000021289 001__ 21289
000021289 005__ 20170522124347.0
000021289 04107 $$aeng
000021289 046__ $$k2017-05-15
000021289 100__ $$aDziopa, Z.
000021289 24500 $$aTHE DYNAMICS OF THE GUIDE ARRANGEMENT BEING AN ELEMENT OF THE LAUNCHER INSTALLED ON A COMBAT VEHICLE

000021289 24630 $$n23.$$pEngineering Mechanics 2017
000021289 260__ $$bBrno University of Technology, Institute of Solid Mechanics, Mechatronics and Biomechanics, Brno
000021289 506__ $$arestricted
000021289 520__ $$2eng$$aThe 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.

000021289 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000021289 653__ $$aGuides arrangement, Launcher, Operator, Combat vehicle, Missile, Dynamics.

000021289 7112_ $$aEngineering Mechanics 2017$$cSvratka, CZ$$d2017-05-15 / 2017-05-18$$gEM2017
000021289 720__ $$aDziopa, Z.$$iNyckowski, M.
000021289 8560_ $$ffischerc@itam.cas.cz
000021289 8564_ $$s998764$$uhttp://invenio.itam.cas.cz/record/21289/files/0298.pdf$$yOriginal version of the author's contribution in proceedings, page 298, section DYN.
000021289 962__ $$r21225
000021289 980__ $$aPAPER