摘要
确定了末制导炮弹发动机点火时间的范围,分析了发动机点火时间和射角对无控弹道射程的影响,同时分析了发动机点火时间对惯性制导启控点散布的影响.结果表明,在发动机点火时间范围内,点火时间对无控弹道射程和惯性制导启控点散布影响不大.
In this paper, the allowed range of rocket ignition time of TGP is determined. The effect of rocket ignition time and elevation angle on uncontrolled trajectory range is analyzed, and the effect of rocket ignition time on the dispersion of the starting position of guidance is analyzed. Results show that the rocket ignition time has little effect on uncontrolled trajectory and the dispersion of the starting position of guidance in the range of the rocket ignition time.
出处
《弹道学报》
CSCD
北大核心
2005年第1期88-92,共5页
Journal of Ballistics
关键词
末制导炮弹
发动机点火时间
射程
散布
terminal guided projectile, rocket ignition time, range, dispersion
