Two degree-of-freedom spacecraft attitude controller

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Two degree-of-freedom spacecraft attitude controller

Two degree-of-freedom controller is designed together with its governing equations for a spacecraft pitch attitude control. The attitude controller incorporates the Active Force Control (AFC) technique into the conventional Proportional-Derivative (PD) controller based spacecraft pitch attitude loop...

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Bibliographic Details
Main Authors:	Varatharajoo, Renuganth, Choo, Tech Wooi, Mailah, Musa
Format:	Article
Language:	English
Published:	Elsevier 2011
Online Access:	http://psasir.upm.edu.my/id/eprint/23143/ http://psasir.upm.edu.my/id/eprint/23143/1/Two%20degree-of-freedom%20spacecraft%20attitude%20controller.pdf

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