Passive attitude estimation using gyroscopes and all-accelerometer IMU

Y. M. Al-Rawashdeh, M. Elshafei, S. El-Ferik
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引用次数: 3

Abstract

In this paper, a novel approach to estimate a vehicle attitude using gyroscopes and an array of linear tri-axial accelerometers arranged in a certain configuration is presented. This configuration provides direct angular acceleration measurements that will be of great value once the quaternion dynamical equation is solved using Unscented Kalman filter. Various new states and measurements models based on the rotational quaternion are presented. Using this approach, estimating the attitude of a vehicle using linear accelerometers along with gyroscopes enables a completely passive attitude estimation under the simultaneous actions of vehicle varying center of gravity position, unknown varying gravitational field, and an accelerating vehicle without any singularity being involved in the states or measurements models which were not reported in the related literature to the best of authors' knowledge.
利用陀螺仪和全加速度计进行被动姿态估计
本文提出了一种利用陀螺仪和一组按一定构型排列的线性三轴加速度计来估计飞行器姿态的新方法。这种配置提供了直接的角加速度测量,一旦使用Unscented卡尔曼滤波器求解四元数动力学方程,这将具有很大的价值。提出了基于旋转四元数的各种新的状态和测量模型。利用该方法,利用线性加速度计和陀螺仪对车辆的姿态进行估计,可以在车辆变化重心位置、未知变化重力场和加速车辆同时作用下进行完全被动的姿态估计,而不涉及任何奇异状态或测量模型,这是作者所知的相关文献中未报道的。
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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