摘要
根据弹箭外弹道方程生成RAM类弹的实际飞行轨迹,针对不同速度RAM弹类目标类抛物线飞行轨迹特性,从防空高炮提前跟踪角速度方面考虑,给出了防空高炮随动系统无法及时跟踪RAM类弹目标的射击死区。射击死区受RAM类弹目标的飞行速度与航迹捷径影响,高炮容易出现提前方位角跟踪角速度上的射击死区。
Based on the trajectory equation of projectile and rocket,the actual flight trajectory of RAM projectile is generated. Aiming at the characteristics of parabolic flight trajectory of RAM projectile with different velocities,and from advance tracking angular velocity of antiaircraft gun,this paper gave the shooting dead zone of antiaircraft gun servo system and the shooting dead zone that cannot be timely tracking the projectile of RAM. The influence of the flight speed and the short path of RAM projectile on the shooting dead zone and the gun is more prone to advance azimuth tracking angular velocity on the shooting dead zone.
出处
《兵器装备工程学报》
CAS
2017年第7期94-97,共4页
Journal of Ordnance Equipment Engineering
基金
十三五装备预先研究基金项目(30101040204)
上海航天科技创新基金项目
关键词
防空高炮
RAM类弹
提前跟踪角速度
射击死区
antiaircraft gun
the projectile of RAM
advance tracking angular velocity
shooting dead zone