摘要
研究了包含一阶动力学滞后的比例导引的解析解,得到并通过仿真验证了脱靶量的解析解表达式,分析了脱靶量与系统参数的关系,得到了脱靶量的大小与初始速度Vm、末制导时间T成正比等结论。
For those simple lag proportional navigation（PN） system, the solution is studied by the way of generalized power progression in this paper and is validated by the simulation. The relation between miss and system parameter is analyzed. It is concluded that the miss is proportional to initial relative velocity V,, and terminal guided time T.
出处
《弹箭与制导学报》
CSCD
北大核心
2007年第5期13-16,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
比例导引
脱靶量
广义幂级数
proportional navigation
miss distance
generalized power series
