• 中国科技核心期刊
  • Scopus收录期刊
  • DOAJ收录期刊
  • JST收录期刊
  • Euro Pub收录期刊
Volume 17 Issue 4
 
Turn off MathJax
Article Contents
Article Navigation >  Journal of Unmanned Undersea Systems  > 2009  >  17(4): 010-15
PAN Guang, WU Wen-hui, MAO Zhao-yong, HUANG Qiao-gao. Key Technologies about Complete Trajectory Simulation for High Altitude Long-range Gliding Torpedo[J]. Journal of Unmanned Undersea Systems, 2009, 17(4): 010-15. doi: 10.11993/j.issn.1673-1948.2009.04.002
Citation: PAN Guang, WU Wen-hui, MAO Zhao-yong, HUANG Qiao-gao. Key Technologies about Complete Trajectory Simulation for High Altitude Long-range Gliding Torpedo[J]. Journal of Unmanned Undersea Systems, 2009, 17(4): 010-15. doi: 10.11993/j.issn.1673-1948.2009.04.002
shu

Key Technologies about Complete Trajectory Simulation for High Altitude Long-range Gliding Torpedo

doi: 10.11993/j.issn.1673-1948.2009.04.002

  • College of Marine Enginerring, Northwestern Polytechnical University, Xi′an 710072,China

  • Received Date: 2009-02-26
  • Rev Recd Date: 2009-03-15
  • Publish Date: 2009-09-05
    Abstract
  • The technology of high altitude long-range gliding torpedo(HALGT) is an integration of high altitude gliding and underwater voyage technologies. The simulation of the complete trajectory of HALGT is an important part and theoretical basis for conceptual design. In this paper, the complete trajectory of a HALGT is divided into several parts according to the leading factors during whole movement, and the main feature is analysed. The technology of trajectory simulation is studied. Modeling and simulation methods are presented on the basis of relative studies. These simulation methods may benefit the research of complete trajectory.

     

    • FullText(HTML)
  • loading
    • References(15)
  • [1]
    张宇文. 鱼雷弹道与弹道设计. 西安：西北工业大学出版社，1999.
    [2]
    薛晓中. U形涡流法计算机弹干扰流场. 弹道学报，1994, 20(2):54-58.
    [3]
    钱翼棱. 空气动力学. 北京：北京航空航天大学出版社，2004.
    [4]
    Singh K P, Newman J C, Baysal O. Dynamic Unstructured Method for Flows Pass Multiple Objects in Relative Motion. AIAA Journal, 1995, 33(4): 641-659.
    [5]
    Saxer A P, Giles M B. Quasi-3-D Non-Reflecting Boundary Condition for the Euler Equations Calculations. Journal of Propulsion and Power, 1993, 9(3): 163-271.
    [6]
    张启南，肖业伦，陈炳永，等. 外挂物与载机分离过程的数值模拟系统. 北京航空航天大学学报，1996, 22(6): 712-716.
    [7]
    管再升，谷良贤. 机载导弹分离过程仿真. 系统仿真学报，2008, 20(12): 3120-3126.
    [8]
    Wang Z J.A Conservative Interface Algorithm for Moving Chimera(overlapped) Grids. International Journal of Computational Fluid Dynamics, 1998, 10(3): 255-265.
    [9]
    李航航，宋笔锋，李育斌. 导弹空中挂飞分离试验仿真研究. 航空计算技术，2006, 36(4): 89-91.
    [10]
    李文强，彭学锋，郑志强. 基于Simulink的无人机六自由度仿真. 系统仿真学报 2007, 19(19): 4604-4606.
    [11]
    杨新，王小虎，申功璋，文传源. 飞机六自由度模型及仿真研究 系统仿真学报，2000, 12(3): 210-213.
    [12]
    卢炽华，郑际嘉. 空投鱼雷倾斜姿态落水冲击研究. 应用力学学报，1997, 14(3): 130-135.
    [13]
    颜开，史淦君，薛晓中，邵大燮. 用Mackey方法计算鱼雷带空泡航行时的入水弹道. 弹道学报，1998, 10(2): 48-50.
    [14]
    Nahon M A.Simplified Dynamics Model for Autonomous Underwater Vehicles. Journal of Ocean Technology, 2006, 1(1): 57-68.
    [15]
    Goheen K R.Modeling Methods for Underwater Robotic Vehicle Dynamics. Journal of Robotic Systems, 1991, 36(3): 295-317.
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article Views(1812) PDF Downloads(622) Cited by()
    Proportional views
    Related
    Service
    Subscribe
    Copyright：陕ICP备09015163号Address:No. 96, Jinye Road, Xi'an, Shaanxi
    Code：710077Tel: 029-88327279QQ: 767358370
    Email: bianjibu705@sohu.com 767358370@qq.com
    Email Alert RSS
    Taobao
    Micro

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return