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Measurement Techniques

, Volume 59, Issue 2, pp 117–121 | Cite as

Model of an Integrated Inertial-Satellite Navigation System Without Gyroscopes

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

A device for determining the angular velocity vector of a moving object as part of an inertial-satellite navigation system without gyroscopes and a system for receiving data from navigation satellites are proposed. A multimodel artificial neural network with a nucleus-free mechanism for adjusting the synaptic coefficients is used to integrate these systems. The results of a numerical simulation are presented.

Keywords

angular velocity inertial-satellite navigation system accelerometer neural network synaptic coefficient 

References

  1. 1.
    A. S. Devyatisil’nyi and K. A. Chislov, “Neuronal inertial-satellite vector gravimetry system,” Izmer. Tekhn., No. 10, 3–8 (2013).Google Scholar
  2. 2.
    V. D. Andreev, Theory of Inertial Navigation. Autonomous Systems, Nauka, Moscow (1966).Google Scholar
  3. 3.
    V. D. Andreev, Theory of Inertial Navigation. Correcting Systems, Nauka, Moscow (1967).Google Scholar
  4. 4.
    R. E. Kalman, P. Falb, and M. Arbib, Topics in Mathematical System Theory [Russian translation], Mir, Moscow (1971).Google Scholar
  5. 5.
    A. S. Devyatisil’nyi and K. A. Chislov, “Integrated inertial-satellite navigation system corrected with observations of a single star,” Izmer. Tekhn., No. 4, 3–5 (2013).Google Scholar
  6. 6.
    N. L. Leskova, “In the country of the Lilliputians,” V Mire Nauki, No. 6, 48–53 (2014).Google Scholar

Copyright information

© Springer Science+Business Media New York 2016

Authors and Affiliations

  1. 1.Institute of Automation and Control ProcessesFar Eastern Branch of the Russian Academy of SciencesVladivostokRussia
  2. 2.Far Eastern Federal UniversityVladivostokRussia

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