| 带有质心运动的挠性空间飞行器运动方程 |
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| 引用本文： | 郭兆曾,胡顺菊,朱广田.带有质心运动的挠性空间飞行器运动方程[J].系统科学与数学,1985,5(1):001-009. |
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| 作者姓名： | 郭兆曾 胡顺菊 朱广田 |
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| 作者单位： | 北京控制工程研究所，南开大学计算机与系统科学系，中国科学院系统科学研究所 天津，北京 |
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| 摘 要： | 一、引言随着空间事业的不断发展,空间飞行器的种类不断增多,其动力学结构也越来越复杂.其中绝大部分飞行器既不是单一的刚体,也不是单一的弹性体,而是既有弹性体又有刚体组成的混合体.带有大型太阳帆板的卫星就是其中的一个典型例子.
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THE DYNAMIC EQUATION OF A FLEXIBLE SPACECRAFT WITH MOVING MASS CENTRE |
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| GUO ZHAOZENG,HU SHUNJU,ZHU GUANGTIAN.THE DYNAMIC EQUATION OF A FLEXIBLE SPACECRAFT WITH MOVING MASS CENTRE[J].Journal of Systems Science and Mathematical Sciences,1985,5(1):001-009. |
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| Authors: | GUO ZHAOZENG HU SHUNJU ZHU GUANGTIAN |
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| Institution: | Beijing Institute of Control Engineering;Department of Computer and System Science,Nankai University,Tianjin;Institute of Systems Science,Academia Sinica |
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| Abstract: | In this paper a dynamic equation for a kind of flexible spacecraft is established,which involves flexible vibration of large dimensional solar arrays,motion of the spa-cecraft body and movement of the mass centre.The existence and uniqueness theoremof this equation is proved by means of semi-group theory. |
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