An optimum magnetic control torque generation of a momentum bias satellite

This paper describes a comparison study of magnetic attitude control torque generation performance of a momentum bias satellite operated in Low Earth Orbit (LEO) with various orbit inclinations. The satellite is equipped with two magnetic torquers that are placed along the +x and +y axes where m...

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Main Authors: Mohd Suhadis, Nurulasikin, Varatharajoo, Renuganth
Format: Article
Language:English
Published: International Society of Multiphysics 2014
Subjects:
Online Access:http://eprints.usm.my/36792/1/%28An_optimum_magnetic_control%29_255-582-1-SM.pdf
http://eprints.usm.my/36792/
http://journal.multiphysics.org/index.php/IJM/article/view/255
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spelling my.usm.eprints.36792 http://eprints.usm.my/36792/ An optimum magnetic control torque generation of a momentum bias satellite Mohd Suhadis, Nurulasikin Varatharajoo, Renuganth TL1-4050 Motor vehicles. Aeronautics. Astronautics This paper describes a comparison study of magnetic attitude control torque generation performance of a momentum bias satellite operated in Low Earth Orbit (LEO) with various orbit inclinations. The satellite is equipped with two magnetic torquers that are placed along the +x and +y axes where magnetic control torque is generated when these magnetic torquers couple with the geomagnetic fields and its vector direction is perpendicular to both the magnetic fields. The control algorithm was structured using a proportional (P) controller for satellite attitudes/nutation control and a proportional-integral (PI) controller for managing the excess angular momentum on the momentum wheel. The structured control algorithm is simulated for 23°, 53° and 83° orbit inclinations and the generated attitude torque performances are compared to see how the variation of the satellite orbit affects the satellite’s attitude torque generation as the magnitude and direction of the geomagnetic fields vary with respect to the altitude and latitude while the magnitude and direction of the magnetic fields generated by the magnetic torquers vary with respect to the orbital motion. Results from simulation show that the higher orbit inclination generates optimum magnetic attitude control torque. Note that this work is the extension of the previous work published in The International Journal of Multiphysics [1]. International Society of Multiphysics 2014 Article PeerReviewed application/pdf en http://eprints.usm.my/36792/1/%28An_optimum_magnetic_control%29_255-582-1-SM.pdf Mohd Suhadis, Nurulasikin and Varatharajoo, Renuganth (2014) An optimum magnetic control torque generation of a momentum bias satellite. International Journal of Multiphysics, 8 (2). pp. 169-179. ISSN 1750-9548 http://journal.multiphysics.org/index.php/IJM/article/view/255
institution Universiti Sains Malaysia
building Hamzah Sendut Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Sains Malaysia
content_source USM Institutional Repository
url_provider http://eprints.usm.my/
language English
topic TL1-4050 Motor vehicles. Aeronautics. Astronautics
spellingShingle TL1-4050 Motor vehicles. Aeronautics. Astronautics
Mohd Suhadis, Nurulasikin
Varatharajoo, Renuganth
An optimum magnetic control torque generation of a momentum bias satellite
description This paper describes a comparison study of magnetic attitude control torque generation performance of a momentum bias satellite operated in Low Earth Orbit (LEO) with various orbit inclinations. The satellite is equipped with two magnetic torquers that are placed along the +x and +y axes where magnetic control torque is generated when these magnetic torquers couple with the geomagnetic fields and its vector direction is perpendicular to both the magnetic fields. The control algorithm was structured using a proportional (P) controller for satellite attitudes/nutation control and a proportional-integral (PI) controller for managing the excess angular momentum on the momentum wheel. The structured control algorithm is simulated for 23°, 53° and 83° orbit inclinations and the generated attitude torque performances are compared to see how the variation of the satellite orbit affects the satellite’s attitude torque generation as the magnitude and direction of the geomagnetic fields vary with respect to the altitude and latitude while the magnitude and direction of the magnetic fields generated by the magnetic torquers vary with respect to the orbital motion. Results from simulation show that the higher orbit inclination generates optimum magnetic attitude control torque. Note that this work is the extension of the previous work published in The International Journal of Multiphysics [1].
format Article
author Mohd Suhadis, Nurulasikin
Varatharajoo, Renuganth
author_facet Mohd Suhadis, Nurulasikin
Varatharajoo, Renuganth
author_sort Mohd Suhadis, Nurulasikin
title An optimum magnetic control torque generation of a momentum bias satellite
title_short An optimum magnetic control torque generation of a momentum bias satellite
title_full An optimum magnetic control torque generation of a momentum bias satellite
title_fullStr An optimum magnetic control torque generation of a momentum bias satellite
title_full_unstemmed An optimum magnetic control torque generation of a momentum bias satellite
title_sort optimum magnetic control torque generation of a momentum bias satellite
publisher International Society of Multiphysics
publishDate 2014
url http://eprints.usm.my/36792/1/%28An_optimum_magnetic_control%29_255-582-1-SM.pdf
http://eprints.usm.my/36792/
http://journal.multiphysics.org/index.php/IJM/article/view/255
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score 13.211869