| 利用GPS载波相位实时测定动态飞行器姿态 |
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| 引用本文： | 王惠南.利用GPS载波相位实时测定动态飞行器姿态[J].空间科学学报,1998,18(1):69-74. |
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| 作者姓名： | 王惠南 |
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| 作者单位： | 南京航空航天大学自动控制系!210016 |
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| 基金项目： | 国防科工委预研基金，中国航空工业总公司预研基金 |
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| 摘 要： | 本文阐述了利用GPS载波相位信号进行实时飞行器姿态测定的基本思想，建立了整个系统实时确定载体姿态的数学模型；给出了动态整周模糊单差的求解过程，阐明了其物理意义．
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| 关 键 词： | 全球卫星定位系统 载波相位测量 实时姿态测定 单差法 差分GPS |
REAL-TIME KINEMATIC ATTITUDE DETERMINATION OF AIRCRAFT USING GPS CARRIER PHASE |
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| WANG Huinan, HE Feng.REAL-TIME KINEMATIC ATTITUDE DETERMINATION OF AIRCRAFT USING GPS CARRIER PHASE[J].Chinese Journal of Space Science,1998,18(1):69-74. |
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| Authors: | WANG Huinan HE Feng |
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| Abstract: | The paper describes the basic idea of real-time attitude determination using GPS carrier phase and introduces a mathematical model for attitude determination system. The paper presents an effcient method for resolving single difference phase ambiguities and reveals the meanings of the physics by nature. |
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| Keywords: | GPS Carrier phase measurement Real-time attitude determination Single difference DGPS |
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