| 1. | At first , the rolling missile model had been established by referring to the figuration dimension of pac - 3
首先以“爱国者? 3 ”的外形尺寸为参考建立本文的研究工作所需的导弹模型。 |
| 2. | This thesis has done the following research : 1 . the mathematical model of rolling missile was established
具体在本文中，完成了如下工作： 1建立了包含已分解的控制力的火箭弹数学模型。 |
| 3. | The motion model and dynamics model of the rolling missile was constructed , and the thrust performance of attitude control system were presented
建立了滚转导弹运动学和动力学模型，以及姿控发动机的推力模型。 |
| 4. | And we gained satisfying result . the method of this thesis works on other general rolling missile as well as the object of the paper
本文所做的工作不仅适用于火箭弹的简控系统，对于一般旋转导弹的控制系统设计也可作为参考。 |
| 5. | Based on the average mathematical model , the transfer function of the rolling missile was deduced , and the stability conclusion was deduced and applied to the research object
从滚转导弹的均态数学模型出发，推导了滚转导弹的弹体传递函数。分析了滚转导弹的稳定性条件。 |
| 6. | The thesis tracks the research about the intercept technology oversea . 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。 |
| 7. | 2 . 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。 |
