空射型反舰导弹虚拟飞行建模仿真
|
摘要
通过对影响空气动力的参数之间的关系进行推到研究,对空气动力系数进行线性简化处理,根据某型空射反舰导弹可查到的性能参数,采用"黑箱建模"及外推的方法确定其空气动力系数,建立某反舰导弹六自由度的简化动力学模型。通过对导弹发射后的各个飞行阶段进行研究,采用航迹角度的控制方法,建立了各个飞行阶段的飞行弹道模型,实现了导弹攻击目标的全过程飞行弹道,并得到飞行航迹的仿真结果,为虚拟对抗仿真系统中水面舰艇的防空反导提供导弹攻击模型支持。
The relationship between the parameters affecting aerodynamic force was studied, and the aerodynamic coefficient was properly linearly simplified. According to the type of airborne anti-ship missile performance model, the "black box modeling" and extrapolation method was adopted to determine its aerodynamic coefficient, a typical anti-ship missile six degrees of freedom of the simplified dynamic model was established. By studying the flight phases after the missile launch, the flight trajectory model of each flight phase was established by using the control method of the track angle. The whole flight trajectory process of the missile attacking a target was realized and the simulation results of the flight path were obtained, which would provide missile attack model support for air defense and anti-missile of surface ship in virtual countermeasure simulation system.
The relationship between the parameters affecting aerodynamic force was studied, and the aerodynamic coefficient was properly linearly simplified. According to the type of airborne anti-ship missile performance model, the "black box modeling" and extrapolation method was adopted to determine its aerodynamic coefficient, a typical anti-ship missile six degrees of freedom of the simplified dynamic model was established. By studying the flight phases after the missile launch, the flight trajectory model of each flight phase was established by using the control method of the track angle. The whole flight trajectory process of the missile attacking a target was realized and the simulation results of the flight path were obtained, which would provide missile attack model support for air defense and anti-missile of surface ship in virtual countermeasure simulation system.
引文
[1]李新国,方群.有翼导弹飞行动力学[M].西安:西北工业大学出版社,2005.(Li Xinguo,Fang Qun.Following missile flight dynamics[M].Xi'an,China:Northwestern Polytechnical University Press,2005.)
[2]高晓光.航空军用飞行器导论[M].西安:西北工业大学出版社,2002.(Gao Xiaoguang.Introduction to Aviation Military Aircraft[M].Xi'an,China:Northwestern Polytechnical University Press,2002.)
[3]徐敏.飞行器空气动力特性分析与计算方法[M].西安:西北工业大学出版社,2012.(Xu Min.Analysis and calculation method of aerodynamic characteristics of aircraft[M].Xi'an,China:Northwestern Polytechnical University Press,2012.)
[4]曾庆华.无人飞行控制系统实验教程[M].北京:国防工业出版社出版,2011.(Zeng Qinghua.Unmanned flight control system experimental tutorial[M].Beijing,China:Defense Industry Press,2011.)
[5]顾浩,康凤举,韩亮,等.典型反舰导弹运动建模与仿真技术[J].系統仿真学报,2006,18(8):2067-2069.(Gu H,Kang F J,Han L,et al.Typical Anti-vessel Missile’s Motion Modeling and Simulation Technology[J].Journal of System Simulation(S1004-731X),2006,18(8):2067-2069.)
[6]刘剑威,吴传利,徐国亮.反舰导弹典型攻击模式及运动仿真研究[J].指挥控制与仿真,2006,28(5):47-50.(Liu Jianwei,Wu Chuanli,Xu Guoliang.Study on Typical Attack Pattern and Motion Simulation of Anti-ship Missile[J].Control&Simulation(S1673-3819),2006,28(5):47-50.)
[7]史高建.导弹弹道设计及其3D实时仿真[D].哈尔滨:哈尔滨工业大学,2015.(Shi Gaojian.Missile Trajectory Design and 3D Real-time Simulation[D].Harbin,China:Harbin Institute of Technology,2015.)
[8]张刚,王文双,张东兴,等.反舰导弹末制导律三维仿真技术研究[J].制导与引信,2012,33(1):6-11.(Zhang Gang,Wang Wenshuang,Zhang Dongxing,et al.Study on 3D Simulation Technology of Terminal Guidance Law for Anti-ship Missile[J].Guidance and Fuze(S1671-0576),2012,33(1):6-11.)
[2]高晓光.航空军用飞行器导论[M].西安:西北工业大学出版社,2002.(Gao Xiaoguang.Introduction to Aviation Military Aircraft[M].Xi'an,China:Northwestern Polytechnical University Press,2002.)
[3]徐敏.飞行器空气动力特性分析与计算方法[M].西安:西北工业大学出版社,2012.(Xu Min.Analysis and calculation method of aerodynamic characteristics of aircraft[M].Xi'an,China:Northwestern Polytechnical University Press,2012.)
[4]曾庆华.无人飞行控制系统实验教程[M].北京:国防工业出版社出版,2011.(Zeng Qinghua.Unmanned flight control system experimental tutorial[M].Beijing,China:Defense Industry Press,2011.)
[5]顾浩,康凤举,韩亮,等.典型反舰导弹运动建模与仿真技术[J].系統仿真学报,2006,18(8):2067-2069.(Gu H,Kang F J,Han L,et al.Typical Anti-vessel Missile’s Motion Modeling and Simulation Technology[J].Journal of System Simulation(S1004-731X),2006,18(8):2067-2069.)
[6]刘剑威,吴传利,徐国亮.反舰导弹典型攻击模式及运动仿真研究[J].指挥控制与仿真,2006,28(5):47-50.(Liu Jianwei,Wu Chuanli,Xu Guoliang.Study on Typical Attack Pattern and Motion Simulation of Anti-ship Missile[J].Control&Simulation(S1673-3819),2006,28(5):47-50.)
[7]史高建.导弹弹道设计及其3D实时仿真[D].哈尔滨:哈尔滨工业大学,2015.(Shi Gaojian.Missile Trajectory Design and 3D Real-time Simulation[D].Harbin,China:Harbin Institute of Technology,2015.)
[8]张刚,王文双,张东兴,等.反舰导弹末制导律三维仿真技术研究[J].制导与引信,2012,33(1):6-11.(Zhang Gang,Wang Wenshuang,Zhang Dongxing,et al.Study on 3D Simulation Technology of Terminal Guidance Law for Anti-ship Missile[J].Guidance and Fuze(S1671-0576),2012,33(1):6-11.)