|
Volumn , Issue 538 CP, 2008, Pages 245-249
|
Compact direct-drive permanent magnet motor for a UAV rotorcraft with improved faulted behaviour through operation as four separate three-phase machines
|
Author keywords
Fault tolerant machine; More electric aircraft; PM motor; Rotorcraft UAV
|
Indexed keywords
APPLICATION REQUIREMENTS;
DIRECT DRIVE;
FAULT SCENARIOS;
FAULT TOLERANT MACHINE;
FAULT-TOLERANT;
FINITE ELEMENT ANALYSIS;
HIGH TORQUE;
MORE ELECTRIC AIRCRAFT;
PERMANENT MAGNET MOTOR;
PM MOTOR;
PROTOTYPE TESTING;
ROTOR BLADES;
ROTOR WINGS;
ROTORCRAFT UAV;
TARGET APPLICATION;
THREE-PHASE MACHINES;
TORQUE RIPPLES;
DRIVES;
ELECTRIC MOTORS;
MACHINE WINDINGS;
PERMANENT MAGNETS;
POWER ELECTRONICS;
QUALITY ASSURANCE;
UNMANNED AERIAL VEHICLES (UAV);
WINDING;
FAULT TOLERANCE;
|
EID: 67449085612
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: 10.1049/cp:20080520 Document Type: Conference Paper |
Times cited : (14)
|
References (6)
|