Analytical configuration uncertainty propagation of geocentric interferometric detection constellation

IF 6.5 1区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Astrodynamics Pub Date : 2023-01-16 DOI:10.1007/s42064-022-0157-x
Dong Qiao, Xingyu Zhou, Xiangyu Li
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引用次数: 2

Abstract

Long-term configuration stability is essential for an interferometric detection constellation (IDC), which is closely related to initial uncertainty. Therefore, it is vital to evaluate the uncertainty and characterize the configuration stability. In this study, an analytical method was developed for the configuration uncertainty propagation of a geocentric triangular IDC. The angular momentum and the argument latitude were found to be significantly affected by the initial uncertainty and were selected as the core variables. By averaging the perturbation in one revolution, an analytical solution was proposed for propagating the core orbital elements in one revolution. Subsequently, the analytical solution of the orbit elements during the mission period is obtained by multiplying the solutions in iterative revolutions. The relationship between the selected orbital elements and the configuration stability parameters was established using an analytical solution. The effects of the initial uncertainty in different directions on the configuration and stable domains were studied. Simulations show that the developed method is highly efficient and accurate in predicting the configuration stability. The relative error with respect to the Monte Carlo simulations was less than 3% with a time consumption of 0.1%. The proposed method can potentially be useful for constellation design and stability analysis.

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地心干涉探测星座解析构型不确定度传播
长期配置稳定性对于干涉检测星座(IDC)至关重要,这与初始不确定性密切相关。因此,评估不确定性和表征构型稳定性至关重要。在本研究中,提出了一种分析地心三角形IDC配置不确定性传播的方法。角动量和自变量纬度被发现受到初始不确定性的显著影响,并被选为核心变量。通过对一周内的扰动求平均值,提出了核心轨道单元在一周内传播的解析解。随后,通过将解乘以迭代转数,获得任务期间轨道元素的解析解。使用解析解建立了所选轨道元素与构型稳定性参数之间的关系。研究了不同方向的初始不确定度对构型和稳定域的影响。仿真结果表明,该方法在结构稳定性预测方面具有较高的效率和准确性。蒙特卡罗模拟的相对误差小于3%,时间消耗为0.1%。所提出的方法可能对星座设计和稳定性分析有用。
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来源期刊
Astrodynamics
Astrodynamics Engineering-Aerospace Engineering
CiteScore
6.90
自引率
34.40%
发文量
32
期刊介绍: Astrodynamics is a peer-reviewed international journal that is co-published by Tsinghua University Press and Springer. The high-quality peer-reviewed articles of original research, comprehensive review, mission accomplishments, and technical comments in all fields of astrodynamics will be given priorities for publication. In addition, related research in astronomy and astrophysics that takes advantages of the analytical and computational methods of astrodynamics is also welcome. Astrodynamics would like to invite all of the astrodynamics specialists to submit their research articles to this new journal. Currently, the scope of the journal includes, but is not limited to:Fundamental orbital dynamicsSpacecraft trajectory optimization and space mission designOrbit determination and prediction, autonomous orbital navigationSpacecraft attitude determination, control, and dynamicsGuidance and control of spacecraft and space robotsSpacecraft constellation design and formation flyingModelling, analysis, and optimization of innovative space systemsNovel concepts for space engineering and interdisciplinary applicationsThe effort of the Editorial Board will be ensuring the journal to publish novel researches that advance the field, and will provide authors with a productive, fair, and timely review experience. It is our sincere hope that all researchers in the field of astrodynamics will eagerly access this journal, Astrodynamics, as either authors or readers, making it an illustrious journal that will shape our future space explorations and discoveries.
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