Abstract:With the problem of poor suitability between active balancing machine and certain multiple rocket launcher, this paper establishes mathematical model of the launcher’s gravity torque and the balancing machine’s balancing torque, then analyzes and presents feasible optimization scheme, and uses the ISIGHT/ MATLAB integrated optimization strategy to achieve the optimization scheme. The results show that after optimization,the active balancing machine’s efficiency is greatly increased, and the rest of the maximum unbalanced torque of the launcher is reduced by 79. 8%. The integrated optimization strategy provides a new solution for other optimization problems.