改善抛物线飞行实验条件的三轴稳定平台

Deepa Anantha Raman, Bruno Comesaña Cuervo, Viktória Jurcáková, Arnau Busom Vidal, Estelle Crouzet, Antoni Eritja Olivella, Juan Gracia García-Lisbon, Rebecka Kjellman, Minka Suomela, Thomas Kuhn, R. Laufer, Olle Persson
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引用次数: 0

摘要

在地球上有不同的方式提供自由落体条件,以测试组件,进行实验或演示设备,然后才能将其纳入太空任务。其中一种选择是抛物线飞行:简单地说,飞机沿着抛物线轨道飞行,机载有效载荷经历几秒钟的失重状态。自20世纪50年代以来,这些飞行一直在进行,以模拟实验和宇航员训练的空间条件。该项目的目标是开发一个立方体平台,在抛物线飞行的微重力阶段为实验进行三轴姿态稳定。目标是稳定平台,从而减少影响微重力质量的扰动和振动。为此,由三个正交构型的反作用轮组成的姿态控制系统将抵消惯性测量单元姿态确定系统测量到的扰动。该平台将在一次自组织飞行活动中使用一架小型飞机进行测试。该项目由9名学生组成,目前处于初步设计阶段。然而,平台结构的原型和测试已经开始使用小规模设计,并且已经订购了几个硬件组件。由于该工艺的诸多优点,该平台将使用增材制造进行打印。组件集成预计将及时完成,以便在2022年5月的飞行活动之前促进各种子系统的实验室测试。飞行活动结束后,收集到的数据将被分析、处理和公布,以确保科学界能够获得这些数据。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A 3-axis stabilisation platform to improve experiment conditions in parabolic flights
There are different ways of providing free-fall conditions on Earth in order to test a component, perform an experiment or demonstrate equipment before it can be included in a space mission. One of these options is a parabolic flight: briefly, the aircraft flies on a parabolic trajectory with the on-board payload experiencing several seconds of weightlessness. These flights have been performed since the 1950s to simulate space conditions for experiments as well as astronaut training. The project objective is to develop a cubical platform to perform 3-axis attitude stabilisation for experiments during the microgravity phase of a parabolic flight. The goal is to stabilise the platform and thus reduce perturbations and vibrations that diminish the quality of the microgravity achieved. To do so the attitude control system, composed of three reaction wheels in orthogonal configuration, will counterbalance the disturbances measured by the attitude determination system, an inertial measurement unit. The platform will be tested using a small aircraft in a self-organised flight campaign. Comprising nine students, this project is currently in the preliminary design phase. However, the prototyping and testing of the platform structure has already been initiated using a small-scale design and several hardware components have been ordered. The platform will be printed using additive manufacturing due to the numerous benefits of this process. The component integration is expected to be completad in time in order to facilitate the laboratory testing of the various subsystems before the flight campaign in May 2022. After the flight campaign, the collected data will be analysed, processed and published to ensure that it is accessible to the scientific community.
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