Email this article Model of an Integrated Inertial-Satellite Navigation System Without Gyroscopes
- Authors: Devyatisil’nyi A.S.1,2, Chislov K.A.1
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Affiliations:
- Institute of Automation and Control Processes, Far Eastern Branch of the Russian Academy of Sciences
- Far Eastern Federal University
- Issue: Vol 59, No 2 (2016)
- Pages: 117-121
- Section: Article
- URL: https://journals.rcsi.science/0543-1972/article/view/245733
- DOI: https://doi.org/10.1007/s11018-016-0927-z
- ID: 245733
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Abstract
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.
About the authors
A. S. Devyatisil’nyi
Institute of Automation and Control Processes, Far Eastern Branch of the Russian Academy of Sciences; Far Eastern Federal University
Author for correspondence.
Email: devyatis@iacp.dvo.ru
Russian Federation, Vladivostok; Vladivostok
K. A. Chislov
Institute of Automation and Control Processes, Far Eastern Branch of the Russian Academy of Sciences
Email: devyatis@iacp.dvo.ru
Russian Federation, Vladivostok
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