LoginProceedings Vol. 23 (2017)
ENGINEERING MECHANICS 2017
23rd INTERNATIONAL CONFERENCE
May 15 – 18, 2017, Svratka, Czech Republic
;
May 15 – 18, 2017, Svratka, Czech Republic
Editors: Vladimír Fuis
Copyright © 2017 Brno University of Technology, Faculty of Mechanical Engineering, Institute of Solid Mechanics, Mechatronics and Biomechanics, Brno
ISBN 978-80-214-5497-2 (printed)
ISSN 1805-8248 (printed)
ISSN 1805-8256 (electronic)
ISSN 1805-8248 (printed)
ISSN 1805-8256 (electronic)
list of papers scientific commitee
THE DYNAMICS OF THE GUIDE ARRANGEMENT BEING AN ELEMENT OF THE LAUNCHER INSTALLED ON A COMBAT VEHICLE
Dziopa Z., Nyckowski M.
pages 298 - 301, full text
pages 298 - 301, full text
The guide arrangement is an element of the self-propelled anti-aircraft missile set. The disturbance which is transferred onto the assembly is generated during the motion of the short-range target homing missiles along the guide. The aim of the paper is to discuss how the input generated within the assembly affects the motion of the guide arrangement.
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Text and facts may be copied and used freely, but credit should be given to these Proceedings.
All papers were reviewed by members of the scientific committee.
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