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弹道学报  2014 

变射面弹道横向转弯飞行程序的设计与优化

Keywords: 弹道导弹,变射面,横向机动,飞行程序

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Abstract:

为有效提高导弹的突防能力和禁避飞区规避能力,实现小射程能量的有效利用,提出一种变射面横向机动弹道,通过初始离面角使弹道一级偏离传统射面,后面级再变换射面以命中目标。针对该机动弹道变换射面的横向转弯段,建立了横向转弯飞行程序仿真模型,为确定最优初始离面角和转弯飞行程序模型参数,采用混合优化算法对其进行了优化。仿真结果表明,模型能够满足弹道横向机动变换射面转弯要求,优化算法能够实时、快速求得最优初始离面角和最优飞行程序,满足射前诸元准备时间要求,实际应用性强。

References

[1]  高先德.某弹道导弹仿真及其误差源分析[D].西安:西安电子科技大学,2010.
[2]  李瑜,杨志红,崔乃刚.助推-滑翔导弹弹道优化研究[J].宇航学报,2008,29(1):66-71.
[3]  LI Yu,YANG Zhi-hong,CUI Nai-gang.A study of optimal trajectory for boost-glide missile[J].Journal of Astronautics,2008,29(1):66-71.(in Chinese)
[4]  聂川义,郭建国,周军,等.空射弹道导弹助推段弹道设计与优化[J].飞行力学,2012,30(4):357-361.
[5]  NIE Chuan-yi,GUO Jian-guo,ZHOU Jun,et al.Design and optimization of boost phase trajectory for air-launched ballistic missile[J].Flight Dynamics,2012,30(4):357-361.(in Chinese)
[6]  龙乐豪.总体设计[M].北京:中国宇航出版社,2009.
[7]  谢政,李建平,陈挚.非线性最优化理论与方法[M].北京:高等教育出版社,2010.
[8]  XIE Zheng,LI Jian-ping,CHEN Zhi.Nolinear optimization theory and method[M].Beijing:High Education Press,2010.(in Chinese)
[9]  张毅,王顺宏.弹道导弹弹道学[M].长沙:国防科技大学出版社,2005.
[10]  ZHANG Yi,WANG Shun-hong.Missile ballistics[M].Changsha:National University of Defense Technology Press,2005.(in Chinese)
[11]  GAO Xian-de.Trajectory simulation and error sources analysis of some ballistic missile[D].Xi’an:Xi’an Electronic Science and Technology University,2010.(in Chinese)
[12]  高洪月.弹道导弹的弹道设计与仿真[D].哈尔滨:哈尔滨工业大学,2010
[13]  GAO Hong-yue.Trajectory simulation and design of the ballistic missile[D].Harbin:Harbin Institute of Technology,2010.(in Chinese)
[14]  杨希祥,李晓斌,肖飞,等.智能优化算法及其在飞行器优化设计领域的应用综述[J].宇航学报,2009,30(6):2 051-2 061.
[15]  YANG Xi-xiang,LI Xiao-bin,XIAO Fei,et al.Overview of intelligent optimization algorithm and its application in flight vehicles optimization design[J].Journal of Astronautics,2009,30(6):2 051-2 061.(in Chinese)
[16]  PONTANI M,CONWAY B A.Particle swarm optimization applied to space trajectories[J].Journal of Guidance,Control,and Dynamics,2010,33(5):1 429-1 441.
[17]  张飞天.近程弹道导弹弹道优化方法研究[D].哈尔滨:哈尔滨工业大学,2009.
[18]  ZHANG Fei-tian.Trajectory optimization research for short-range multi-task ballistic missile[D].Harbin:Harbin Institute of Technology,2009.(in Chinese)
[19]  SUBBARAO K,SHIPPEY B M.Hybrid genetic algorithm collocation method for trajectory optimization[J].Journal of Guidance,Control,and Dynamics,2009,32(4):1 396-1 403.
[20]  ALSUMAIT J S,SYKULSKI J K,AL-THMAN A K.A hybrid GA-PS-SQP method to solve power system valve-point economic dispatch problems[J].Applied Energy,2010,87(5):1 773-1 781.
[21]  LONG Le-hao.General design[M].Beijing:China Astronautic Publishing House,2009.(in Chinese)
[22]  邓建中,刘之行.计算方法[M].西安:西安交通大学出版社,2000.
[23]  DENG Jian-zhong,LIU Zhi-xing.Computing method[M].Xi’an:Xi’an Jiaotong University Press,2000.(in Chinese)

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