Resource type
Thesis type
(Thesis) M.A.Sc.
Date created
2006
Authors/Contributors
Author: Jia, Guangqing
Abstract
In this work, the actuator fault isolation problem for the aircraft is investigated. An adaptive observer and sliding mode observer were chosen for fault diagnosis purpose.
Document
Copyright statement
Copyright is held by the author.
Scholarly level
Language
English
Member of collection
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