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A GPS Based Attitude Determination System for a UAV Aided by Low Grade Angular Rate Gyros

机译:基于GPS基于GPS的低级角速率陀螺仪AVAV的姿态确定系统

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The Satellite Navigation and Positioning (SNAP) group at The University of New South Wales has been conducting research into high-precision attitude determination using a multi-antenna single-frequency GPS array, aided by low grade angular rate gyros. The objective of the research is to develop an accurate, reliable attitude sensor solution at an affordable cost which can be implemented on UAVs (Unmanned Airborne Vehicles) developed for geophysical exploration by Newmont Australia. UAVs used by the geophysical exploration industry will be required to fly lower and for significantly longer periods compared to UAVs used for most other applications. Flying at a low height, approximately 30m above ground level, introduces many communications and control challenges, not the least being the need for rapid response to unexpected platform movements. The GPS attitude determination subsystem is important in enabling an external, independent reference to constrain the control inputs to the UAV flight subsystem. Of particular importance is a good understanding of the integrity of the system.
机译:新南威尔士大学的卫星导航和定位(Snap)集团使用多天线单频GPS阵列进行了高精度姿态确定,通过低等级角速率陀螺仪辅助。该研究的目的是以可承受的成本开发一种准确,可靠的态度传感器解决方案,可以在为Newmont澳大利亚的地球物理勘探开发的无人机(无人驾驶机载车辆)上实施。与大多数其他应用的无人机相比,地球物理勘探行业使用的无人机将需要较低,并且在更长的时间内飞行。在低高的高度上飞行,大约30米以上地面,引入了许多通信和控制挑战,并非最不需要快速响应意外的平台运动。 GPS姿态确定子系统在启用外部,独立参考方面很重要,以将控制输入限制为UAV飞行子系统。特别重要的是对系统完整性的良好理解。

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