Cover Image

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...

Full description

Saved in:
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/23142/1/Attitude%20pointing%20enhancement%20for%20combined%20energy%20and%20attitude%20control%20system.pdf
http://psasir.upm.edu.my/id/eprint/23142/
Tags: Add Tag
No Tags, Be the first to tag this record!
id my.upm.eprints.23142
record_format eprints
spelling my.upm.eprints.231422015-12-07T03:15:26Z http://psasir.upm.edu.my/id/eprint/23142/ Attitude pointing enhancement for combined energy and attitude control system Varatharajoo, Renuganth Choo, Tech Wooi Mailah, Musa 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 effectiveness of AFC. The attitude control capability of the combined energy and attitude control system (CEACS) is expected to improve. The result shows an important attitude pointing enhancement for the CEACS attitude control task. Elsevier 2011-06 Article PeerReviewed application/pdf en http://psasir.upm.edu.my/id/eprint/23142/1/Attitude%20pointing%20enhancement%20for%20combined%20energy%20and%20attitude%20control%20system.pdf Varatharajoo, Renuganth and Choo, Tech Wooi and Mailah, Musa (2011) Attitude pointing enhancement for combined energy and attitude control system. Acta Astronautica, 68 (11-12). pp. 2025-2028. ISSN 0094-5765; ESSN: 1879-2030 10.1016/j.actaastro.2010.11.006
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
description 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 effectiveness of AFC. The attitude control capability of the combined energy and attitude control system (CEACS) is expected to improve. The result shows an important attitude pointing enhancement for the CEACS attitude control task.
format Article
author Varatharajoo, Renuganth
Choo, Tech Wooi
Mailah, Musa
spellingShingle Varatharajoo, Renuganth
Choo, Tech Wooi
Mailah, Musa
Attitude pointing enhancement for combined energy and attitude control system
author_facet Varatharajoo, Renuganth
Choo, Tech Wooi
Mailah, Musa
author_sort Varatharajoo, Renuganth
title Attitude pointing enhancement for combined energy and attitude control system
title_short Attitude pointing enhancement for combined energy and attitude control system
title_full Attitude pointing enhancement for combined energy and attitude control system
title_fullStr Attitude pointing enhancement for combined energy and attitude control system
title_full_unstemmed Attitude pointing enhancement for combined energy and attitude control system
title_sort attitude pointing enhancement for combined energy and attitude control system
publisher Elsevier
publishDate 2011
url http://psasir.upm.edu.my/id/eprint/23142/1/Attitude%20pointing%20enhancement%20for%20combined%20energy%20and%20attitude%20control%20system.pdf
http://psasir.upm.edu.my/id/eprint/23142/
_version_ 1643827971330408448
score 13.211869

Similar Items