Stochastic simulation of the automatic control systems of unmanned aircraft using optimal Kalman filter
Сlosed loop continuous and discrete automatic control systems of unmanned aircraft which contain the autopilot, the glider, sensors and Kalman filters in a straight chain are considered. Discrete model of the system and present in graphs simulation results is proposed.
Main Authors: | , , |
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Format: | Article |
Language: | Russian |
Published: |
Educational institution «Belarusian State University of Informatics and Radioelectronics»
2019-06-01
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Series: | Doklady Belorusskogo gosudarstvennogo universiteta informatiki i radioèlektroniki |
Subjects: | |
Online Access: | https://doklady.bsuir.by/jour/article/view/254 |