Evaluation of Reduction in the Performance of a Small UAV After an Aileron Failure for an Adaptive Guidance System

After an actuator failure, the performance of an aircraft is degraded. If a fault detection and isolation system is available in the flight control system, the knowledge of the failure can be used to evaluate the new aircraft performance. Based thereon, a supervision system decides whether the missi...

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Bibliographic Details

Published in:	2007 American Control Conference pp. 1793 - 1798
Main Authors:	Ducard, G., Kulling, K.C., Geering, H.P.
Format:	Conference Proceeding
Language:	English
Published:	IEEE 01.07.2007
Subjects:	Actuators Adaptive control Adaptive systems Aerospace control Aircraft Airplanes Base stations Degradation Fault detection Unmanned aerial vehicles
ISBN:	9781424409884, 1424409888
ISSN:	0743-1619
Online Access:	Get full text
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