Multi-target optimization of the dynamic parameters for missile transporter-launchers

An arbitrary-site support-free launching mode is taken by some vehicular missile weapon system. Vibration damping requirements are necessary for both the launching and the transporter-launchers simultaneously. On the basis of response sensitivity analysis for the suspension parameters, nonlinear constraints and weighting multi-target functions are constructed and a multi-target optimization for the responses of some selected important points is completed. It is proved by simulation results that the purpose of multi-target optimization can be accomplished by the proposed method.