| 光纤陀螺与GPS组合定姿技术在航天器上的应用研究 |
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| 引用本文： | 王海. 光纤陀螺与GPS组合定姿技术在航天器上的应用研究[J]. 中国惯性技术学报, 2004, 12(1): 49-54 |
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| 作者姓名： | 王海 |
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| 作者单位： | 国防科技大学航天学院,湖南,长沙,410073 |
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| 摘 要： | 在重量轻、功耗低和可靠性高等较高技术要求下,采用光纤陀螺与GPS组合定姿定轨技术,作为微小型航天器或舱外机动装置上高精度自主姿态确定系统,文中重点研究了光纤陀螺与GPS组合定姿在航天器定姿中的应用情况。
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| 关 键 词： | 光纤陀螺 姿态确定 航天器控制 数学仿真 |
| 文章编号： | 1005-6734(2004)01-0049-06 |
| 修稿时间： | 2003-12-11 |
Application of Integrated FOG/GPS Attitude Control Technology in Spacecraft |
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| WANG Hai. Application of Integrated FOG/GPS Attitude Control Technology in Spacecraft[J]. Journal of Chinese Inertial Technology, 2004, 12(1): 49-54 |
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| Authors: | WANG Hai |
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| Abstract: | In order to meet the requirements of advanced technology on low weight, low consumed power and high reliability, the integrated FOG/GPS are used as a high precision attitude determination system. In this paper, the application of integrated FOG/GPS system on spacecrafts attitude control is studied. |
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| Keywords: | FOG attitude determination spacecrafts control mathematic modeling |
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