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Geometric stochastic filter with guaranteed performance for autonomous navigation based on IMU and feature sensor fusion

机译:几何随机滤波器,基于IMU的自主导航保证性能和特征传感器融合

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This paper concerns the estimation problem of attitude, position, and linear velocity of a rigid-body autonomously navigating with six degrees of freedom (6 DoF). The navigation dynamics are highly nonlinear and are modeled on the matrix Lie group of the extended Special Euclidean Group SE_2(3). A computationally cheap geometric nonlinear stochastic navigation filter is proposed on SE_2(3) with guaranteed transient and steady-state performance. The proposed filter operates based on a fusion of sensor measurements collected by a low-cost inertial measurement unit (IMU) and features (obtained by a vision unit). The closed loop error signals are guaranteed to be almost semi-globally uniformly ultimately bounded in the mean square from almost any initial condition. The equivalent quaternion representation is included in the Appendix. The filter is proposed in continuous form, and its discrete form is tested on a real-world dataset of measurements collected by a quadrotor navigating in three dimensional (3D) space.
机译:本文涉及用六个自由度(6 DOF)自主导航的刚性态度,位置和线性速度的估计问题。导航动态是高度非线性的,并在扩展特殊欧几里德组SE_2(3)的矩阵Lie组上建模。在SE_2(3)上提出了一种计算上便宜的几何非线性随机导航滤波器,具有保证的瞬态和稳态性能。所提出的滤波器基于由低成本惯性测量单元(IMU)收集的传感器测量的融合和特征(由视觉单元获得)的传感器测量的融合。闭环误差信号被保证几乎在几乎任何初始条件下在平均方形中均匀地最终界定。等效的四元数表示包含在附录中。滤波器以连续形式提出,并且其离散形式在由三维(3D)空间中导航的四分之一电位的测量的实际数据集上进行测试。

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