| 制导航弹飞行力学中的坐标系研究 |
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| 引用本文： | 于英杰,张运,刘藻珍.制导航弹飞行力学中的坐标系研究[J].兵工学报,2002,23(2):201-204. |
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| 作者姓名： | 于英杰 张运 刘藻珍 |
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| 作者单位： | 北京理工大学机电工程学院,北京,100081 |
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| 摘 要： | 参考坐标系是导弹飞行力学研究的基础.本文针对某型制导航弹的特点建立了斜置坐标系,并且给出了斜置坐标系之间以及斜置坐标系与常规坐标系之间的转化关系.对于在斜置坐标系中建立的制导航弹的运动方程组的研究结果表明了该坐标系在导弹飞行力学研究中的突出优点.
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| 关 键 词： | 制导航弹 飞行力学 参考坐标系 |
COORDINATE SYSTEMS FOR USE ON GUIDED BOMB'S DYNAMICS OF FLIGHT |
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| Yu Yingjie,Zhang Yun,Liu Zaozhen.COORDINATE SYSTEMS FOR USE ON GUIDED BOMB''S DYNAMICS OF FLIGHT[J].Acta Armamentarii,2002,23(2):201-204. |
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| Authors: | Yu Yingjie Zhang Yun Liu Zaozhen |
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| Abstract: | Reference coordinate system is the basis of research on the dynamics of flight for missiles. Considering the characteristics of a guided bomb, the paper establishes a series of sideling coordinate systems. The transformation relation between sideling coordinate systems and the transformation relation between the sideling coordinate system and groovy coordinate system are given. The simulation results of research on the equations of motion of guided bomb established in sideling coordinate system show the advantages of the sideling coordinate system. |
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| Keywords: | guided bomb dynamics of flight reference coordinate system |
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