[6] [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] [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] [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] [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] [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] [13] XIA X.Dynamic power distribution management for all electric aircraft［D］.Cranfield:Cranfield University, 2011.

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