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Volumn 2, Issue , 2003, Pages 1321-1327
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The impact of matrix converter technology on motor design for an integrated flight control surface actuation system
a a a a a a a a a b b |
Author keywords
Aerospace control; Aircraft; Commutation; Current supplies; Drives; Electric motors; Energy storage; Load flow; Matrix converters; Voltage
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Indexed keywords
AIRCRAFT;
AIRCRAFT CONTROL;
CONTROL SURFACES;
DISTRIBUTED COMPUTER SYSTEMS;
DRIVES;
ELECTRIC COMMUTATION;
ELECTRIC DRIVES;
ELECTRIC LOAD FLOW;
ELECTRIC MACHINERY;
ELECTRIC MOTORS;
ELECTRIC POTENTIAL;
ENERGY STORAGE;
FIGHTER AIRCRAFT;
FLIGHT CONTROL SYSTEMS;
MATRIX CONVERTERS;
AEROSPACE CONTROL;
CURRENT SUPPLIES;
FLIGHT CONTROL SURFACE;
INTEGRATED ELECTRIC MOTORS;
LOAD FLOW;
MATRIX CONVERTER TECHNOLOGY;
MORE ELECTRIC AIRCRAFT;
SUPPLY CURRENT HARMONICS;
ELECTRIC MACHINE CONTROL;
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EID: 77951626133
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: 10.1109/IEMDC.2003.1210410 Document Type: Conference Paper |
Times cited : (9)
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References (9)
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