| 摆动扫描地球敏感器数学模型及飞行试验结果 |
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| 引用本文： | 孙宝祥,赵健翔,李宝绶. 摆动扫描地球敏感器数学模型及飞行试验结果[J]. 航天控制, 2000, 18(2): 40-45 |
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| 作者姓名： | 孙宝祥 赵健翔 李宝绶 |
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| 作者单位： | 北京控制工程研究所!北京100080 |
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| 摘 要： | 描述了东方红三号卫星(DFH-3)控制系统设计和数学仿真中采用的摆动扫描地球敏感器IRES-01的数学模型,东方红三号卫星近三年飞行试验结果与数学仿真结果基本一致,证明数学模型是正确的。
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| 关 键 词： | 地球敏感器 数学模型 飞行试验 |
| 修稿时间： | 1999-12-01 |
The Mathematical Model and the Flight Results of the Swing Scanning Earth Sensor |
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| Sun Baoxiang,Zhao Jianxiang,Li Baoshou. The Mathematical Model and the Flight Results of the Swing Scanning Earth Sensor[J]. Aerospace Control, 2000, 18(2): 40-45 |
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| Authors: | Sun Baoxiang Zhao Jianxiang Li Baoshou |
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| Affiliation: | Sun Baoxiang
,Zhao Jianxiang
,Li Baoshou
(Beijing Institute of Control Engineering, Beijing 100080) |
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| Abstract: | The paper describes the mathematical model of the swing scanning earth sensor IRES-01 used in design and mathematical simulation of DFH-3 satellite control system.During 3 years the flight results of DFH-3 Satellite is coincident with the results of the mathematical simulation, showing that the mathematical model is correct. |
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| Keywords: | Earth sensor Mathematical model Flight test |
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