| 太阳同步轨道卫星的太阳帆板驱动规律研究 |
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| 引用本文： | 翟坤.太阳同步轨道卫星的太阳帆板驱动规律研究[J].空间控制技术与应用,2008,34(4):38-41. |
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| 作者姓名： | 翟坤 |
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| 作者单位： | 清华大学航天航空学院,北京,100084 |
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| 摘 要： | 研究一类斜飞斜装特殊的太阳同步轨道卫星。首先确定太阳帆板的开始驱动时刻，并给出地球阴影区的计算方法，然后根据不同情况分析太阳帆板的过程驱动规律，并提出基于MATLAB／Simulink／RTW软件的数值设计方法，最后以某卫星为例，说明太阳帆板驱动规律的设计过程，并得到满足工程需要的结果，验证该设计方法的准确性和可行性。
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| 关 键 词： | 太阳同步轨道 帆板 驱动规律 MATLAB Simulink |
Driving Laws of Sun Synchronous Orbit Satellite's Solar Arrays |
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| ZHAI Kun.Driving Laws of Sun Synchronous Orbit Satellite's Solar Arrays[J].Aerospace Contrd and Application,2008,34(4):38-41. |
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| Authors: | ZHAI Kun |
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| Abstract: | A special sun synchronous orbit satellite which flies slantingly and has a pair of slanting solar arrays is investigated in this paper.First of all,the driving time of solar arrays is determined and an algorithm for calculating the earth's shadow area is derived.Then,the process driving laws of solar arrays are analyzed for different conditions and a numerical design method is obtained through the saftware MATLAB/Simulink/RTW.Finally,the design process of solar array driving laws is shown by taking some sat... |
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| Keywords: | sun synchronous orbit solar array driving law MATLAB Simulink |
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