摘要
文中将比例导引运用到了天基动能拦截器的末制导中,并利用轨控发动机对拦截器的质心运动进行调节,建立了末制导段拦截器和目标的相对运动模型,简单介绍了轨控发动机模型。用真比例导引TPN和实际真比例导引RTPN对目标不机动和机动两种情况进行了数字仿真,并给出了仿真结果及分析。
in this paper,proportional guidance is used in the terminal guidance of kinetic energy interceptor on space, and the trajectory control thrusters are utilized to adjust the center of mass of interceptor motion.The relative motion model between interceptor and target are founded at the terminal guidance phase,and the model of trajectory thrusters are produced in brief.At the same time,using true proportional navigation TPN and real true proportional navigation RTPN,the simulation is developed to the target m...
出处
《弹箭与制导学报》
CSCD
北大核心
2006年第S1期185-188,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
比例导引
空间拦截器
末制导
轨控发动机
proportional guidance
space interceptor
terminal guidance
trajectory control thruster
