REAL-TIME KINEMATIC ATTITUDE DETERMINATION OF AIRCRAFT USING GPS CARRIER PHASE
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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.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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Key words:
- GPS /
- Carrier phase measurement /
- Real-time attitude determination /
- Single difference /
- DGPS
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