DSL 任务中环月卫星编队的相对导航:不完整观测数据的实时解决方案

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Fan Wu , Rui Zou , Zichen Zhao , Xinlong Le , Ruichen Xi
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引用次数: 0

摘要

DSL(发现最长波长的天空)任务是通过超长波长观测来探测宇宙黎明和黑暗时代的关键。然而,由于GNSS信号丢失、难以获得相对测量值和严重的轨道模糊问题,它给导航带来了重大挑战。考虑到这些因素,本文提出了一种针对DSL任务不完全星间观测的协同相对导航策略,该策略主要包括无锚定位、锚节点定位和坐标配准三个部分。首先,利用星间距离信息,采用多星协同定位方法获取非锚定位置,即使在距离缺失的情况下也能快速求解相对位置;其次,考虑到视场限制和光照条件导致的角度测量不完全,设计了一种新的信息融合互补方法来确定锚节点卫星的位置;第三,为实现高精度坐标配准,提出了一种基于不同锚节点定位精度的协方差加权Procrustes分析算法,将非锚点卫星位置转换为期望的坐标系。将这三种算法结合为一种融合的导航策略。对DSL任务中的聚类和尾随编队两种实际情况进行了数值仿真,验证了该方法的有效性,显示了该方法在处理不完全测量信息方面的有效性。在测量角度误差为50 μrad、测距误差为0.1 m的情况下,该方法在100 km范围内仍能保持5 m的精度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Relative navigation of circumlunar satellite formation in DSL mission: Real-time solution for incomplete observations
DSL (Discovering the sky at the longest wavelengths) mission is crucial for probing the cosmic dawn and dark ages through ultra-long wavelength observations. However, it presents significant navigation challenges due to GNSS signal loss, difficulty in obtaining relative measurements and severe orbital ambiguity problem. Considering these factors, this paper proposes a cooperative relative navigation strategy for the DSL mission's incomplete inter-satellite observations, consisting of three main parts: unanchored positioning, anchor nodes positioning and coordinate registration. Firstly, we obtain unanchored positions using inter-satellite range information through a multi-satellite cooperative localization method, which can quickly resolve relative positions even with missing range measurements. Secondly, considering the incomplete angle measurements caused by field of view limitations and illumination conditions, we design a new information fusion and complementary method to determine positions of the ANS (Anchor Node Satellites). Thirdly, to achieve high-precision coordinate registration, we propose a covariance-weighted Procrustes analysis algorithm based on positioning accuracies of different anchor nodes to transform unanchored satellite positions into the desired coordinate system. These three proposed algorithms are combined as a fused navigation strategy. Numerical simulations of two practical cases, clustering and trailing formation in the DSL mission, validate the effectiveness of the proposed method, showing the efficiency dealing with incomplete measurement information. Specifically, even with only 30 % angle measurements and 70 % range measurements, the proposed method can still maintain 5-meter accuracy within a distance of 100 km under 50 μrad angle-measuring error and 0.1 m ranging error.
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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