Fault Diagnosis in Spacecraft Attitude Control System.POMPES PAR TRANSITIONS MULTIPLES

منو

" Fault Diagnosis in Spacecraft Attitude Control System.POMPES PAR TRANSITIONS MULTIPLES "

Document Type	:	Latin Dissertation
Language of Document	:	English
Record Number	:	154268
Doc. No	:	ET26060
Main Entry	:	Hamed Azarnoush
Title Proper	:	Fault Diagnosis in Spacecraft Attitude Control System.POMPES PAR TRANSITIONS MULTIPLES
Note	:	This document is digital این مدرک بصورت الکترونیکی می باشد
Abstract	:	This thesis presents a method for fault diagnosis in spacecraft attitude control system.The focus of this diagnosis problem will be on the actuator components. The consideredactuator is assumed to be a reaction wheel. Since the attitude model of the spacecraft to.
Subject	:	Electericl tess
	:	برق
electronic file name	:	TL50333.pdf
Title and statement of responsibility and	:	Fault Diagnosis in Spacecraft Attitude Control System.POMPES PAR TRANSITIONS MULTIPLES [Thesis]