Proceedings Vol. 24 (2018)
ENGINEERING MECHANICS 2018
May 14 – 17, 2018, Svratka, Czech Republic
Copyright © 2018 Institute of Theoretical and Applied Mechanics of the Cech Academy of Sciences, Prague
ISBN 978-80-86246-91-8 (electronic)
ISSN 1805-8248 (printed)
ISSN 1805-8256 (electronic)
list of papers scientific commitee
pages 261 - 264, full text
The paper reports a control algorithm for air-to-ground missile that performs a pre-programmed flight along an ellipse section. The control system of the object flight is based on classical PD controllers. The efficiency of the system that guides the missile onto a ground target was analysed. The paper presents selected results of numerical simulations obtained using Matlab/Simulink package.
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All papers were reviewed by members of the scientific committee.