在小卫星反应轮中实施磁屏蔽

Q2 Engineering INCAS Bulletin Pub Date : 2024-03-11 DOI:10.13111/2066-8201.2024.16.1.11
Satriya Utama, Deddy El Amin, M. A. Saifudin, Moh. Farid Huzain, Widya Roza, C. T. Judianto, Mohammad Mukhayadi
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引用次数: 0

摘要

低地球轨道卫星面临着来自地球磁场的挑战,磁场会对卫星姿态造成干扰。实现无磁偶极子卫星至关重要。布局优化和在轨偶极子补偿是常用的方法,但布局优化可能不切实际。相比之下,在轨偶极子补偿则难以应对快速变化的磁偶极子,如反作用轮电机产生的磁偶极子。这项研究提出了一种使用缪金属(Mu-metal)的替代解决方案。这种屏蔽可用于捕捉电机产生的磁场。地面试验对这种方法进行了评估。首先,它确定了磁强计与屏蔽罩之间的最小距离,以便在干扰最小的情况下进行精确测量,结果发现 10 厘米是受影响最小的距离,这对小型卫星布局设计尤为重要。其次,它评估了屏蔽罩在捕获电机产生的磁场方面的有效性。测试表明,当电机启动时,磁场幅度明显减小,磁场波动减少达 95%。这项研究为小型卫星布局设计提供了一个实用的解决方案,解决了其紧凑尺寸带来的挑战。事实证明,μ金属屏蔽可有效缓解快速变化的磁偶极子,并提高低地球轨道的磁洁净度。
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Magnetic Shielding Implementation in the Small Satellite Reaction Wheel
Low Earth orbit satellites face challenges from Earth's magnetic field, causing attitude disturbances. Attaining a magnetic-dipole-free satellite is crucial. Layout optimization and in-orbit dipole compensation are common methods, but layout optimization can be impractical. In contrast, in-orbit dipole compensation struggles with rapidly changing magnetic dipoles like those from reaction wheel motors. This research proposes an alternative solution using Mu-metal, known for shielding against magnetic exposure. This shield can be applied to trap the magnetic field generated by the motors. Ground tests evaluated this approach. First, it determined the minimum distance between the magnetometer and the shield for accurate measurements with minimal interference, with the result of 10 cm as the least affected distance, particularly important for small satellite layout design. Second, it assessed the shield's effectiveness in trapping the motor-generated magnetic field. Tests showed a significant reduction in magnetic field magnitude and up to a 95% reduction in field fluctuations when the motor is activated. This research offers a practical solution for small satellite layout design, addressing the challenges posed by their compact dimensions. Mu-metal shielding proves effective for mitigating rapidly changing magnetic dipoles and enhancing magnetic cleanliness in low Earth orbit.
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来源期刊
INCAS Bulletin
INCAS Bulletin Engineering-Aerospace Engineering
自引率
0.00%
发文量
50
审稿时长
8 weeks
期刊介绍: INCAS BULLETIN is a scientific quartely journal published by INCAS – National Institute for Aerospace Research “Elie Carafoli” (under the aegis of The Romanian Academy) Its current focus is the aerospace field, covering fluid mechanics, aerodynamics, flight theory, aeroelasticity, structures, applied control, mechatronics, experimental aerodynamics, computational methods. All submitted papers are peer-reviewed. The journal will publish reports and short research original papers of substance. Unique features distinguishing this journal: R & D reports in aerospace sciences in Romania The INCAS BULLETIN of the National Institute for Aerospace Research "Elie Carafoli" includes the following sections: 1) FULL PAPERS. -Strength of materials, elasticity, plasticity, aeroelasticity, static and dynamic analysis of structures, vibrations and impact. -Systems, mechatronics and control in aerospace. -Materials and tribology. -Kinematics and dynamics of mechanisms, friction, lubrication. -Measurement technique. -Aeroacoustics, ventilation, wind motors. -Management in Aerospace Activities. 2) TECHNICAL-SCIENTIFIC NOTES and REPORTS. Includes: case studies, technical-scientific notes and reports on published areas. 3) INCAS NEWS. Promote and emphasise INCAS technical base and achievements. 4) BOOK REVIEWS.
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