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交叉重组方法在帆板驱动线路中的应用研究

Study of the cross recombination method used in solar array drive electronics
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摘要 帆板驱动线路(SADE:Solar Array Drive Electronics)和电机绕组的连接通常是固定的,即驱动线路的主备份分别连接电机绕组的主备份。原理上看,主备份线路是相互独立的,但考虑主备份电机绕组是并绕模式,工作的电机绕组会通过电磁耦合施加电应力到非工作线路,从而对非通电器件产生应力冲击,影响整机性能。本文通过在驱动线路和绕组间引入交叉重组设计,解决了主备份驱动线路之间的耦合影响,大大提高了可靠性。 Solar Array and motor coils is usually fixed together.That is to say,the main backup of the drive electronics respectively connected to the main backup of the motor coils.In principle,the main and the backup circuit are separated between each other.But the mode of the main backup coils is parallel wound.The working motor coils will exert electric stress to non-working coils by electromagnetic coupling.That will produce stress to the non-powed components,and impact the performance of the drive electronics.In this paper,we design cross recombinations between the array driving circuit and motor coils,which can eliminate the electromagnetic coupling effects between the main and the backup circuit,and greatly improve the reliability.
出处 《电子设计工程》 2014年第3期178-180,共3页 Electronic Design Engineering
关键词 帆板驱动线路 电磁耦合 交叉重组 可靠性 SADE electromagnetic coupling cross recombinations reliability
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  • 1[2]陈德顺,王常先等译.国际通讯卫星V.北京:国防工业出版社,1982.99-102
  • 2[3]Granzow M. Mechanisms for Communications Satellites. Proc. ESA Sym. Sat. Broadc., 1976,Stockholm, 181-186
  • 3[4]Cab'illic J. Design aspects of a solar array drive for SPOT with a high platform stability objective.Proc. 16th Aeros. Mech. Sym., Kennedy Space Center, USA, 1982, 143-157
  • 4[5]TELDIX GmbH. Solar Array Drive Mechanism and Solar Array Drive Electronics for DFH-3. Technical and Management Proposal. 1987
  • 5[6]Cab'illic J. Design considerationon the solar array drive mechanism developed for SPOT. Proc. second Space Trib. Work. ESTL Risley U K, 1980, 39-42
  • 6吴凤江 高晗璎 孙力.桥式拓扑结构功率MOSFET驱动电路设计[J].哈尔滨工业大学学报,2002,43(2):20-25.
  • 7Application Note AN - 978 about HV Floating MOS - Gate Driver ICs, 2002.
  • 8高星.卫星姿态动力学与控制(4)[M].北京:中国宇航出版社,2006.
  • 9Chretien J P, Reboulet C, Rodrigo P, et al. Attitude control of a satellite with a rotating solar array [ J ]. Jour-nal of Guidance, 1982(5) : 589-596.
  • 10Doherty M J, Tolson R I-I. Input shaping to reduce solar array structural vibrations [ R ]. NASA/CR-1998- 208698, 1998.

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