摘要
首先分析空空复合制导交接班的特点以及交接时间点。然后结合具体的制导律,设计一种与不同的中段制导律、末段制导律匹配的空空复合制导交接班方案,实现中段制导和末段制导的平滑过渡,确定交接时间点。最后经理想制导系统仿真,验证了方案的有效性。
Firstly,the characters of air-to-air composite guidance missiles and hand-off time point were analyzed.Then,based on concrete guidance law,a hand-off scheme of air-to-air composite guidance missiles was designed,which matched with different midcourse and terminal guidance law,to ensure smooth transition from midcourse guidance stage to terminal guidance stage,and to get hand-off time point.Finally,according to desirable guidance system simulation,the effectiveness of this designed scheme was validated.
出处
《弹箭与制导学报》
CSCD
北大核心
2012年第1期1-2,6,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
基金
博士基金(10xznk)资助
关键词
复合制导
交接班
制导律
系统仿真
composite guidance
hand-off
guidance law
system simulation
