The rolling missile model with attitude-control-system is established by referring to the figuration dimension of PAC-3.
本文跟踪国外研究，以“爱国者—3”导弹外形尺寸为参考建立了具有姿态控制系统的滚转导弹模型。
参考来源 - 滚转导弹喷流直接力与气动力复合控制研究·2,447,543篇论文数据，部分数据来源于NoteExpress
本文考虑导弹水下发射时的力学环境条件，给出了导弹模型水下点火动响应测试试验原理与实现方法。
In considering the mechanical ambient for missile launching under water, principle and implementation for measuring the dynamic response of missile model under water are give out.
并基于某导弹缩比模型进行了实际测试，取得了导弹模型水下发射时发动机推力以及相应的结构壳体应变量等参数。
Practical tests of launching under water have been carried out based on a missile model, and parameters such as driving force of the engine and the structural strain of the model are obtained.
已经发表的自寻的非滚转导弹拦截问题的数学模型往往是平面模型或空间质点模型。
Presents a space motion model (SMM) of multiple rigid bodies with varying mass for the description of the intercept problem of homing missiles with roll stabilization.
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