摘要
对空空导弹控制系统建立了数学模型,并在此基础上设计了变结构控制律。仿真结果表明,变结构控制鲁棒性强、抗干扰能力好。
Based on the mathematical model of air-to-air missile control system, a variable structure control law is designed. The results of simulation analysis show that variable structure control has high robustness and good capability of anti-jamming.
出处
《航空兵器》
2006年第4期14-17,共4页
Aero Weaponry
关键词
变结构控制
控制系统
空空导弹
variable structure control
control system
air-to-air missile
