基于陀螺仪偏差指数的实验室无人机姿态机动流畅性评价

S. Fiori, Nicola Sabino, A. Bonci
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引用次数: 1

摘要

本文综述了基于实验室的四轴飞行器姿态机动流畅性评估的研究进展。该手稿说明了基于实验室的数据采集设置和数学数据处理算法,以测试一种新的姿态机动流畅性估计指标称为几何偏移。几何倾斜指数是根据四旋翼飞行器的陀螺仪传感器返回的角变量值来定义的。对合成陀螺仪信号和实际陀螺仪信号进行了数值测试,结果表明几何偏移指数对姿态机动的流畅性相当敏感。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
In-Lab Drone’s Attitude Maneuvering Fluency Evaluation by a Gyroscopic Lurch Index
The present paper reports on the current progress about the laboratory-based assessment of the fluency of attitude maneuvering of a quadcopter. The manuscript illustrates a laboratory-based data-acquisition setup and a mathematical data-processing algorithm to test a novel attitude maneuvering fluency estimation index termed geometric lurch. The geometric lurch index is defined in terms of angular variables’ values as returned by gyroscopic sensors that a quadcopter vehicle is equipped with. The results of several numerical tests, conducted on both synthetic and real-world gyroscopic signals, show that the geometric lurch index is fairly sensitive to the fluency of attitude maneuvering.
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