摘要
介绍了比例导引规律及比例导引规律制导控制系统设计,着重讨论了导引头数学建模过程,同时通过仿真计算表明比例导引规律在导弹控制系统设计中的可行性。
This paper introduces the proportional navigation laws and the design of proportional navigation laws for missile control system, it＇s focus on the math modeling Of homing head, the result of the simulation shows that the proportional navigation laws in design of missile control system is effective.
出处
《弹箭与制导学报》
CSCD
北大核心
2007年第5期105-107,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
制导与控制
导引头
比例导引规律
control and guidance
homing head
proportional navigation laws
