Attitude pointing enhancement for combined energy and attitude control system

This paper extends the previous works that appeared in Acta Astronautica. An approach that incorporates the Active Force Control (AFC) technique into a conventional Proportional-Derivative (PD) controller is proposed for a 50 kg small satellite. Numerical treatments are performed to validate the eff...

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Bibliographic Details
Main Authors: Varatharajoo, Renuganth, Choo, Tech Wooi, Mailah, Musa
Format: Article
Published: Elsevier Limited 2011
Subjects:
Online Access:http://eprints.utm.my/id/eprint/28847/
http://dx.doi.org/10.1016/j.actaastro.2010.11.006
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