A Hybrid Robust Information Fusion Scheme for SFNS/XNAV Integration

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2025-01-07 DOI:10.1109/TAES.2025.3526738
Gaoge Hu;Qian Zhang;Guangle Gao;Tao Feng;Bingbing Gao
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Abstract

The integration of the spectral frequency-shift navigation system (SFNS) and the X-ray pulsar navigation (XNAV) system provides a promising solution for deep-space navigation, with respect to the complementarity in velocity and position determination. However, since the gross errors involved in the SFNS and the inherent systemic errors in XNAV pertain to different types of measurement uncertainties, it is very difficult to acquire the globally robust state estimation for SFNS/XNAV integration via the existing distributed information fusion methods as usual. This article develops a hybrid robust information fusion scheme with a two-layer architecture to address the aforementioned issue. In the first layer, a Huber M-estimation based extended Kalman filter (HEKF) is designed for the SFNS to restrain the effect of gross errors, while the systemic errors in XNAV are compensated in parallel based on system state augmentation with the augmented extended Kalman filter (AEKF). In the second layer, from the perspective of minimum variance criterion, a multisource optimal data fusion strategy is established to fuse the local robust state estimations output by the HEKF and the AEKF, such that SFNS/XNAV integration is realized in a globally optimal manner. Simulations on a Mars exploration mission have validated that the proposed information fusion scheme exhibits excellent performance in terms of robustness and navigation accuracy in comparison with the existing works.
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SFNS/XNAV集成的混合鲁棒信息融合方案
频谱频移导航系统(SFNS)与x射线脉冲星导航系统(XNAV)相结合,在速度和位置确定方面具有互补性,为深空导航提供了一种很有前途的解决方案。然而,由于SFNS的粗误差和XNAV的固有系统误差属于不同类型的测量不确定性,通常通过现有的分布式信息融合方法很难获得SFNS/XNAV集成的全局鲁棒状态估计。本文开发了一种具有两层体系结构的混合健壮信息融合方案来解决上述问题。在第一层,设计了基于Huber m估计的扩展卡尔曼滤波器(HEKF)用于SFNS抑制粗误差的影响,而XNAV的系统误差则基于增强的扩展卡尔曼滤波器(AEKF)进行系统状态增强并行补偿。第二层从最小方差准则出发,建立多源最优数据融合策略,将HEKF和AEKF输出的局部鲁棒状态估计融合,以全局最优方式实现SFNS/XNAV集成。火星探测任务的仿真结果表明,该信息融合方案在鲁棒性和导航精度方面均优于现有方案。
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来源期刊
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
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