A prototype electrical actuator for aircraft flaps and slats

2005 IEEE International Conference on Electric Machines and Drives

Volumn , Issue , 2005, Pages 41-47

  Bennett, J W ^a   Mecrow, B C ^a   Jack, A G ^a   Atkinson, D J ^a   Sheldon, S ^d   Cooper, B ^b   Mason, G ^d   Sewell, C ^c   Cudley, D ^c  

^a NEWCASTLE UNIVERSITY   (United Kingdom)

^b FR HiTemp   (United Kingdom)

^c BAE SYSTEMS   (United Kingdom)

^d NONE

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; ELECTRIC DRIVES; HYDROELECTRIC POWER; POSITION CONTROL; POWER ELECTRONICS; SENSORS;

AIRCRAFT WING SURFACES; ELECTRICAL ACTUATION; FAULT TOLERANT MOTORS; POSITION SENSOR SYSTEMS;

ACTUATORS;

EID: 33749068695     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/iemdc.2005.195699     Document Type: Conference Paper

References (13)

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2. J.W. Bennett, A.G. Jack, B.C. Mecrow, D.J. Atkinson, C. Sewell, G.Mason, "Fault Tolerant Control Architectures for an Electrical Actuator", IEEE PESC Conference, Aarchen, 2004.
3. IEEE Recommended Practice for Reliable Industrial and Commercial Power Systems, IEEE Gold Book, ISBN 1-55937-969-3.
4. rd 1999, pp286-290.
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6. Jahns, T.M., "Improved Reliability in Solid State a.c. Drives by means of Multiple Independent Phase-Drive Units,", IEEE Trans. IAS, Vol. 16, no. 3, May 1980, pp321-331.
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