accuracy.
Keywords :
adaptive Kalman filters; aerospace computing; evolutionary computation; inertial navigation; neural nets; SINS; adaptive Kalman filter; evolutionary neural network; inertial navigation system; integrated navigation system; Artificial neural networks; Error analysis; Genetic algorithms; Genetic programming; Geography; Inertial navigation; Kalman filters; Neural networks; Silicon compounds; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008. 2nd International Symposium on
Conference_Location :
Shenzhen
Print_ISBN :
978-1-4244-3908-9
Electronic_ISBN :
978-1-4244-2386-6
Type :
conf
DOI :
10.1109/ISSCAA.2008.4776148
Filename :
4776148
Link To Document :
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