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
An optimization design of small rolling missile controller parameter based on genetic algorithms was developed.
提出了一种基于遗传算法的小型旋转弹控制器参数优化设计方法。
The mechanism of dynamic instability of rolling missile was analyzed by describing the dynamics of rolling missile as a closed loop with dynamic negative feedback.
将滚转导弹动力学系统描述为一个具有动态负反馈的闭环系统，分析了滚转导弹动态失稳的机理。
Considering the difference of the rolling missile and the non-rolling missile, the mechanism of rolling missile control force and the control theory of rolling missile was analyzed rigorously.
考虑到滚转导弹与非滚转导弹的不同，本文仔细分析了滚转导弹控制力的产生机理和滚转导弹的控制原理。
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