Abstract

This chapter adopts Response Surface Methodology (RSM) combined with dynamic simulation and statistical analysis to deeply investigate the impact of modal matching of the inherent frequencies of key components of the launching system on the disturbances at the launch box opening during firing. Through experimental design, a polynomial fitting response surface model is established between design parameters and response objectives. The ultimate goal is to find the optimal design scheme that minimizes the initial disturbance, thereby achieving effective modal matching between the main components of the launching device. This research aims to provide a theoretical basis for improving firing accuracy and system stability.

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