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Variational Bayesian adaptive high-degree cubature Huber-based filter for vision-aided inertial navigation on asteroid missions

机译:基于变分的贝叶斯自适应高度立方Huber基于小行星任务的视觉辅助惯性导航滤波器

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摘要

Vision-aided inertial navigation (VAIN) is a prospective technique for determining the pose of the spacecraft during asteroid missions. The VAIN system can fuse the inertial and visual data by employing the high-degree cubature Kalman filter (HCKF) because it can accurately handle non-linear problems. However, the visual measurements can be corrupted by non-Gaussian noise with unknown time-varying covariance, resulting in severe degradation of the HCKF. To improve the navigational accuracy of the spacecraft in these situations, the authors propose a novel adaptive robust HCKF known as variational Bayesian (VB) adaptive high-degree cubature Huber-based filter (VB-AHCHF). In the novel algorithm, the fifth-degree cubature rule and VB theory are combined to estimate the state and track the non-stationary statistical characteristics of the measurement noise. In addition, utilising the M-estimation, which is defined as the Huber technique, it modifies the update step of the formal Bayesian filtering. Therefore, the VB-AHCHF can exhibit adaptability and robustness to the covariance uncertainty and non-Gaussianity of the measurement noise. Their simulation results show that the estimation accuracy of VB-AHCHF, as well as its adaptability and robustness, is superior to all state-of-the-art algorithms, e.g. HCKF, high-degree cubature Huber-based filter, and the VB adaptive HCKF.
机译:视觉辅助惯性导航(Vain)是用于在小行星任务期间确定航天器姿势的前瞻性技术。 Vain系统可以通过使用高度Cubature Kalman滤波器(HCKF)来融合惯性和视觉数据,因为它可以准确地处理非线性问题。然而,视觉测量可以通过具有未知时变协方差的非高斯噪声损坏,导致HCKF的严重降解。为了提高这些情况下航天器的航行准确性,作者提出了一种称为变形贝叶斯(VB)自适应高度CCKF的新型自适应稳健Hckf,基于自适应高度Cuber的滤波器(VB-AHCHF)。在新颖的算法中,组合第五次级规则和VB理论以估计状态并跟踪测量噪声的非静止统计特征。此外,利用M-估计,该估算被定义为HUBER技术,它修改了正式贝叶​​斯滤波的更新步骤。因此,VB-AHCHF可以表现出对调节噪声的协方差的不确定性和非高斯的适应性和鲁棒性。它们的仿真结果表明,VB-AHCHF的估计精度以及其适应性和鲁棒性,优于所有最先进的算法,例如, HCKF,高度Cubature Huber的过滤器,以及VB自适应HCKF。

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  • 来源
    《Radar, Sonar & Navigation, IET》 |2020年第9期|1391-1401|共11页
  • 作者单位

    Harbin Inst Technol Dept Aerosp Engn Harbin Peoples R China;

    Harbin Inst Technol Dept Aerosp Engn Harbin Peoples R China;

    Harbin Inst Technol Dept Aerosp Engn Harbin Peoples R China;

    Harbin Inst Technol Dept Aerosp Engn Harbin Peoples R China;

    Harbin Inst Technol Dept Aerosp Engn Harbin Peoples R China;

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