基于实际采样的导弹弹道建模与仿真
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摘要
针对作战模拟训练中缺乏合适的导弹弹道仿真方法的问题,分析了常用的导弹6自由度和3自由度仿真模型的局限性,提出一种将导弹运动学模型与历史实测数据相结合的弹道仿真方法,并以带中末制导的空对面弹道导弹为例,详细阐述了模型的构建过程,通过校核、验证和仿真实验,表明该方法可以高可信度仿真"红蓝"双方各种型号的导弹弹道,对作战模拟训练导弹弹道仿真具有重要参考意义。
Aiming at the problem of lacking the proper simulation method for missile trajectory in combat simulation training, this paper analyzes the limitations of the 6D and 3D simulation models, proposes a method of trajectory simulation with missile kinematics model and history measured data, and taking an air-to-surface ballistic missile with midcourse-terminal guidance as an example, describes the model construction process in detail. Through the verification, validation and simulation experiments, it shows that this method can simulate various types of missile trajectory with high confidence on both sides of "red and blue", which has an important reference meaning for missile trajectory simulation in combat simulation training.
Aiming at the problem of lacking the proper simulation method for missile trajectory in combat simulation training, this paper analyzes the limitations of the 6D and 3D simulation models, proposes a method of trajectory simulation with missile kinematics model and history measured data, and taking an air-to-surface ballistic missile with midcourse-terminal guidance as an example, describes the model construction process in detail. Through the verification, validation and simulation experiments, it shows that this method can simulate various types of missile trajectory with high confidence on both sides of "red and blue", which has an important reference meaning for missile trajectory simulation in combat simulation training.
引文
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[7]胡海,刘鼎臣.飞航导弹弹道仿真的校核、验证和确认[J].系统仿真学报,2002,14(3):274-277.Hu Hai,Liu Dingchen.Verification Validation&Accreditation of Aerodynamic Missile Trajectory Simulation.Journal of System Simulation,2002,14(3):274-277.
[2]杨艳明,唐胜景.基于Simulink的子导弹全弹道仿真[J].系统仿真学报,2006,18(6):1442-1444.Yang Yanming,Tang Shengjing.Trajectory Simulation of Submunitions Based on Simulink[J].Journal of System Simulation,2006,18(6):1442-1444.
[3]张安民,崔连虎,赵世明.战术导弹三自由度弹道仿真模型研究[J].系统仿真技术,2016,12(2):88-94.Zhang Anmin,Cui Lianhu,Zhao Shiming.Study of three Degree of Freedom Tactical Missile Simulation Model[J].Journal of System Simulation,2016,12(2):88-94.
[4]胡晓峰.大数据时代对建模仿真的挑战与思考[J].军事运筹与系统工程,2013,27(4):5-12.Hu Xiaofeng.Challenge and Thinking of Modeling and Simulation in Big Data Era[J].Military Operations Research and Systems Engineering,2013,27(4):5-12.
[5]李鹏波,张士峰,蔡洪.远程反舰导弹试验弹道折合直接推算方法[J].战术导弹技术,2000,1(1):30-33.Li Pengbo,Zhang Shifeng,Cai Hong.Direct Calculation Method for Test Ballistic Trajectory of Long Range Anti-ship Missile[J].Tactical Missile Technology,2000,1(1):30-33.
[6]刘万俊,魏贤智,张艺瀚,等.导弹飞行力学[M].西安:西安电子科技大学出版社,2014:117-130.Liu Wanjun,Wei Xianzhi,Zhang Yihan,et al.Missile Flight Mechanics[M].Xi’an:Xidian University Press,2014:117-130.
[7]胡海,刘鼎臣.飞航导弹弹道仿真的校核、验证和确认[J].系统仿真学报,2002,14(3):274-277.Hu Hai,Liu Dingchen.Verification Validation&Accreditation of Aerodynamic Missile Trajectory Simulation.Journal of System Simulation,2002,14(3):274-277.