THE DYNAMICS OF THE GUIDE ARRANGEMENT BEING AN ELEMENT OF THE LAUNCHER INSTALLED ON A COMBAT VEHICLE
Abstract eng: 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.
Contributors:
Publisher:
Brno University of Technology, Institute of Solid Mechanics, Mechatronics and Biomechanics, Brno
Conference Title:
Conference Title:
Engineering Mechanics 2017
Conference Venue:
Svratka, CZ
Conference Dates:
2017-05-15 / 2017-05-18
Rights:
Text je chráněný podle autorského zákona č. 121/2000 Sb.
Record appears in:
Record created 2017-05-22, last modified 2017-05-22
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