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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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Main Authors: Varatharajoo, Renuganth, Alkhodari, Saleh Basha
Format: Article
Language:English
English
Published: 2011
Online Access:http://psasir.upm.edu.my/id/eprint/23356/1/Attitude%20Control%20Augmentation%20for%20Combined%20Attitude%20and%20Thermal%20Control%20System.pdf
http://psasir.upm.edu.my/id/eprint/23356/
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spelling my.upm.eprints.233562015-10-07T04:36:29Z http://psasir.upm.edu.my/id/eprint/23356/ Attitude Control Augmentation for Combined Attitude and Thermal Control System. Varatharajoo, Renuganth Alkhodari, Saleh Basha 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 equations are established and the proposed attitude control architecture is made amenable to numerical treatments. The result shows an important attitude pointing enhancement using the AFC technique in CATCS. 2011 Article PeerReviewed application/pdf en http://psasir.upm.edu.my/id/eprint/23356/1/Attitude%20Control%20Augmentation%20for%20Combined%20Attitude%20and%20Thermal%20Control%20System.pdf Varatharajoo, Renuganth and Alkhodari, Saleh Basha (2011) Attitude Control Augmentation for Combined Attitude and Thermal Control System. International Review of Mechanical Engineering, 5 (6). pp. 1139-1143. ISSN 1970-8734 English
institution Universiti Putra Malaysia
building UPM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Putra Malaysia
content_source UPM Institutional Repository
url_provider http://psasir.upm.edu.my/
language English
English
description 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 equations are established and the proposed attitude control architecture is made amenable to numerical treatments. The result shows an important attitude pointing enhancement using the AFC technique in CATCS.
format Article
author Varatharajoo, Renuganth
Alkhodari, Saleh Basha
spellingShingle Varatharajoo, Renuganth
Alkhodari, Saleh Basha
Attitude Control Augmentation for Combined Attitude and Thermal Control System.
author_facet Varatharajoo, Renuganth
Alkhodari, Saleh Basha
author_sort Varatharajoo, Renuganth
title Attitude Control Augmentation for Combined Attitude and Thermal Control System.
title_short Attitude Control Augmentation for Combined Attitude and Thermal Control System.
title_full Attitude Control Augmentation for Combined Attitude and Thermal Control System.
title_fullStr Attitude Control Augmentation for Combined Attitude and Thermal Control System.
title_full_unstemmed Attitude Control Augmentation for Combined Attitude and Thermal Control System.
title_sort attitude control augmentation for combined attitude and thermal control system.
publishDate 2011
url http://psasir.upm.edu.my/id/eprint/23356/1/Attitude%20Control%20Augmentation%20for%20Combined%20Attitude%20and%20Thermal%20Control%20System.pdf
http://psasir.upm.edu.my/id/eprint/23356/
_version_ 1643828033807712256
score 13.160551

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