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Multiple Robust High-degree Cubature Kalman Filter for Relative Position and Attitude Estimation of Satellite Formation

机译:用于卫星编队相对位置和姿态估计的多重鲁棒高阶Cubature卡尔曼滤波

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摘要

The High-degree Cubature Kalman Filter (HCKF) is proposed as a novel methodology based on the arbitrary degree spherical rule, which can achieve better performance than the traditional Kalman filter. However, it also has a large calculation burden when used in a high-dimension and high-degree of accuracy estimation system. The number of sampling points of an HCKF increases polynomially with increasing state-space dimensions, which further increases the calculation burden. The reduction of the number of the state-space dimensions is the main contribution of this study. A strategy for HCKF based on the partitioning of the state-space and orthogonal principle is introduced, referred to as the Multiple Robust HCKF (MRHCKF). It is shown that this technique can effectively reduce the calculation burden for the high-dimension system with robust performance. Numerical simulations are performed for the example of high-dimension relative position and attitude estimation to show that the proposed method can obtain nearly the same performance as the HCKF, while drastically reducing computational complexity.
机译:提出了一种基于任意度球面法则的新颖的高阶Cubature卡尔曼滤波器(HCKF),该算法比传统的卡尔曼滤波器具有更好的性能。然而,当用于高维度和高精确度估计系统时,它也具有很大的计算负担。 HCKF的采样点数量随着状态空间尺寸的增加而呈多项式增加,这进一步增加了计算负担。减少状态空间维数是这项研究的主要贡献。介绍了一种基于状态空间划分和正交原理的HCKF策略,称为多重鲁棒HCKF(MRHCKF)。结果表明,该技术可以有效地降低具有鲁棒性能的高维系统的计算负担。以高维相对位置和姿态估计为例进行了数值模拟,结果表明所提方法可以取得与HCKF几乎相同的性能,同时大大降低了计算复杂度。

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