Attitude Control Augmentation for Combined Attitude and Thermal Control System.

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Attitude Control Augmentation for Combined Attitude and Thermal Control System.

An approach that incorporates the Active Force Control (AFC) technique into a conventional Proportional-Derivative (PD) controller is proposed for spacecraft attitude controls. The combined attitude and thermal control system (CATCS) is proposed as an attitude control actuator. All the governing equ...

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Bibliographic Details
Main Authors:	Varatharajoo, Renuganth, Alkhodari, Saleh Basha
Format:	Article
Language:	English English
Published:	2011
Online Access:	http://psasir.upm.edu.my/id/eprint/23356/ http://psasir.upm.edu.my/id/eprint/23356/1/Attitude%20Control%20Augmentation%20for%20Combined%20Attitude%20and%20Thermal%20Control%20System.pdf

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