Space-Based Passive Orbital Maneuver Detection Algorithm for High-Altitude Situational Awareness

Shihang Yang, Xin Jin, Baichun Gong, Fei Han
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Abstract

Orbital maneuver detection for non-cooperative targets in space is a key task in space situational awareness. This study develops a passive maneuver detection algorithm using line-of-sight angles measured by a space-based optical sensor, especially for targets in high-altitude orbit. Emphasis is placed on constructing a new characterization for maneuvers as well as the corresponding detection method. First, the concept of relative angular momentum is introduced to characterize the orbital maneuver of the target quantitatively, and the sensitivity of the proposed characterization is analyzed mathematically. Second, a maneuver detection algorithm based on the new characterization is designed in which sliding windows and correlations are utilized to determine the mutation of the maneuver characterization. Subsequently, a numerical simulation system composed of error models, reference missions and trajectories, and computation models for estimating errors is established. Then, the proposed algorithm is verified through numerical simulations for both long-range and close-range targets. The results indicate that the proposed algorithm is effective. Additionally, the sensitivity of the proposed algorithm to the width of the sliding window, accuracy of the optical sensor, magnitude and number of maneuvers, and different relative orbit types is analyzed, and the sensitivity of the new characterization is verified using simulations.
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用于高空态势感知的天基被动轨道机动探测算法
空间非合作目标的轨道机动探测是空间态势感知的一项关键任务。本研究利用天基光学传感器测量的视线角开发了一种被动机动探测算法,尤其适用于高空轨道目标。重点是构建一种新的机动特征以及相应的探测方法。首先,引入相对角动量的概念来定量表征目标的轨道机动,并对所提出的表征方法的灵敏度进行数学分析。其次,设计了一种基于新表征的机动检测算法,利用滑动窗口和相关性来确定机动表征的突变。随后,建立了一个由误差模型、参考任务和轨迹以及用于估计误差的计算模型组成的数值模拟系统。然后,通过对远程和近程目标的数值模拟验证了所提出的算法。结果表明,所提出的算法是有效的。此外,还分析了所提算法对滑动窗口宽度、光学传感器精度、机动幅度和次数以及不同相对轨道类型的敏感性,并通过仿真验证了新表征的敏感性。
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