• Electronics Optics & Control
  • Vol. 24, Issue 9, 88 (2017)
XU Ke-lu1, XIE Ning1, WANG Cheng-min1, and SHI Xu-dong2
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2017.09.019 Cite this Article
    XU Ke-lu, XIE Ning, WANG Cheng-min, SHI Xu-dong. Modeling and Simulation of More Electric Aircraft VSVF Power System[J]. Electronics Optics & Control, 2017, 24(9): 88 Copy Citation Text show less
    References

    [6] WU T,BOZHKO S V,ASHER G M,et al.A fast dynamic phasor model of autotransformer rectifier unit for more electric aircraft[C]//Industrial Electronics,35th Annual Conference of IEEE,2009:2531-2536.

    [7] GRIFFO A,WANG J B.Modeling and stability analysis of hybrid power systems for the more electric aircraft [J].Electric Power Systems Research,2012,82(1):59-67.

    [8] EID A,EL-KISHKY H,ABDEL-SALAM M,et al.Modeling and characterization of an aircraft electric power system with a fuel cell-equipped APU paralleled at main AC bus[C]//Power Modulator and High Voltage Confe-rence,2010:891-904.

    [9] EID A,EL-KISHKY H,ABDEL-SALAM M,et al.Modeling and characterization of an aircraft electric power system with a fuel cell-equipped APU connected at HVDC bus[C]//Power Modulator and High Voltage Conference, 2010:639-642.

    [11] HAN L,WANG J,HOWE D.State-space average modelling of 6-and 12-pulse diode rectifiers[C]//European Confe-rence on Power Electronics and Applications,2007:1-10.

    [13] XIA X.Dynamic power distribution management for all electric aircraft[D].Cranfield:Cranfield University, 2011.

    [14] Department of Defense Interface Standard.MIL-STD-704F Aircraft electric power characteristic [S].[s.l.]:DOD, 2004.

    XU Ke-lu, XIE Ning, WANG Cheng-min, SHI Xu-dong. Modeling and Simulation of More Electric Aircraft VSVF Power System[J]. Electronics Optics & Control, 2017, 24(9): 88
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