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A Direct and Non-Singular UKF Approach Using Euler Angle Kinematics for Integrated Navigation Systems

机译:基于欧拉角运动学的直接非奇异UKF方法用于组合导航系统

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摘要

This paper presents a direct and non-singular approach based on an unscented Kalman filter (UKF) for the integration of strapdown inertial navigation systems (SINSs) with the aid of velocity. The state vector includes velocity and Euler angles, and the system model contains Euler angle kinematics equations. The measured velocity in the body frame is used as the filter measurement. The quaternion nonlinear equality constraint is eliminated, and the cross-noise problem is overcome. The filter model is simple and easy to apply without linearization. Data fusion is performed by an UKF, which directly estimates and outputs the navigation information. There is no need to process navigation computation and error correction separately because the navigation computation is completed synchronously during the filter time updating. In addition, the singularities are avoided with the help of the dual-Euler method. The performance of the proposed approach is verified by road test data from a land vehicle equipped with an odometer aided SINS, and a singularity turntable test is conducted using three-axis turntable test data. The results show that the proposed approach can achieve higher navigation accuracy than the commonly-used indirect approach, and the singularities can be efficiently removed as the result of dual-Euler method.
机译:本文提出了一种基于无味卡尔曼滤波器(UKF)的直接且非奇异的方法,用于借助速度对捷联惯性导航系统(SINS)进行集成。状态向量包含速度和欧拉角,系统模型包含欧拉角运动学方程。身体框架中测得的速度用作过滤器测量值。消除了四元数非线性等式约束,克服了交叉噪声问题。滤波器模型简单易行,无需线性化。数据融合由UKF执行,UKF直接估算并输出导航信息。由于在滤波时间更新期间同步完成了导航计算,因此无需分别处理导航计算和纠错。另外,借助双重欧拉方法避免了奇异性。所提方法的性能通过配备有里程表辅助SINS的陆地车辆的道路测试数据进行了验证,并使用三轴转盘测试数据进行了奇异性转盘测试。结果表明,所提出的方法比常用的间接方法具有更高的导航精度,并且由于双重欧拉方法,可以有效地去除奇异点。

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