| 基于GPS的飞机姿态实时测量实现及误差分析 |
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| 引用本文： | 韦庆洲,罗兆文,朱昱,李智勇,赵文波.基于GPS的飞机姿态实时测量实现及误差分析[J].测绘科学,2010,35(4):20-22. |
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| 作者姓名： | 韦庆洲 罗兆文 朱昱 李智勇 赵文波 |
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| 作者单位： | 军械工程学院,石家庄050003;63883部队,河南洛阳471000;63883部队,河南洛阳,471000 |
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| 摘 要： | 本文阐述了用GPS接收机实时测量飞机姿态的基本思想,建立了数学模型并推导了相关的公式,并构建了基于两台GPS接收机构成的姿态实时测量系统,分析了利用两台独立GPS接收机进行测姿的方法所获结果精度,实验表明该系统有效满足了工程需要,具有一定实用价值。
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| 关 键 词： | GPS 姿态测量 姿态角 |
Realization and error analysis of the real-time aerial attitude-measuring base on GPS |
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| WEI Qing-zhou,LUO Zhao-wen,ZHU Yu,LI Zhi-yong,ZHAO Wen-bo.Realization and error analysis of the real-time aerial attitude-measuring base on GPS[J].Science of Surveying and Mapping,2010,35(4):20-22. |
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| Authors: | WEI Qing-zhou LUO Zhao-wen ZHU Yu LI Zhi-yong ZHAO Wen-bo |
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| Abstract: | This paper described the fundamental principle of measuring real-time airplane attitude with the GPS receiver,built up mathematics model and deduced the related formula.It established the measuring system base on two GPS receivers,verified the final accuracies achieved from the methods using two independent GPS receivers.The test result showed that this system could meet the engineering needs and get something useful. |
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| Keywords: | GPS |
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