Model of an Integrated Inertial-Satellite Navigation System Without Gyroscopes


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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.

作者简介

A. Devyatisil’nyi

Institute of Automation and Control Processes, Far Eastern Branch of the Russian Academy of Sciences; Far Eastern Federal University

编辑信件的主要联系方式.
Email: devyatis@iacp.dvo.ru
俄罗斯联邦, Vladivostok; Vladivostok

K. Chislov

Institute of Automation and Control Processes, Far Eastern Branch of the Russian Academy of Sciences

Email: devyatis@iacp.dvo.ru
俄罗斯联邦, Vladivostok

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