Design and Construction of a Magnetic Field Simulator for CubeSat Attitude Control Testing
A real time, three axis space magnetic field simulator, developed using only commercial off the shelf components, is described in this paper. It is a complete and independent system to be used for the ground testing of nanosatellites, allowing automated magnetic attitude control systems to be verified. The main aim of this simulator is to reproduce magnetic field conditions in orbit with low cost mechanical and electronic designs. The system is capable of creating a region of uniform, directed magnetic field on command for nanosatellite ground testing.
X.-W. Zhou, C. T. Russell and G. Le, “Comparison of observed and model magnetic fields at high altitudes above the polar cap: Polar initial results”, Geophysical Research Letters, Vol,24, No, 12, 1997, pp 1451-1454.
MacIntyre Electronic Design Associates (MEDA), “HCS01CL with gradient coils operation and maintenance Manual”, 2007.
K. Grossekatthoefer and C. Raschke, “Support of ACS development and test by dynamic simulation models”, 8th IAA Symposium on Small Satellites for Earth Observation, 2011.
F. M. Poppenk, R. Amini, G. F. Brouwer, “Design and application of a Helmholtz cage for testing nano-satellites”, 6th International Symposium on Environmental Testing for Space Programmes, Noordwijk, The Netherlands, 2007.
A. Klesh, S. Seagraves, M. Bennett, D. Boone, H. Bahcivan, J. Cutler, “Dynamically driven helmholtz cage for experimental magnetic attitude determination”, AAS/AIAA Astrodynamics Specialist Conference, Pittsburgh, PA, 2009.
B. Asokan, “Development of an in orbit simulator for nanosatellites”, Master of Science Thesis at Lulea University of Technology, 2012.
M. Pastena, L. Sorrentino, and M. Grassi, Design and validation of the university of naples space magnetic field simulator (SMAFIS), Journal Institute of Environmental Sciences and Technology Vol, 44 , No, 1, 2001, pp 3342.
M. R. Brewer, “CubeSat attitude determination and helmholtz cage design”, Master of Science Thesis at Air Force Institute of Technology, 2012.
F. Piergentili, G. P., Candini, and M. Zannoni, “Design, manufacturing, and test of a real-time, three-Axis magnetic field simulator” , IEEE Transactions on Aerospace and Electronics Systems, Vol,47, No, 2, 2011, pp 1369- 1379.
Pastena, M. and Grassi, M., “Optimum design of a three-axis magnetic field simulator”, IEEE Transactions on Aerospace and Electronics Systems, Vol,38, No, 2, 2002, pp 488- 501.
K. P. Ryan, “Experimental testing of the accuracy of attitude determination solutions for a spin stabilized spacecraft”, Master of Science Thesis, Utah State University 2011.
G. Grandi, and M. Landini, “Magnetic-field transducer based on closed loop operation of magnetic sensors”, IEEE Transactions on Industrial Electronics, Vol. 53, No. 3, 2006, pp 880-885.
F. te Hennepe, B. T. C. Zandbergen, and R. J. Hamann, “Simulation of the attitude behaviour and available power profile of the Delfi-c3 spacecraft with application of the opsim platform”, 1st CEAS European Air and Space Conference, 2007.
N. Sugimura, K. Fukuda, Y. Tomioka, M. Fukuyama, Y. Sakamoto, T. Kuwahara, T. Fukuhara, K. Yoshida, Y. Takahashi, “Ground test of attitude control system for micro satellite RISING-2”, 2012 IEEE/SICE International Symposium on System Integration (SII), Japan, December 2012.
T. T. Li, “Tri-axial Square Helmholtz coil for neutron EDM experiment”, www.phy.cuhk.edu.hk, 2004.
William M. Frix, George G. Karady, Brian A. Venetz. “Comparison of calibration system for magnetic field measurement equipment”. IEEE Transactions on Power Delivery, Vol. 9, No. 1, January 1994.
W.-S. Lee, W.-I. Son, K.-S. Oh, and J.-W. Yu, “Contactless energy transfer systems using antiparallel resonant loops”, IEEE Transactions on Industrial Electronics, Vol. 60, No. 1, 2013, pp 350-359.
S. R. Trout, “Use of Helmholtz coils for magnetic measurements”, IEEE Transactions on Magnetics, Vol. 24, No. 4, 1988, pp 2108-2111.
F. Van der Pijl, P. Bauer, M. Castilla, “Control method for wireless inductive energy transfer systems with relatively large air gap”, IEEE Transactions on Industrial Electronics, Vol. 60, No. 1, 2013, pp 382-388.
M.-Y. Chen, T.-B. Lin, S.-K. Hung, L.-C. Fu, “Design and experiment of a macro-micro planar maglev positioning system”, IEEE Transactions on Industrial Electronics, Vol, 59, No. 11, 2012, pp 4128-4139.
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