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混合式MPPT星载电源系统拓扑设计与仿真分析 被引量：4

Design and Simulation of a Mixed MPPT Electrical Power System Topology
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摘要 为适应低轨道卫星、深空探测器等航天器的应用需求,本文提出采用一种新型串并联混合式峰值功率点跟踪(Maximum Power Point Tracking,MPPT)电路拓扑结构,控制算法采用增量电导法,以保证太阳电池阵工作在峰值功率点附近,充分利用太阳电池阵输出功率。文章重点介绍了新型串并联混合式MPPT电路拓扑的四种工作模式、两域控制方法和增量电导法的MPPT控制策略的实现,并搭建MPPT系统仿真平台,仿真验证结果表明,串并联MPPT拓扑结构能够快速、无扰动实现太阳电池阵峰值功率点跟踪。 Maximum Power Point Tracking（MPPT）control is especially suitable for high-power LEO spacecraft and deep-space spacecraft whose light intensity received and temperature variation are in a wide range.A new series-parallel mixed MPPT electrical power system topology is proposed in the paper,in which the control strategy uses increment-conductance method to trace the maximum power point and make full use of the output electrical power of the solar array.Details are presented in the paper,including four modes for the new circuit topology,two-area control and increment-conductance control implementations.The system simulation platform is built and some experiments and analysis are processed.The outcomes show that the new power topology can quickly trace the solar array maximum power point.
作者 蔡晓东 刘治钢 张明 林文立
机构地区 北京空间飞行器总体设计部
出处 《航天器工程》 2013年第3期77-82,共6页 Spacecraft Engineering
关键词 峰值点功率跟踪 串并联拓扑 MPPT两域控制 MPPT series-parallel mixed topology MPPT two-area control
分类号 V442 [航空宇航科学与技术—飞行器设计]
  • 相关文献

参考文献10

  • 1马世俊.卫星电源技术[M]北京:宇航出版社,2001236-240.
  • 2Lempereur V,Jauquet D,Liegeois B. Power conditioning and distribution unit of Globalstar-2 constellation[A].Paris:ESA,2008.119-125.
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二级参考文献12

  • 1Maset E,Sanchis-Kilders E,Weinberg A H.Ion drivepropulsion MPP power conditioning system withoutbattery. Proceedings of the8th European SpacePower Conference . 2008
  • 2Garrigos A,Blanes J M,Carrasco J A,et al.Maximumpower point tracking for GEO telecommunication satel-lites. Proceedings of the8th European Space PowerConference . 2008
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  • 4Jensen H,Laursen J.Power conditioning unit for Rosetta/Mars Express. Proceedings of the6th European SpacePower Conference . 2002
  • 5Loche D.Mars Express and Venus Express power sub-system in-flight behaviour. Proceedings of the8th Eu-ropean Space Power Conference . 2008
  • 6Luca A D,Gray R,Otero J.The LISA Pathfinderpower system. Proceedings of the8th EuropeanSpace Power Conference . 2008
  • 7Lempereur V,Jauquet D,Liegeois B.Power condition-ing and distribution unit of Globalstar-2constellation. Proceedings of the8th European Space PowerConference . 2008
  • 8Santoni F,Piergentili F.Design and test of a maximumpower point tracking system for UNISAT-3microsatel-lite. Proceedings of the55th International Astronau-tical Congress . 2004
  • 9Breier N,Kiewe B,Mourra O.The power control anddistribution unit for the SWARM satellites. Pro-ceedings of the8th European Space Power Conference . 2008
  • 10H. Fiebrich,J. E. Haines,F. Tonicello.Power System Design of the Rosetta Spacecraft. . 2004

共引文献19

同被引文献28

  • 1王宇宾,常鲜戎,罗艳,马瑞军.基于隐式Taylor级数法的电力系统暂态稳定计算[J].华北电力大学学报（自然科学版）,2005,32(2):1-6. 被引量：13
  • 2ANTOINE C, ROBERTO G. MPPC regulated bus power system management for LEO and GEO missions [C]// Proceedings of the 8th European Space Power Conference, Paris, ESA, 2008: 1-11.
  • 3DAKERMANJI G, PERSON C, JENKINS J. The MESSENGER spacecraft power system design and early mission performance [C]//Proceedings of the 7th European Space Power Conference, Paris, ESA, 2005: 1-8.
  • 4USMAN L, SHAKEEL B. Stability study of spacecraft electrical power system with constant-power loads [C]//Proeeedings of the 14th International Multitopic Conference, IEEE, 2011: 217-221.
  • 5LUCIANO C, PAOLO D, ALBERTO L. Maximum power point tracker point controller for unregulated bus architecture [C]//Proceedings of the 7th European Space Power Conference, Paris, ESA, 2005: 1-6.
  • 6KAMIAR J, ANDREW J, ALVIN C. Verification of Space Station secondary power system stability using design of experiment [C] // Proceedings of the 32nd Intersociety Energy Conversion Engineering Conference, Hawaii, AIAA, 1997: 1-6.
  • 7VALDIVIA V, BARRADO A, LAZARO A. Analysis of dynamic interactions between solar array simulators and spacecraft power conditioning and distribution units [C] // Proceedings of the 9th European Space Power Conference, Saint Raphael, ESA, 2011: 1-8.
  • 8FERNANDEZ A, TONICELLO F, AROCA J, et al. Battery discharge regulator for space applications based on the boost converter [C] // Proceedings of the 25th IEEE Applied Power Electronics Conference and Exposition (APEC), Noordwijk, Netherland, 2010: 1792-1799.
  • 9O GARCIA, P ALOU, J OLIVER, et al. Boost-based MPPT converter topology trade-off for space applications [C]//Proceedings of the 8th European Space Power Conference, Paris, ESA, 2008: 1-7.
  • 10JENSEN H. Power conditioning unit for BepiColombo transfer module [C] // Proceedings of the 8th European Space Power Conference, Paris, ESA, 2008: 1-6.

引证文献4

二级引证文献11

航天器工程
2013年 第3期

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