Enviar artigo por via de e-mail Model of an Integrated Inertial-Satellite Navigation System Without Gyroscopes
- Autores: Devyatisil’nyi A.S.1,2, Chislov K.A.1
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Afiliações:
- Institute of Automation and Control Processes, Far Eastern Branch of the Russian Academy of Sciences
- Far Eastern Federal University
- Edição: Volume 59, Nº 2 (2016)
- Páginas: 117-121
- Seção: 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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Resumo
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.
Sobre autores
A. Devyatisil’nyi
Institute of Automation and Control Processes, Far Eastern Branch of the Russian Academy of Sciences; Far Eastern Federal University
Autor responsável pela correspondência
Email: devyatis@iacp.dvo.ru
Rússia, Vladivostok; Vladivostok
K. Chislov
Institute of Automation and Control Processes, Far Eastern Branch of the Russian Academy of Sciences
Email: devyatis@iacp.dvo.ru
Rússia, Vladivostok
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