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LEDSAT: a LED-based LEO demonstrator for space debris orbit and attitude determination

机译:LEDSAT:用于空间碎片轨道和姿态决心的基于LEO的狮子座演示器

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Optical Ground based space debris monitoring and orbit determination are mainly restricted to a short time window, with the observable exposed to sunlight and the observer in darkness. Most of the times, the target is detected by means of sidereal tracking or it is directly tracked to acquire its lightcurve. In both configurations the object luminous flux depends on the elevation angle, due to the atmospheric extinction, the Sun-object-observatory phase angle, and the object-observatory range. Among space debris, a large number of inoperative satellites and spent rockets lie in Low Earth Orbit (LEO), introducing high risks for operational spacecraft, including crewed vessels. The LEDSAT (LED-based small SATellite) 1-Unit CubeSat project, managed by the Sapienza Space Systems and Space Surveillance Laboratory (S5Lab) at Sapienza - University of Rome and conceived in collaboration with the University of Michigan, has been accepted in 2017 for the European Space Agency "Fly Your Satellite!" Programme. The project aims at testing a Light Emitting Diodes (LED)-based payload for verification and improvement of the current methodologies of optical orbit determination. In the first project year, the LED-based payload radiometric properties have been validated, while the diodes have been qualified for the LEO environment. The CubeSat will be launched in early 2020. The satellite will be equipped with LEDs boards of different colors (red, green and blue), paired in opposite faces. This self-illuminating system increases the visibility to the totality of the Earth dark hemisphere, regardless of the phase angle, with a consequent improvement of the available data for orbit determination. Moreover, the emission in different visible spectral bands will allow to reconstruct the spacecraft attitude with the use of a theoretical model that is currently being finalized. Since small satellites are usually deployed in large clusters and the identification in the first hours from deploy
机译:基于光学地面的空间碎片监测和轨道测定主要限于短时间窗口,可观察到的阳光和观察者在黑暗中。大多数时候,通过恒星跟踪检测目标,或者直接跟踪以获取其光电。在这两种配置中,物体光通量取决于仰角,由于大气消光,太阳对象观测位角和对象天文台范围。在空间碎片中,大量不起作用的卫星和花火在低地轨道(LEO)中位于低地轨道(LEO)中,为运营宇宙飞船引入了高风险,包括船员。 LEDSAT(基于LED的小型卫星)1-INEO CUBESAT项目由Sapienza Space Systems及太空监测实验室(S5LAB)管理的Sapienza - 罗马大学和与密歇根大学建立合作,已在2017年被接受欧洲航天局“飞卫星!”程序。该项目旨在测试基于发光二极管(LED)的有效载荷,用于验证和改进光学轨道测定的当前方法。在第一个项目年份中,已经验证了基于LED的有效载荷辐射性属性,而二极管已获得Leo环境的资格。 CubeSat将于2020年初推出。卫星将配备不同颜色(红色,绿色和蓝色)的LED板,配对相对的面孔。这种自我照明系统增加了地球黑暗半球整体的可见性,无论相位角如何,随后改善了用于轨道确定的可用数据。此外,不同可见光谱带中的发射将允许使用目前最终确定的理论模型来重建航天器姿态。由于小型卫星通常部署在大群中,并且在部署的第一小时内识别

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