摘要
以静不稳定导弹为研究对象,给出了一种三回路过载控制方法。基于最优控制理论,采用三回路过载控制方法对俯仰通道控制系统进行了设计,得出了经典三回路最优控制方案,并对十种可能的三回路控制方案进行了参数摄动30%时的鲁棒性分析和控制效果比较,结果表明经典三回路过载控制能更好的控制静不稳定导弹。
The three loops acceleration control method is put forward taking the static unstable missile as research object. Three loops acceleration control are used to design the pitch./yaw channe based on optical control theory, and the optimal control scheme of classic three loops control scheme is obtained. The com- parison of robust analysis of the controller parameter perturbations 30% are carried out for the ten possi- ble three loops control methods. The results show that the classic three loops acceleration control is better to control the static unstable missile.
出处
《战术导弹技术》
北大核心
2016年第3期89-95,共7页
Tactical Missile Technology
关键词
静不稳定
三回路过载控制
鲁棒分析
static unstable
three loops acceleration control
robust analysis
