隼鸟2号太空舱单次机载观测轨迹分析

IF 1.3 4区 工程技术 Q2 ENGINEERING, AEROSPACE Journal of Spacecraft and Rockets Pub Date : 2023-08-25 DOI:10.2514/1.a35719
F. Zander, D. Buttsworth, Byrenn Birch, Allan Payne
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引用次数: 0

摘要

使用澳大利亚对“隼鸟2号”太空舱进行空中观测期间拍摄的单个视频流测量了“隼鸟”2号太空舱的再入轨迹。需要并开发了一种新的分析方法,以便能够从单一的角度确定轨迹。开发的方法使用视频流中可见的星场背景,结合飞机全球定位系统的数据,建立了实时测量太空舱的视线。然后使用一组常识性标准,包括高度和速度限制,来排除不可能的轨迹。然后使用最小二乘拟合程序对剩余的弹道进行检查和评估,以分析候选弹道。基于拟合参数对轨迹进行排序,从而能够确定单个最可能轨迹和一组最可能轨迹。根据测量推断,最有可能的“隼鸟2号”太空舱轨迹经过库伯佩迪以西10公里处,以150度的航向飞行。对其他极有可能的轨迹的评估表明,它们都以相似的距离经过了库伯-佩迪;然而,它们倾向于略高的航向,接近155度。在整个测量期间,测量飞机和太空舱之间的距离保持相对恒定,约为180公里。这项工作展示了一种新的方法来确定在星场背景下测量的物体的轨迹。重要的是,我们已经利用这一点建立了隼鸟2号返回舱的轨迹,从而确定了与我们飞机的距离,这将允许对我们的光谱数据进行详细分析。
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Trajectory Analysis of the Hayabusa2 Capsule from a Single Airborne Observation
The reentry trajectory of the Hayabusa2 capsule has been measured using a single video stream captured during the Australian Airborne Observation of the Hayabusa2 capsule. A new analysis methodology was required, and developed, to enable the trajectory to be determined from a single viewpoint. The method developed used the star-field background visible in the video stream, combined with the aircraft Global Positioning System data, to establish lines of sight along which the capsule was measured in time. A set of common sense criteria including altitude and velocity limits were then used to exclude impossible trajectories. The remaining trajectories were then examined and evaluated using a least-squares fitting routine to analyze candidate ballistic trajectories. The trajectories were ranked based on the fit parameter, enabling the determination of the single most likely trajectory and a family of most probable trajectories. The most probable Hayabusa2 capsule trajectory inferred from the measurements passed 10 km west of Coober Pedy and traveled at a heading of 150 deg. Evaluation of other highly probable trajectories showed they all passed Coober Pedy at a similar distance; however, they tended toward a slightly higher heading, approaching 155 deg. The distance between the measurement aircraft and the capsule remained relatively constant at approximately 180 km throughout the measurement period. This work demonstrates a new method for determining the trajectory of an object measured with a star-field background. Importantly, we have used this to establish the Hayabusa2 reentry capsule trajectory, and hence the distance from our aircraft, which will allow the detailed analysis of our spectral data.
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来源期刊
Journal of Spacecraft and Rockets
Journal of Spacecraft and Rockets 工程技术-工程:宇航
CiteScore
3.60
自引率
18.80%
发文量
185
审稿时长
4.5 months
期刊介绍: This Journal, that started it all back in 1963, is devoted to the advancement of the science and technology of astronautics and aeronautics through the dissemination of original archival research papers disclosing new theoretical developments and/or experimental result. The topics include aeroacoustics, aerodynamics, combustion, fundamentals of propulsion, fluid mechanics and reacting flows, fundamental aspects of the aerospace environment, hydrodynamics, lasers and associated phenomena, plasmas, research instrumentation and facilities, structural mechanics and materials, optimization, and thermomechanics and thermochemistry. Papers also are sought which review in an intensive manner the results of recent research developments on any of the topics listed above.
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