中高空超音速有控火箭靶弹的弹道设计  

Trajectory Design of Mid-High Altitude and Supersonic Controllable Rocket Target

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)

机构地区：[1]西安航空职业技术学院,西安710089 [2]国营990厂,合肥230601

出　　处：《兵器装备工程学报》2019年第5期52-55,共4页Journal of Ordnance Equipment Engineering

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.

关 键 词：有控火箭靶弹 舵偏角 供靶条件 飞行弹道 弹道仿真 

分 类 号：TJ013.2[兵器科学与技术—兵器发射理论与技术]