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Measurement Techniques

, Volume 56, Issue 7, pp 753–757 | Cite as

Neuronal Model for Correction of an Astroinertial System

  • A. S. Devyatisil’nyi
  • K. A. Chislov
Article
  • 34 Downloads

A multimodel algorithm based on an expanded interpretation of the Kalman filter algorithm is proposed. The results of a numerical simulation are presented.

Keywords

astroinertial system navigation stars artificial neuron network 

References

  1. 1.
    V. D. Andreev, Theory of Inertial Navigation. Correction Systems [in Russian], Nauka, Moscow (1967).Google Scholar
  2. 3.
    R. E. Kalman, P. L. Falb, and M. A. Arbib, Topics in Mathematical System Theory, McGraw-Hill, NY (1969).MATHGoogle Scholar
  3. 3.
    Yu. S. Osipov and A. V. Kryazhimskii, “Dynamic inversion problems,” Vestn. RAN, 76, No. 7, 615–624 (2006).Google Scholar
  4. 3.
    A. Yu. Ishlinskii, Classical Mechanics and Inertial Forces [in Russian], Nauka, Moscow (1987).Google Scholar

Copyright information

© Springer Science+Business Media New York 2013

Authors and Affiliations

  1. 1.Institute of Automation and Control Processes, Far Eastern BranchRussian Academy of Sciences (IAPU DVO RAN)VladivostokRussia

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