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Verification of the Microgravity Active Vibration Isolation System based on Parabolic Flight

机译:基于抛物线飞行的微重力主动隔振系统验证

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摘要

The Microgravity active vibration isolation system (MAIS) is a device to reduce on-orbit vibration and to provide a lower gravity level for certain scientific experiments. MAIS system is made up of a stator and a floater, the stator is fixed on the spacecraft, and the floater is suspended by electromagnetic force so as to reduce the vibration from the stator. The system has 3 position sensors, 3 accelerometers, 8 Lorentz actuators, signal processing circuits and a central controller embedded in the operating software and control algorithms. For the experiments on parabolic flights, a laptop is added to MAIS for monitoring and operation, and a power module is for electric power converting. The principle of MAIS is as follows: the system samples the vibration acceleration of the floater from accelerometers, measures the displacement between stator and floater from position sensitive detectors, and computes Lorentz force current for each actuator so as to eliminate the vibration of the scientific payload, and meanwhile to avoid crashing between the stator and the floater. This is a motion control technic in 6 degrees of freedom (6-DOF) and its function could only be verified in a microgravity environment. Thanks for DLR and Novespace, we get a chance to take the DLR 27th parabolic flight campaign to make experiments to verify the 6-DOF control technic. The experiment results validate that the 6-DOF motion control technique is effective, and vibration isolation performance perfectly matches what we expected based on theoretical analysis and simulation. The MAIS has been planned on Chinese manned spacecraft for many microgravity scientific experiments, and the verification on parabolic flights is very important for its following mission. Additionally, we also test some additional function by microgravity electromagnetic suspension, such as automatic catching and locking and working in fault mode. The parabolic flight produces much useful data for these experiments.
机译:微重力主动隔振系统(MAIS)是一种减少在轨振动并为某些科学实验提供较低重力水平的装置。 MAIS系统由定子和浮子组成,定子固定在航天器上,浮子通过电磁力悬挂,以减少定子的振动。该系统具有3个位置传感器,3个加速度计,8个洛伦兹执行器,信号处理电路以及嵌入在操作软件和控制算法中的中央控制器。为了进行抛物线飞行实验,向MAIS添加了便携式计算机以进行监视和操作,电源模块用于电力转换。 MAIS的原理如下:系统从加速度计采样浮子的振动加速度,从位置敏感探测器测量定子和浮子之间的位移,并计算每个执行器的洛伦兹力电流,以消除科学有效载荷的振动,同时避免定子和浮子之间的碰撞。这是6自由度(6-DOF)的运动控制技术,其功能只能在微重力环境中进行验证。感谢DLR和Novespace,我们有机会参加DLR 27抛物线飞行运动,进行实验以验证6自由度控制技术。实验结果证明了六自由度运动控制技术是有效的,并且隔振性能与理论分析和仿真所期望的完全吻合。 MAIS已计划在中国载人飞船上进行许多微重力科学实验,而抛物线飞行的验证对其后续任务非常重要。此外,我们还通过微重力电磁悬挂测试了一些附加功能,例如自动捕捉和锁定以及在故障模式下工作。抛物线飞行为这些实验提供了许多有用的数据。

著录项

  • 来源
    《Microgravity science and technology》 |2017年第6期|415-426|共12页
  • 作者单位

    Chinese Acad Sci, Technol & Engn Ctr Space Utilizat, Key Lab Space Utilizat, Beijing 100094, Peoples R China;

    Chinese Acad Sci, Technol & Engn Ctr Space Utilizat, Key Lab Space Utilizat, Beijing 100094, Peoples R China;

    Chinese Acad Sci, Technol & Engn Ctr Space Utilizat, Key Lab Space Utilizat, Beijing 100094, Peoples R China;

    Chinese Acad Sci, Technol & Engn Ctr Space Utilizat, Key Lab Space Utilizat, Beijing 100094, Peoples R China;

    Chinese Acad Sci, Technol & Engn Ctr Space Utilizat, Key Lab Space Utilizat, Beijing 100094, Peoples R China;

    Chinese Acad Sci, Technol & Engn Ctr Space Utilizat, Key Lab Space Utilizat, Beijing 100094, Peoples R China;

    Chinese Acad Sci, Technol & Engn Ctr Space Utilizat, Key Lab Space Utilizat, Beijing 100094, Peoples R China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Microgravity; Vibration isolation; Parabolic flights;

    机译:微重力;隔振;抛物线飞行;

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