A novel design of spacecraft combined attitude & sun tracking system using a versatile fuzzy controller

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A novel design of spacecraft combined attitude & sun tracking system using a versatile fuzzy controller

Purpose – The purpose of this paper is to develop a theoretical design for the alternative attitude control of the rotation about the pitch axis for the nadir-pointing spacecraft in the event of inertial actuator faults. Design/methodology/approach – This paper presents a novel and viable solut...

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Bibliographic Details
Main Authors:	Yew, Chung Chak, Varatharajoo, Renuganth
Format:	Article
Language:	English
Published:	Emerald Group Publishing 2015
Online Access:	http://psasir.upm.edu.my/id/eprint/43535/ http://psasir.upm.edu.my/id/eprint/43535/1/abstract00.pdf

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