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安徽红星机电科技股份有限公司
纸质出版:2013
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胡松涛. 导电纤维子弹药空中弹道计算与分析[J]. 中北大学学报(自然科学版), 2013,34(4):403-407.
胡松涛. Calculation and Analysis on Air Trajectory of Submunition Made of Conductive Fiber[J]. 2013, 34(4): 403-407.
导电纤维子母弹是一类以电力系统为攻击目标的软杀伤弹药
其导电纤维子弹药常见的外形为圆柱形
不带减速稳定装置
在飞行过程中攻角变化范围较大.当子弹药运动出现不确定或者过大的姿态角时
弹道计算方法中应用的传统的欧拉运动学方程会出现奇异性.为了解决奇异性的问题
运用四元数法建立了弹道计算模型
并将计算结果与实验数据进行了对比.分析了初始弹道倾角
母弹开舱高度
子弹药抛撒速度等因素对子弹药最优飞行时间的影响
同时给出了指定初始条件下子弹药的失效时间.
Submunition made of conductive fiber was a kind of soft kill munition for attacking electrical power infrastructure.The shape of the submunition usually looked like a circular cylinder without any deceleration stabilized device.The angle of attack had a wide range during the flight.When uncertain or excessive attitude angle occurred
conventional Eulerian equations of motion usually applied in ballistic calculation showed singularity.To solve this problem
calculation model of ballistics was established based on quaternion
the calculated results and experimental data were compared.Some influence factors including initial ballistic angle
cabin open height of the carrier and dispersed velocity of submunition are considered.Impact of these factors on optimal time of flight is analyzed.Also
the failure time of submunition is provided in certain initial conditions.
冯顺山,张国伟,何玉彬,等.导电纤维弹关键技术分析[J].弹箭与制导学报,2004,24(1):40-42.Feng Shunshan,Zhang Guowei,He Yubin,et al.KEY technology analysis about conductivity fiberbomb[J].Journal of Projectiles,Rockets,Missile andGuidance,2004,24(1):40-42(in Chinese)
Wang Fang,Feng Shunshan,Wu Wenxuan,et al.Analysis of action mechanism of graphite bombs andreaction method of power system[C].Xi'an:2010 In-ternational Conference on Power System Technology,2010.
徐明友.火箭外弹道学[M].北京:兵器工业出版社,1989.
肖亚伦.飞行器运动方程[M].北京:航空工业出版社,1987.
黄雪樵.克服欧拉方程奇异性的双欧法[J].飞行力学,1994(12):28-37.Huang Xueqiao.The dual euler method for overcom-ing the singularity of euler equation[J].Flight Dy-namics,1994(12):28-37.(in Chinese)
周伟.双欧法在克服伞-弹系统欧拉方程奇异性中的应用[J].航天返回与遥感,2003,24(3):4-8.Zhou Wei.The application of the dua-leuler methodfor overcoming the singularity of euler equation inparachute-missile system[J].Spacecraft Recovery&Remote Sensing,2003,24(3):4-8.(in Chinese)
李臣明,韩子鹏,刘怡昕,等.基于四元数法变换的末敏弹扫描运动研究[J].兵工学报,2009,30(4):389.Li Chenming,Han Zipeng,Liu Yixin,et al.Study onstable scanning of terminal sensing ammunition basedon quaternion amendment[J].Acta Armamentarii,2009,30(4):389.(in Chinese)
周思渊.无伞末敏弹稳态扫描运动模型与计算方法研究[D].南京:南京理工大学,2010.
Fragopoulous D,Innocenti M.Stability considerationsin quaternion attitude control using discontinuous Lya-punov functions[J].Controul Theory Appl.,2004,151(3):253-258.
王鹏,邹晖,陈万春,等.敏捷导弹六自由度动力学建模与仿真[J].飞行力学,2003,23(1):43-46.Wang Peng,Zou Hui,Chen Wanchun,et al.Agilemissile 6-DOF dynamics modeling and simulation[J].Flight Dynamics,2003,23(1):43-46(in Chinese)
徐明友.弹箭飞行动力学[M].北京:国防工业出版社,2003.
刘爱东,黄彬,卢中武.基于四元数的坐标旋转与插值方法研究[J].计算机与现代化,2012(2):44-47.Liu Aidong,Huang Bin,Lu Zhongwu.Research onmethods of coordinate rotation and interpolationbased on quaternion[J].Computer and Moderniza-tion,2012(2):44-47.(in Chinese)
沈仲书,刘亚飞.弹丸空气动力学[M].北京:国防工业出版社,1984.
苗瑞生,居贤铭,吴甲生.导弹空气动力学[M].北京:国防工业出版社,2006.
Holly Moore.MATLAB实用教程[M].高会生,刘童娜,李聪聪,译.北京:电子工业出版社,2011.
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