Fault diagnosis in spacecraft attitude control system

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 considered actuator is assumed to be a reaction wheel. Since the attitude model of the spacecraft to be used is a coupled three-axis, t...

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Bibliographic Details
Main Author: Azarnoush, Hamed
Format: Others
Published: 2005
Online Access:http://spectrum.library.concordia.ca/8663/1/MR10232.pdf
Azarnoush, Hamed <http://spectrum.library.concordia.ca/view/creators/Azarnoush=3AHamed=3A=3A.html> (2005) Fault diagnosis in spacecraft attitude control system. Masters thesis, Concordia University.