基于OPTIMUS的控制系统参数优化计算

Optimization of Parameters for Control System Based on OPTIMUS

文中以自寻的反坦克导弹为背景,为了减小着靶时的俯仰角,利用多学科优化软件OPTIMUS集成弹道仿真程序,对部分控制系统参数进行了优化设计。结果表明,使用优化后控制系统参数可以明显减小俯仰角,同时满足制导精度的要求。

A kind of homing antitank missile was regarded as the background. In order to decrease the pitch angle when the missile attacks a target, simulation of missile trajectory program was integrated by OPTIMUS, and optimization of parameters for control system was completed with it. The result shows pitch angle is significantly decreased by optimized parameters for control system, and the requirement of guiding precision is satisfied at the same time.