Distributed angle-only orbit determination algorithm for non-cooperative spacecraft based on factor graph

IF 1.4 4区 管理学 Q3 ENGINEERING, ELECTRICAL & ELECTRONIC Iet Radar Sonar and Navigation Pub Date : 2024-05-22 DOI:10.1049/rsn2.12580
Zhixun Zhang, Keke Zhang, Leizheng Shu, Zhencai Zhu, Meijiang Zhou
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Abstract

Bayesian filtering provides an effective approach for the orbit determination of a non-cooperative target using angle measurements from multiple CubeSats. However, existing methods face challenges such as low reliability and limited estimation accuracy. Two distributed filtering algorithms based on factor graphs employed in the sub-parent and distributed cluster spacecraft architectures are proposed. Two appropriate factor graphs representing different cluster spacecraft structures are designed and implement distributed Bayesian filtering within these models. The Gaussian messages transmitted between nodes and the probability distributions of variable nodes are calculated using the derived non-linear Gaussian belief propagation algorithm. Gaussian messages propagate from the deputy spacecraft to the chief spacecraft in the sub-parent spacecraft architecture, demonstrating that the estimation accuracy converges to the centralised extended Kalman filter (EKF). Simulation results indicate that the algorithm enhances system robustness in observation node failures without compromising accuracy. In the distributed spacecraft architecture, neighbouring spacecraft iteratively exchanges Gaussian messages. The accuracy of the algorithm can rapidly approach the centralised EKF, benefiting from the efficient and unbiased transmission of observational information. Compared to existing distributed consensus filtering algorithms, the proposed algorithm improves estimation accuracy and reduces the number of iterations needed to achieve consensus.

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基于因子图的非合作航天器分布式纯角轨道确定算法
贝叶斯滤波为利用多颗立方体卫星的角度测量确定非合作目标的轨道提供了一种有效方法。然而,现有方法面临着可靠性低和估计精度有限等挑战。本文提出了两种基于子父和分布式集群航天器架构中使用的因子图的分布式滤波算法。设计了两种代表不同集群航天器结构的适当因子图,并在这些模型中实现了分布式贝叶斯滤波。使用衍生的非线性高斯信念传播算法计算节点间传输的高斯信息和变量节点的概率分布。高斯信息从副航天器传播到子母航天器结构中的主航天器,证明估计精度趋近于集中式扩展卡尔曼滤波器(EKF)。仿真结果表明,该算法在不影响精度的情况下增强了系统在观测节点故障时的鲁棒性。在分布式航天器架构中,相邻航天器迭代交换高斯信息。得益于高效、无偏的观测信息传输,该算法的精度可迅速接近集中式 EKF。与现有的分布式共识滤波算法相比,所提出的算法提高了估计精度,减少了达成共识所需的迭代次数。
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来源期刊
Iet Radar Sonar and Navigation
Iet Radar Sonar and Navigation 工程技术-电信学
CiteScore
4.10
自引率
11.80%
发文量
137
审稿时长
3.4 months
期刊介绍: IET Radar, Sonar & Navigation covers the theory and practice of systems and signals for radar, sonar, radiolocation, navigation, and surveillance purposes, in aerospace and terrestrial applications. Examples include advances in waveform design, clutter and detection, electronic warfare, adaptive array and superresolution methods, tracking algorithms, synthetic aperture, and target recognition techniques.
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