The Effect of Thrust Eccentric and Erection Cylinder Anchor Position on the Initial Disturbances

Abstract

A certain type of vehicle missile launch system is selected as the research object in this paper. The dynamic model is established on the base of reasonable hypothesis and simplification and by using of PRO / E software. In this paper, we find out the most dangerous thrust eccentric position of the missile and a better anchor position between the erection cylinder and the landing gear by using ADAMS software simulation of different conditions. The research is to provide a reference for the design of relevant weapons systems.