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.

Bibliographic Details
Main Authors: Y. V. Gridnev, A. Y. Rusetski, S. A. Rak
Format: Article
Language:Russian
Published: Educational institution «Belarusian State University of Informatics and Radioelectronics» 2019-06-01
Series:Doklady Belorusskogo gosudarstvennogo universiteta informatiki i radioèlektroniki
Subjects:
Online Access:https://doklady.bsuir.by/jour/article/view/254