Direct drive permanent magnet generator fed AC-DC active rectification and control for more-electric aircraft engines

IET Electric Power Applications

Volumn 5, Issue 1, 2011, Pages 14-27

  Fernando, W U N ^a   Barnes, M ^a   Marjanovic, O ^a  

^a UNIVERSITY OF MANCHESTER   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL ALGORITHMS; CONTROL OBJECTIVES; CONTROLLER GAIN; COPPER LOSS; DC DISTRIBUTION; DC LINK VOLTAGE REGULATION; DC VOLTAGE REGULATION; DIRECT DRIVE; ELECTRICAL POWER GENERATION; FAULT-TOLERANT; GENERATOR LOAD; INPUT/OUTPUT STABILITY; LOAD SHARING CONTROL; MORE ELECTRIC AIRCRAFT; NOVEL ALGORITHM; OPERATIONAL CAPABILITIES; PERMANENT MAGNET GENERATOR; PHASE ANGLE CONTROL; UNBALANCED OPERATIONS; VARIABLE SPEED;

AC GENERATOR MOTORS; AIRCRAFT CONTROL; AIRCRAFT ENGINES; ALGORITHMS; BEHAVIORAL RESEARCH; CONTROLLERS; DC POWER TRANSMISSION; ELECTRIC CURRENT REGULATORS; ELECTRIC GENERATORS; JET ENGINES; MAGNETIC DEVICES; PERMANENT MAGNETS; REACTIVE POWER; VOLTAGE CONTROL; VOLTAGE REGULATORS;

ELECTRIC RECTIFIERS;

EID: 79551595150     PISSN: 17518660     EISSN: 17518679     Source Type: Journal    
DOI: 10.1049/iet-epa.2009.0280     Document Type: Article

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