• 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