摘要
以某型号导弹为背景,针对天线罩瞄准线误差斜率严重影响制导控制系统稳定性这一关键问题,通过对控制系统的设计,提出了一种解决办法,并通过数学仿真加以验证。
A method based on the guidance and control loop design is presented to solve the problem that the radome slope serious affects the stability of guidance and control system for a certain missile. In order to check the performance of the design,a mathematical simulation is conducted.
出处
《现代防御技术》
2002年第6期27-29,共3页
Modern Defence Technology
