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Journal of Projectiles, Rockets, Missiles and Guidance >
The Study on Dynamics Characteristics of Missile Launcher with Flexible Support
Received date: 2013-01-22
Online published: 2025-05-26
In order to study the dynamic characteristics of a vehicular missile launcher with flexible support, the fictitious prototype model of the vehicular missile launcher was established in ADAMS by the software of UG and ANSYS. The launcher's natural frequencies and mode shape and the influence rules of altitude angles were obtained by modal analysis in ADAMS. Then the response of the vehicle and the influence of missile's angle and angle velocity for different launching angles during launching were studied by simulation. The results could provide a basis for specifications of launching system and parameter selection.
Key words： missile launcher; modal analysis; launch dynamics; simulation analysis
FAN Zhanjun , ZHANG Gaofeng , JIANG Denglin . The Study on Dynamics Characteristics of Missile Launcher with Flexible Support[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013 , 33(5) : 173 -176,180 . DOI: 10.15892/j.cnki.djzdxb.2013.05.044
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