王龙, 雷韫璠, 张新宇, 张辉, 武延鹏. 基于光学成像探测的仅测角高轨空间物体接近感知方法[J]. 红外与激光工程, 2024, 53(7): 20240183. DOI: 10.3788/IRLA20240183
引用本文: 王龙, 雷韫璠, 张新宇, 张辉, 武延鹏. 基于光学成像探测的仅测角高轨空间物体接近感知方法[J]. 红外与激光工程, 2024, 53(7): 20240183. DOI: 10.3788/IRLA20240183
WANG Long, LEI Yunfan, ZHANG Xinyu, ZHANG Hui, WU Yanpeng. Angles-only method of space objects approach perception based on optical imaging[J]. Infrared and Laser Engineering, 2024, 53(7): 20240183. DOI: 10.3788/IRLA20240183
Citation: WANG Long, LEI Yunfan, ZHANG Xinyu, ZHANG Hui, WU Yanpeng. Angles-only method of space objects approach perception based on optical imaging[J]. Infrared and Laser Engineering, 2024, 53(7): 20240183. DOI: 10.3788/IRLA20240183

基于光学成像探测的仅测角高轨空间物体接近感知方法

Angles-only method of space objects approach perception based on optical imaging

  • 摘要: 提出一种仅利用任务航天器光学成像探测设备给出的测角信息进行高轨空间物体接近行为感知的方法。首先,分析了空间物体相对任务航天器的方位变化规律,得到物体接近时在任务航天器轨道坐标系下方位角正切值随时间波动幅值逐渐增大;其次,分析了在光学成像探测设备成像过程中,逆光与探测设备灵敏度对空间物体可见性的影响,得到物体可见弧段在每个轨道周期内具有一定的相似性;进一步地,根据物体相对方位及可见性的变化规律,设计了一种空间物体接近行为感知方法,利用物体观测量的轨道周期一致性进行多段观测量关联,拟合方位角正切值随时间波动趋势,预测波动极值并统计极值变化规律,实现物体接近行为感知;最后,仿真验证了该方法具备不依赖距离信息感知高轨空间物体相对任务航天器接近行为的能力,仅利用3个轨道周期内、每周期有效弧段大于30 min的高轨空间物体指向测量信息判断物体相对任务航天器存在接近行为的准确率优于96%。结果证明:该方法通过赋能任务航天器常用光学成像探测设备高效费比地实现航天器自我防护能力有效提升,可普遍用于高轨航天器任务。

     

    Abstract:
    Objective Geosynchronous orbit (GEO) satellites are a critical component of global telecommunications and navigation systems, but they are also vulnerable to potential collisions or hostile interactions with other space objects. Therefore, the ability to accurately perceive the approach behavior of these objects is paramount for enhancing the safety and autonomy of GEO spacecraft. This paper proposes a sophisticated and reliable method for detecting the approach behavior of GEO space objects only using line-of-sight measurements of objects derived from optical imaging sensors. Existing methods often rely on distance measurements, which can be challenging to obtain accurately in space environments. Research in this paper aims to overcome this limitation by utilizing only line-of-sight information of objects, which is readily available from optical sensors. By analyzing the temporal variations in azimuth and elevation angles, we aim to identify patterns that are indicative of an approaching object and develop algorithms to accurately perceive the approach behavior of these objects.
    Methods To achieve this objective, a comprehensive analytical framework is presented. First, the effects of illumination conditions and the sensitivity of the optical sensor on the object's visibility are considered (Fig.2). Second, the azimuth and elevation angle variations of a GEO object relative to a mission spacecraft are analyzed to identify patterns that are indicative of an approaching object (Fig.4). As the object approaches, the magnitude of variations in the tangent of the azimuth angle increases over time (Fig.5), providing a potential signature for perception. By leveraging the orbital periodicity of the space object and the consistency of its visible arcs, the proposed method correlates multiple observation segments (Fig.7), fits the temporal trend of the azimuth angle tangent, predicts extreme values, and monitors the pattern of these extremes to accurately perceive the object's approach behavior.
    Results and Discussions Simulations were conducted to evaluate the performance of the proposed method (Fig.8). The results demonstrate that the method is capable of accurately detecting the approach of GEO objects using only line-of-sight measurements from optical imaging sensors. Specifically, the method achieved an accuracy rate of over 96% in identifying approaching objects using only three orbital periods of data, with each orbital period containing effective segments greater than 30 minutes (Tab.2). This high accuracy indicates that the method can provide valuable information for spacecraft self-defense systems, enabling them to detect potential threats at an early stage. Furthermore, the method exhibits several advantages over traditional methods that rely on distance measurements. First, it does not require additional sensors or instrumentation for distance measurements, thus reducing the complexity and cost of the overall system (Fig.10). Second, it is robust to variations in illumination conditions and sensor sensitivity, ensuring reliable performance in a range of environmental conditions. Finally, the method's simplicity and efficiency make it suitable for real-time implementation on spacecraft with limited computational resources.
    Conclusions A method for detecting the approach behavior of GEO space objects only using line-of-sight measurements of objects derived from optical imaging sensors is designed, by leveraging the unique patterns in the temporal variations of azimuth and elevation angles. This method represents a significant advancement in the field of space safety and security, as it overcomes the limitations of traditional distance-based methods and provides a reliable means for autonomous threat detection. The simplicity and efficiency of the proposed method make it suitable for real-time implementation on spacecraft, enabling them to detect potential threats at an early stage. In summary, this research has laid the foundation for a new paradigm in space object perception and trackin, leveraging line-of-sight information from optical sensors to provide enhanced capabilities for spacecraft self-defense and situational awareness.

     

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