Study on Ballistic Correction Technique of A Rocket Projectile under impulse
Aiming at improving the precision of the homing shells, an impulse control method is studied in this paper, a mathematical model for the ballistic trajectory was established. In order to study the ballistic trajectory characteristics, the simulation is done based the dynamic model. The effect of the value, number, working position and working time of the impulse and the rotate speed of the shell on the correction ability were analyzed. The essentials for the design of impulse control scheme were outlined. The result provides reference for the design of impulse control on homing shells.
ballistic correction impulse control rocket projectile projectile-load detector
LI Chenming
Nanjing College, Artillery Academy of PLA, Nanjing 211132, China
国际会议
北京
英文
2007-08-05（万方平台首次上网日期，不代表论文的发表时间）