计算机科学 ›› 2019, Vol. 46 ›› Issue (6A): 585-588.

• 综合、交叉与应用 • 上一篇    下一篇

一种巡航导弹动力学仿真通用类库的研究与设计

赵鑫业1, 杨光1, 王义涛1, 王栋2   

  1. 海军大连舰艇学院 辽宁 大连1160181;
    海军航空大学 山东 烟台2640012
  • 出版日期:2019-06-14 发布日期:2019-07-02
  • 通讯作者: 赵鑫业(1984-),男,博士,讲师,主要研究方向为作战仿真、作战软件,E-mail:zhaoxinye@nudt.edu.cn
  • 作者简介:杨 光(1986-),男,硕士,助理研究员,主要研究方向为武器系统与运用工程;王义涛(1973-),男,博士,副研究员,主要研究方向为作战软件设计;王 栋(1986-),男,硕士,讲师,主要研究方向为导弹总体设计与分析。
  • 基金资助:
    本文受中国博士后科学基金项目(2016M602962,2017T100797)资助。

Research and Design of General Class Library for Cruise Missile Dynamic Simulation

ZHAO Xin-ye1, YANG Guang1, WANG Yi-tao1, WANG Dong2   

  1. DALIAN Naval Academy,Dalian,Liaoning 116018,China1;
    Naval Aeronautical University,Yantai,Shandong 264001,China2
  • Online:2019-06-14 Published:2019-07-02

摘要: 针对巡航导弹动力学仿真的任务要求,对巡航导弹作战流程和飞行弹道工作展开了深入研究,并设计开发了新一代具有跨平台、通用性、可灵活配置及高可扩展特性等特点的巡航导弹动力学仿真通用类库。以YJ系列某型导弹岸基发射攻击水面舰艇为背景,使用类库对其进行优化计算,并对其轨迹和弹道参数做出分析。结果表明,该型巡航导弹的轨迹仿真可达到良好的效果。通用类库既可以应用于各类巡航导弹的动力学仿真,也可以作为导弹制导系统的重要子系统,完成对制导算法的验证等工作。

关键词: 飞行仿真, 航迹仿真, 通用类库, 巡航导弹

Abstract: Aiming at the mission requirements of cruise missile dynamic simulation,this paper studied the missile combat process and flight trajectory,and designed and developed a new generation of cruise misscile dynamic simulation with characteristics of cross-platform,versatility,flexible configuration and high scalability.Based on missile-based surface-launched attack surface ships of the YJ series,the class library is used to optimize the calculation,and its trajectory and trajectory parameters are analyzed.The results show that the trajectory simulation of this cruise missile can achieve good results.The general class library can be applied to all kinds of cruise missile dynamics simulation,also can be used as an important subsystem of the missile guidance system to complete the guidance algorithm verification and so on.

Key words: Cruise missile, Flight simulation, General class library, Trajectory simulation

中图分类号: 

  • TP391.9
[1]Wikipedia.Cruise missile [EB/OL].http:// https://en.wikipedia.org/wiki/Cruise_missile,2016-10-23.
[2]关世义.飞航导弹仿真技术若干问题的探讨[J].战术导弹技术,1991(1):42-46.
[3]CLARK T,JONES R.Organizational Interoperability Maturity Model for C2[C]∥Proceedings of the 4th Command and Control Research and Technology Symposium.Rhode Island,USA:US Naval WarCollege,1999.
[4]姚雯,陈小前,郭忠全.面向 MDO 的战略导弹动力学仿真通用类库的设计与实现[J].导弹与航天运载技术,2007(5):29-32.
[5]姜光焱,张伟,段昶.基于Vega Prime的导弹仿真系统的研究[J].系统仿真学报,2013,25(4):645-649.
[6]ELTOHAMY K G,KUO C Y.Analysis of Nonlinear Missile Guidance Systems Through Linear Adjoint Method[J].Smart Science,2015,3(4):170-175.
[7]CHOMACHAR S A A,FARD A M.Flight control system for guided rolling-airframe missile[C]∥2016 IEEE Aerospace Conference.IEEE,2016:1-9.
[8]顾浩,康凤举,韩亮,等.典型反舰导弹运动建模与仿真技术[J].系统仿真学报,2016,18(8):2067-2069.
[9]CAVAGLIERI D,BEWLEY T.Low-storage implicit/explicit Runge-Kutta schemes for the simulation of stiff high-dimensional ODE systems[J].Journal of Computational Physics,2015,286:172-193.
[10]STEVENS B L,LEWIS F L,JOHNSON E N.Aircraft Control and Simulation:Dynamics,Controls Design,and Autonomous Systems[M].Hoboken:John Wiley & Sons,2015.
[11]MCDONOUGH K,KOLMANOVSKY I.Integrator resetting for enforcing constraints in aircraft flight control systems[C]∥AIAA Guidance,Navigation,and Control Conference.2015:2015-1995.
[12]FALANGAS E T.Performance Evaluation and Design of Flight Vehicle Control Systems[M].Hoboken:John Wiley & Sons,2015.
[13]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.
[14]MHLANGA F S,PERRY E L,KIRCHNER R.On Adapting a Military Combat Discrete Event Simulation with Big Data and Geospatial Modeling Toward a Predictive Model Ecosystem for Interpersonal Violence[J].Journal of Information Systems Applied Research,2015,8(1):42-55.
[15]ZHAO X,YANG M,XING Z,et al.Structure and content enhancement to Military Scenario Definition Language[C]∥2012 IEEE Symposium on Robotics and Applications(ISRA).2012:379-382.
[16]HUBER D,KALLFASS D.Applying data farming for military operation planning in nato MSG-124 using the interoperation of two simulations of different resolution[C]∥2015 Winter Simulation Conference(WSC).IEEE,2015:2535-2546.
[1] 陈升来,郑爱民,李涛.
基于小波编码的巡航导弹图像压缩方法研究
Study on Compression Algorithm of Cruise Missile Image Based on Wavelet Code
计算机科学, 2009, 36(12): 263-266.
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