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  1. Four degree of freedom missile motion equation based on proportional navigation method

    2下载量:
  2. Four degree of freedom missile motion equation based on proportional navigation method,The motion equation of 4-DOF missile based on proportional guidance method is given, and the termination conditions are given
  3. 所属分类:其他行业

    • 发布日期:2022-10-19
    • 文件大小:1238
  1. Missile Datcom 2011 GUI

    8下载量:
  2. GUI version of missiledatcom. The aerodynamic parameters, including drag coefficient, lift coefficient and torque coefficient, can be calculated quickly by inputting missile shape parameters.
  3. 所属分类:编译

    • 发布日期:2022-10-19
    • 文件大小:45143987

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