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Document Type : Latin Dissertation
Language of Document : English
Record Number : 154942
Doc. No : ET26734
Main Entry : Guangqing Jia
Title Proper : ADAPTIVE OBSERVER AND SLIDING MODE OBSERVER BASED ACTUATOR FAULT DIAGNOSIS FOR CIVIL AIRCRAFTET C A L I B ~ RIQUEMENTET C A L I B ~RIQUEMENT.POMPES PAR TRANSITIONS MULTIPLES
Note : This document is digital این مدرک بصورت الکترونیکی می باشد
Abstract : Aircraft modelling based on Research Civil Aircraft Model (RCAM) is first introducedin this work. The actuator fault isolation problem for the aircraft is then investigated.An adaptive observers (AO) and a sliding mode observers (SMO), were chosen forfault diagnosis purposes. An adaptive scheme based on a bank of AOs is designed todetect and isolate constant actuator faults. Theoretical results are obtained.
Subject : Electericl tess
: برق
electronic file name : TL51009.pdf
Title and statement of responsibility and : ADAPTIVE OBSERVER AND SLIDING MODE OBSERVER BASED ACTUATOR FAULT DIAGNOSIS FOR CIVIL AIRCRAFTET C A L I B ~ RIQUEMENTET C A L I B ~RIQUEMENT.POMPES PAR TRANSITIONS MULTIPLES [Thesis]
 
 
 
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