中高空超音速有控火箭靶弹的弹道设计
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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.
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.
引文
[1]李晓斌,王英杰,孙晓峰.简易控制火箭靶弹总体设计[J].弹道学报,2010,22(1):41-44.
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[3]沈冠军,冯顺山,曹红松.一种超音速火箭靶弹程序角优化方法研究[J].兵工学报,2015,36(4):644-647.
[4]史震,赵万生,张惠平.超低空靶弹弹道设计[J].战术导弹控制技术,2003,3:6-8.
[5] Pat Buckley. U. S. Navy Aerial Target Systems[C]. 49th Annual NDIA Symposium&Exhibition. Monterey CA,10October 2011.
[6]李晓斌,董敬文.火箭靶弹零升阻力系数辨识[J].固体火箭技术,2010,33(1):5-8.
[7] YAN X D,LYU S,TANG S. Analysis of optimal initialglide conditions for hypersonic glide vehicles[J]. Chinese Journal of Aeronautics,2014,27(2):217-225.
[8]王刚,张驰,吴建业.靶弹平飞高度拓展的设计与实现[J].船舶电子工程,2017(2):38-39.
[9]张艳,单时卓.基于有控方案的超音速火箭靶弹平飞弹道设计[J].战术导弹技术,2014(1):37-41.
[10]杜韩东.单组舵控火箭弹气动布局与控制策略研究[D].太原:中北大学,2011:36-37.
[11]张团.超音速靶标分析与弹道设计[D].太原:中北大学,2009:10-13.
[2] MENTAS M. U. S. Aerial Target Programs[C]//46th annual targets,uavs&range OPERATIONS Symposium. san antonio,Texas. 2008:51-55.
[3]沈冠军,冯顺山,曹红松.一种超音速火箭靶弹程序角优化方法研究[J].兵工学报,2015,36(4):644-647.
[4]史震,赵万生,张惠平.超低空靶弹弹道设计[J].战术导弹控制技术,2003,3:6-8.
[5] Pat Buckley. U. S. Navy Aerial Target Systems[C]. 49th Annual NDIA Symposium&Exhibition. Monterey CA,10October 2011.
[6]李晓斌,董敬文.火箭靶弹零升阻力系数辨识[J].固体火箭技术,2010,33(1):5-8.
[7] YAN X D,LYU S,TANG S. Analysis of optimal initialglide conditions for hypersonic glide vehicles[J]. Chinese Journal of Aeronautics,2014,27(2):217-225.
[8]王刚,张驰,吴建业.靶弹平飞高度拓展的设计与实现[J].船舶电子工程,2017(2):38-39.
[9]张艳,单时卓.基于有控方案的超音速火箭靶弹平飞弹道设计[J].战术导弹技术,2014(1):37-41.
[10]杜韩东.单组舵控火箭弹气动布局与控制策略研究[D].太原:中北大学,2011:36-37.
[11]张团.超音速靶标分析与弹道设计[D].太原:中北大学,2009:10-13.