Dynamics of the Missile Launch from the Very Short-Range Mobile Firing Unit

In this article, the results of research of dynamical processes during the first stage of a missile launch from very short-range mobile firing unit (MFU) are presented. The determined laws of motion of the system’s components enabled determining characteristic motions that need to be reconstructed b...

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Main Authors: Algimantas Fedaravičius, Karolis Jasas, Rimvydas Gaidys, Kęstutis Pilkauskas
Format: Article
Language:English
Published: Hindawi Limited 2023-01-01
Series:Shock and Vibration
Online Access:http://dx.doi.org/10.1155/2023/3082704
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author Algimantas Fedaravičius
Karolis Jasas
Rimvydas Gaidys
Kęstutis Pilkauskas
author_facet Algimantas Fedaravičius
Karolis Jasas
Rimvydas Gaidys
Kęstutis Pilkauskas
author_sort Algimantas Fedaravičius
collection DOAJ
description In this article, the results of research of dynamical processes during the first stage of a missile launch from very short-range mobile firing unit (MFU) are presented. The determined laws of motion of the system’s components enabled determining characteristic motions that need to be reconstructed by the launcher simulator intended to be developed for personnel training. The half-car approach is applied for modelling the unit which consists of a vehicle and is attached to its missile launcher. The combined system is represented by a lumped-parameter model. The mathematical model is derived by applying the principle of Lagrange differential equations. Motion laws of the components of the system as its response to excitation load generated during missile launch were determined.
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spelling doaj.art-14d03df7484349ed9fd2111092aa54662023-04-09T00:00:03ZengHindawi LimitedShock and Vibration1875-92032023-01-01202310.1155/2023/3082704Dynamics of the Missile Launch from the Very Short-Range Mobile Firing UnitAlgimantas Fedaravičius0Karolis Jasas1Rimvydas Gaidys2Kęstutis Pilkauskas3Kaunas University of TechnologyKaunas University of TechnologyKaunas University of TechnologyKaunas University of TechnologyIn this article, the results of research of dynamical processes during the first stage of a missile launch from very short-range mobile firing unit (MFU) are presented. The determined laws of motion of the system’s components enabled determining characteristic motions that need to be reconstructed by the launcher simulator intended to be developed for personnel training. The half-car approach is applied for modelling the unit which consists of a vehicle and is attached to its missile launcher. The combined system is represented by a lumped-parameter model. The mathematical model is derived by applying the principle of Lagrange differential equations. Motion laws of the components of the system as its response to excitation load generated during missile launch were determined.http://dx.doi.org/10.1155/2023/3082704
spellingShingle Algimantas Fedaravičius
Karolis Jasas
Rimvydas Gaidys
Kęstutis Pilkauskas
Dynamics of the Missile Launch from the Very Short-Range Mobile Firing Unit
Shock and Vibration
title Dynamics of the Missile Launch from the Very Short-Range Mobile Firing Unit
title_full Dynamics of the Missile Launch from the Very Short-Range Mobile Firing Unit
title_fullStr Dynamics of the Missile Launch from the Very Short-Range Mobile Firing Unit
title_full_unstemmed Dynamics of the Missile Launch from the Very Short-Range Mobile Firing Unit
title_short Dynamics of the Missile Launch from the Very Short-Range Mobile Firing Unit
title_sort dynamics of the missile launch from the very short range mobile firing unit
url http://dx.doi.org/10.1155/2023/3082704
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AT karolisjasas dynamicsofthemissilelaunchfromtheveryshortrangemobilefiringunit
AT rimvydasgaidys dynamicsofthemissilelaunchfromtheveryshortrangemobilefiringunit
AT kestutispilkauskas dynamicsofthemissilelaunchfromtheveryshortrangemobilefiringunit