基于MEMS传感技术的姿态航向参考系统设计

Peng Huang, Haojie Lv
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引用次数: 2

摘要

针对传统姿态航向参考系统(ARHS)在航天器、机器人和车辆等领域应用成本高、体积大的问题,提出了一种基于低成本MEMS传感器的姿态航向参考系统(ARHS)新方法。该算法以四元数和三陀螺漂移为状态向量,建立状态方程。同时,将重力加速度分量和磁场强度分量作为观测向量,建立观测方程。该算法采用一种特殊的方法对地磁场进行补偿。为了验证所提出的基于四元数的扩展卡尔曼滤波算法,研制了一种微型四旋翼飞行器。结果表明,该方法能获得准确的姿态信息,并能有效抑制白噪声。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The design of attitude heading reference system based on MEMS sensing technology
In view of the high cost and large volume of the traditional attitude heading reference system (ARHS) applied in the fields of spacecraft, robot and vehicle, a new method based on low cost MEMS sensor for AHRS is proposed. In this algorithm, the quaternion and three gyro drift are chosen as state vector to establish the state equation. At the same time, the components of acceleration of gravity and magnetic field intensity in the body fixed reference are considered as the observation vectors to establish the observation equation. In this algorithm, the earth's magnetic field is compensated by a special method. In order to evaluate the proposed quaternion-based extended Kalman filter algorithm, a micro quadrotor is developed. The results show that the proposed method can obtain the accurate attitude information and can suppress the white noise.
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