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Model of an Integrated Inertial-Satellite Navigation System Without Gyroscopes

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Measurement Techniques Aims and scope

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.

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References

  1. A. S. Devyatisil’nyi and K. A. Chislov, “Neuronal inertial-satellite vector gravimetry system,” Izmer. Tekhn., No. 10, 3–8 (2013).

  2. V. D. Andreev, Theory of Inertial Navigation. Autonomous Systems, Nauka, Moscow (1966).

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  4. R. E. Kalman, P. Falb, and M. Arbib, Topics in Mathematical System Theory [Russian translation], Mir, Moscow (1971).

  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).

  6. N. L. Leskova, “In the country of the Lilliputians,” V Mire Nauki, No. 6, 48–53 (2014).

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Authors and Affiliations

  1. Institute of Automation and Control Processes, Far Eastern Branch of the Russian Academy of Sciences, Vladivostok, Russia

    A. S. Devyatisil’nyi & K. A. Chislov

  2. Far Eastern Federal University, Vladivostok, Russia

    A. S. Devyatisil’nyi

Authors
  1. A. S. Devyatisil’nyi
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  2. K. A. Chislov
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Corresponding author

Correspondence to A. S. Devyatisil’nyi.

Additional information

K. A. Chislov is Deceased.

Translated from Izmeritel’naya Tekhnika, No. 2, pp. 11–14, February, 2016.

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Devyatisil’nyi, A.S., Chislov, K.A. Model of an Integrated Inertial-Satellite Navigation System Without Gyroscopes. Meas Tech 59, 117–121 (2016). https://doi.org/10.1007/s11018-016-0927-z

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  • DOI: https://doi.org/10.1007/s11018-016-0927-z

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