Magnetic Levitation for Spherical Drag-Free Sensor Ground Testing

被引:0
|
作者
Alfauwaz, Abdulrahman [1 ]
Alhusain, Abdulaziz [2 ]
Wang, Suwen [3 ]
Lipa, John [4 ]
机构
[1] KACST, King Abdullah Rd, Riyadh, Saudi Arabia
[2] Technol Control Co, Khurais Rd,TCC Bldg, Riyadh, Saudi Arabia
[3] Hainan Trop Ocean Univ, OOIT, Sanya, Hainan, Peoples R China
[4] Stanford Univ, Dept Phys, Stanford, CA 94304 USA
关键词
D O I
10.1109/aero47225.2020.9172658
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Testing drag-free proof mass systems for gravitational physics requires a ground test system that simulates space conditions as closely as possible. In this experiment, a magnetic levitation system was built, which can levitate, hold, and spin a hollow sphere in a vacuum to simulate operations in a zero-G environment. An optical shadow sensor consisting of an infrared emitter and a pair of photodiodes is used to determine the position of the sphere. A custom-made electronic board converts the analog signal to digital. The board has a switch to reverse the current direction through the coil in case the sphere becomes magnetized and is attracted to the coil in the vacuum. Digital control code has been developed to create a stable feedback control system to drive the coil and hold the sphere in a stable levitating position. The position of the sphere can be adjusted digitally. The system is designed to achieve initial levitation and to restore the sphere to its levitating position if it drops out of lock. COMSOL Multiphysics[1] was used for thermal and magnetic simulation and system analysis. Importantly, the heat generated by the coil is not easily dissipated in the vacuum. The design is optimized to ensure that the coil can be run for at least two hours without overheating. The sphere is spun using four coils driven by digitally generated sine and cosine functions to produce a rotating magnetic field around its equator. Operation up to 18 Hz is easily achieved. The system can be used to test the three-axis optical sensor system Differential Optical Shadow Sensor (DOSS)[2], which is being developed separately, by rapidly switching to the DOSS sensor while the sphere is levitating. Small magnetic pulses can also be used to simulate thruster perturbations in the plane orthogonal to the support axis.
引用
收藏
页数:7
相关论文
共 50 条
  • [21] Development of hardware for a drag-free control system
    Leach, R
    GRAVITATIONAL-WAVE DETECTION, 2003, 4856 : 19 - 30
  • [22] Hydrodynamic Metamaterial Cloak for Drag-Free Flow
    Park, Juhyuk
    Youn, Jae Ryoun
    Song, Young Seok
    PHYSICAL REVIEW LETTERS, 2019, 123 (07)
  • [23] Drag-free control concepts for the step mission
    Schleicher, A
    Theil, S
    PROCEEDINGS OF THE 5TH ESA INTERNATIONAL CONFERENCE ON SPACECRAFT GUIDANCE, NAVIGATION AND CONTROL SYSTEMS, 2003, 516 : 595 - 598
  • [24] Drag-free and attitude control for the GOCE satellite
    Canuto, Enrico
    AUTOMATICA, 2008, 44 (07) : 1766 - 1780
  • [25] Position sensors for LISA drag-free control
    Weber, WJ
    Cavalleri, A
    Dolesi, R
    Fontana, G
    Hueller, M
    Vitale, S
    CLASSICAL AND QUANTUM GRAVITY, 2002, 19 (07) : 1751 - 1756
  • [26] Quantum fluctuations for drag-free geodesic motion
    Courty, JM
    Reynaud, S
    JOURNAL OF OPTICS B-QUANTUM AND SEMICLASSICAL OPTICS, 2000, 2 (02) : 90 - 93
  • [27] Drag-free and attitude control for the GOCE satellite
    Andreis, Davide
    Canuto, Enrico S.
    2005 44TH IEEE CONFERENCE ON DECISION AND CONTROL & EUROPEAN CONTROL CONFERENCE, VOLS 1-8, 2005, : 4041 - 4046
  • [28] ANALYTICAL MODELING OF MOTION OF A DRAG-FREE SATELLITE
    CLOCHET, A
    PAITEL, F
    RECHERCHE AEROSPATIALE, 1977, (03): : 139 - 146
  • [29] A 2-DOF drag-free control ground simulation system based on Stewart platform
    Lin, Jueqi
    Lian, Junxiang
    Zhao, Guoying
    Li, Hongyin
    Xu, Chi
    ISA TRANSACTIONS, 2024, 146 : 528 - 540
  • [30] In-orbit identification of drag-free satellite dynamics
    Leite, Waldemar de Castro
    Theil, Stephan
    Guilherme, Michel Silas
    SPACEFLIGHT MECHANICS 2006, VOL 124, PTS 1 AND 2, 2006, 124 : 613 - 631