Research and application of attitude optimal estimation for quadrotor UAV

Qi Li, Qiong Hu, Jie Chen, Raja Rajeswari, S. Selvaperumal
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Abstract

optimal estimation of the attitude, an attitude solution system based on low-cost IMU sensors is proposed. The system uses quadratic coordinate conversion to fuse the gyroscope, accelerometer, and magnetic compass data, and the attitude deviation is corrected by the PI controller, and the attitude information of the vehicle is solved by a complementary filtering algorithm. The experimental results show that the proposed algorithm not only effectively improves the accuracy of the attitude solution to meet the flight requirements of small UAV, but also suppresses the influence of random deviation of the attitude sensor and the noise of the three-axis acceleration measurement on the attitude solution, and achieves the requirement of accurate and reliable attitude data output for a long time.
四旋翼无人机姿态最优估计研究与应用
针对姿态最优估计问题,提出了一种基于低成本IMU传感器的姿态求解系统。该系统采用二次坐标转换对陀螺仪、加速度计和磁罗经数据进行融合,由PI控制器对姿态偏差进行校正,并采用互补滤波算法求解飞行器姿态信息。实验结果表明,所提算法不仅有效提高了姿态解的精度,满足小型无人机的飞行要求,而且抑制了姿态传感器随机偏差和三轴加速度测量噪声对姿态解的影响,实现了长期准确可靠的姿态数据输出要求。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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