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加速度表安装位置对弹道导弹射击精度的影响分析 被引量:1

Influence of Accelerator Eccentricity on Ballistic Missle Firing Accuracy
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摘要 该文建立了在发射点重力惯性坐标系内的视加速度误差模型。在导弹弹体干扰运动和控制装置数学模型的基础上,应用面向对象技术建立了计算机仿真模型,实现了导弹全弹道六自由度仿真,仿真结果得到了实际飞行试验验证。该文得出加速度表安装位置不在质心处影响导弹落点偏差的结论,该结论对于下一步提出误差修正方法奠定了基础,对于提高弹道导弹射击精度具有重要的意义。 Apparent acceleration error models are established in gravity interial coordinate at launching point. Based on the mathematical models of the disturbed movements and the control equipments of the missile body, simulation models are set up by applying object-oriented technology. A six-degree-of-freedom simulation in full trajeeto~ is made, and the simulation results are validated by an actual flight test. The conelusion that the accelerator eccentricity leaves influence on the firing accuracy of ballistic missiles is made, which lays a foundation for the error correction methods in further research and has significance in improving the firing accuracy of ballistic missiles.
出处 《南京理工大学学报》 EI CAS CSCD 北大核心 2006年第4期503-507,共5页 Journal of Nanjing University of Science and Technology
基金 国防试验技术项目
关键词 弹道导弹 加速度表 精度分析 ballistic missiles accelerators accuracy analysis
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参考文献5

  • 1张金槐.远程火箭精度分析与评估[M].长沙:国防科技大学出版社,1995..
  • 2张涛,彭绍雄,聂永芳.基于Simulink的导弹三通道弹道仿真模型[J].航天控制,2002,20(3):66-70. 被引量:2
  • 3Li Hongru,Feng Zhensheng,Li Ke.Object-oriented modeling of flying vehicle[A].ISTM/2001[C].Shanghai,China:International Academic Publishers/Beijing World Publishing Corporation,2001.1289-1292.
  • 4Li Hongru,Feng Zhensheng,Li Ke.Object-oriented simulation of antiaircraft missile[A].ISTM/2003[C].Shenzhen,China:International Academic Publishers/Beijing World Publishing Corporation,2003.2877-2880.
  • 5Dimirovski G M.A simulator for line-of-sight missile control and guidance systems:Object-oriented design[A].Proceedings of Aerospace Conference,2003[C].Montana,USA:IEEE,2003.1680-1686.

二级参考文献2

  • 1[1]张有济主编.战术导弹飞行力学设计.宇航出版社.1995
  • 2[3]马金铎,周绍磊,程继红编著.导弹控制系统原理.航空工业出版社.1996

共引文献14

同被引文献2

  • 1陆元九.惯性器件[M].北京:宇航出版社,1993.
  • 2Theresia C B. Approaches to optimal inertial instrument calibration using slewing[ D]. Cambridge, USA: Dept of Aeronautics and Astronautics, Massachusetts Institute of Technology,2005.11 - 13.

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二级引证文献6

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