Enhanced attitude control structure for small satellites with reaction wheels

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Enhanced attitude control structure for small satellites with reaction wheels

Purpose: This paper aims to describe a design enhancement for the satellite attitude control system using reaction wheels, and the wheel momentum unloading using magnetorquers. Design/methodology/approach: The proportional – integral–derivative-controller and active force control (AFC) schemes are d...

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Bibliographic Details
Main Authors:	Ismail, Zuliana, Varatharajoo, Renuganth, Mohd Ajir, Mohd Ramly, Mohd Rafie, Azmin Shakrine
Format:	Article
Language:	English
Published:	Emerald 2015
Online Access:	http://psasir.upm.edu.my/id/eprint/44624/ http://psasir.upm.edu.my/id/eprint/44624/1/Enhanced%20attitude%20control%20structure%20for%20small%20satellites%20with%20reaction%20wheels.pdf

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