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Optical In-Situ Monitor A Breadboard System to Enable Space-Based Optical Observation of Space Debris

机译:光学原位监控面包板系统,以实现空间碎片的空间光学观察

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The goals of the ESA project "Optical In-Situ Monitor" are to design and integrate a breadboard of a space-based space debris camera and to develop and test its end-to-end processing chain. The corresponding future flight model shall be used for the detection of small-sized (down to 1 mm) space debris in LEO as well as larger objects in GEO. It is intended to be flown on a platform in sun-synchronous orbit near the terminator plane. The activity's breadboard system is comprised of the following three main elements: Breadboard Instrument: Acquires images of space debris scenes generated by the Test Set-Up with the characteristics of the future flight model instrument. Image processing pipeline: On-board debris detection and data reduction, on-ground astrometry and photometry. Test Set-Up: Scene generator for space debris observation scenarios. The breadboard system will constitute a unique facility to perform realistic tests of the end-to-end chain for debris observations within a controlled environment. This chain starts from signal generation via the scene generator, is followed by the acquisition of images via the breadboard instrument and finally performs the data processing until the astrometric and photometric reduction step. High accuracy is required for the scene generation part regarding motion and photometric accuracy because it serves as ground-truth for the system. As prime contractor, Airbus Defence and Space is responsible for project management, system and performance engineering, the breadboard instrument, and on-board data processing hardware issues. The required image processing software is being developed at the Astronomical Institute of the University of Bern (AIUB). Micos provides the space debris scene generator, emulating both debris and star background. The paper will provide an overview of requirements and the design of the three main elements as well as on the results of the end-to-end performance tests.
机译:ESA项目“光学原位监视器”的目标是设计和集成基于空间的空间碎片摄像头的面包板,并开发和测试其端到端处理链。相应的未来飞行模型应用于检测Leo中小型(下至1 mm)空间碎片以及Geo中的较大物体。它旨在在终结者平面附近的太阳同步轨道的平台上飞行。活动的面包板系统由以下三个主要元素组成:面包板器械:获取测试设置生成的空间碎片场景图像,与未来飞行模型仪器的特点。图像处理管道:车载碎片检测和数据减少,接地横梁和光度测量。测试设置:空间碎片观察场景的场景发生器。面包板系统将构成一个独特的设施,以便在受控环境中执行碎屑观测的端到端链条的现实测试。该链从通过场景发生器从信号产生开始,然后通过面包板器械获取图像,最后执行数据处理,直到天体测量和光度降低步骤。现场生成部分需要高精度,有关运动和光度学精度,因为它用作系统的地面真实性。作为主要承包商,空中客车防御和空间负责项目管理,系统和性能工程,面包板仪器和板载数据处理硬件问题。所需的图像处理软件正在伯尔尼大学(AIUB)的天文学研究所开发。 MICOS提供空间碎片场景发生器,模拟碎片和星背景。本文将概述要求和三个主要元素的设计以及端到端性能测试的结果。

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