GNSS Based Attitude Determination

Musab Ramazan Akaslan, Y. Ozkazanc
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引用次数: 1

Abstract

Attitude determination in aircraft is a critical function both for navigation and flight control. Within the scope of this study, attitude determination by using GNSS position outputs is studied. An attitude determination system consisting of multiple GNSS receivers is designed and tested on the field. The attitude results were calculated by considering the reference lines of different lengths among GNSS receivers and the performance of the attitude computation were evaluated.
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基于GNSS的姿态确定
飞行器姿态确定是飞行器导航和飞行控制的关键功能。在本研究范围内,研究了利用GNSS位置输出确定姿态。设计了由多个GNSS接收机组成的姿态确定系统,并进行了现场测试。考虑GNSS接收机之间不同长度的参考线计算姿态结果,并对姿态计算的性能进行了评价。
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