摘要
在末制导段,引入直接力控制,使得基于气动力/直接力复合控制的导弹获得更好的机动能力和响应速度。文中基于广泛应用的比例导引律,对目标机动与导引指令信号进行分析,提出了一种直接力引入时机的设计方法。通过数字仿真,验证了文中提出的设计方法能够有效地解决直接力引入时机问题,且易于工程应用。
In terminal guidance phase, direct force let missile with aerodynamic /reaction-jet controller have better maneuvering ability and response speed. Based on proportional navigation which is popularly used, target maneuver and guidance command is analyzed, and one design method of beginning time of reaction-jet is proposed. The computer simulation results prove that the method is efficient and it will be realized easily.
出处
《弹箭与制导学报》
CSCD
北大核心
2007年第5期11-12,16,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
直接力控制
引入时机
目标机动
导弹
direet force control
beginning time
target maneuvers missile
