摘要
提出了利用无控火箭弹改装成有控火箭靶弹的方案,通过调整发射角、舵偏角和舵面偏转控制时间等参量,仿真得到了满足不同高度和供靶条件的滑翔、准平飞和平飞等多种飞行弹道。通过弹道仿真可知,超音速有控火箭靶弹能实现模拟不同目标的飞行弹道,为防空导弹的试验提供条件。
This paper proposed a scheme for retrofiting uncontrollable rocket into controllable rocket target.Through adjusting the launching angle,rudder yaw-angle and the deflection control time,the simulation gets various of trajectory under different conditions,whichcontainmany altitude and glide,approximate level flight and flat flightfor target-supplying condition.According the calculation result,this paper compared and analyzed target-supplying schemes.By trajectory simulation,supersonic controllable rocket targetcan simulate flight trajectory of the different target,which could provide the conditions to test the antiaircraft missile.
作者
王朋飞
周前进
江多琨
WANG Pengfei;ZHOU Qianjin;JIANG Duokun(Xi’an Aeronautical Polytechnic Institute,Xi’an 710089,China;No.990 State Factory,Hefei 230601,China)
出处
《兵器装备工程学报》
CAS
北大核心
2019年第5期52-55,共4页
Journal of Ordnance Equipment Engineering
关键词
有控火箭靶弹
舵偏角
供靶条件
飞行弹道
弹道仿真
controllable rocket target
rudder yaw-angle
target-supplying condition
flight trajectory
trajectory simulation