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

منو

" 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 "

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]