Testing and validation of a Β; algorithm for cubesat satellites

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Testing and validation of a Β; algorithm for cubesat satellites

For most satellite missions, it is essential to decrease the satellite angular velocity. The Β algorithm is a common algorithm to stabilize the spacecraft by using magnetorquers. Controlling the satellite using the magnetorquers is part of the attitude control subsystem detumbling mode. Due to...

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Bibliographic Details
Main Authors:	Bottcher, M., Eshghi, S., Varatharajoo, Renuganth
Format:	Article
Language:	English
Published:	Institute of Physics Publishing 2016
Online Access:	http://psasir.upm.edu.my/id/eprint/52941/ http://psasir.upm.edu.my/id/eprint/52941/1/article.pdf

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