Enhanced attitude control structure for small satellites with reaction wheels

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Enhanced attitude control structure for small satellites with reaction wheels

Attitude accuracies of a three-axis satellite are highly influenced by space environment disturbances and uncertainties. Similar to actuators, an attitude controller also plays an important role and must be robust enough to cope with any disturbances and uncertainties. Various controllers have be...

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Bibliographic Details
Main Author:	Ismail, Zuliana
Format:	Thesis
Language:	English
Published:	2019
Subjects:	Attitude control systems (Astronautics) Microspacecraft
Online Access:	http://psasir.upm.edu.my/id/eprint/98227/ http://psasir.upm.edu.my/id/eprint/98227/1/FK%202019%20159%20-%20IR.pdf

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