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Development Of Attitude Determination For Student Pico-Satellite INNOSAT.

Information of satellite’s attitude is very useful in autonomous satellite control system. For a small satellite particularly, attitude sensor cannot be installed in the satellite because of the limited weight and power consumption.

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Bibliographic Details
Main Authors: M, Fadly, Sidek, Dr.Othman, Md Said, Md Azlin
Format: Conference or Workshop Item
Language:English
Published: 2010
Subjects:
TK1-9971 Electrical engineering. Electronics. Nuclear engineering
Online Access:http://eprints.usm.my/19413/1/Paper_518.pdf
http://eprints.usm.my/19413/
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id my.usm.eprints.19413
record_format eprints
spelling my.usm.eprints.19413 http://eprints.usm.my/19413/ Development Of Attitude Determination For Student Pico-Satellite INNOSAT. M, Fadly Sidek, Dr.Othman Md Said, Md Azlin TK1-9971 Electrical engineering. Electronics. Nuclear engineering Information of satellite’s attitude is very useful in autonomous satellite control system. For a small satellite particularly, attitude sensor cannot be installed in the satellite because of the limited weight and power consumption. 2010-02 Conference or Workshop Item PeerReviewed application/pdf en http://eprints.usm.my/19413/1/Paper_518.pdf M, Fadly and Sidek, Dr.Othman and Md Said, Md Azlin (2010) Development Of Attitude Determination For Student Pico-Satellite INNOSAT. In: Regional Conference on Mechanical and Aerospace Technology , 9-10 February 2010, Bali,Indonesia.
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 TK1-9971 Electrical engineering. Electronics. Nuclear engineering
spellingShingle TK1-9971 Electrical engineering. Electronics. Nuclear engineering
M, Fadly
Sidek, Dr.Othman
Md Said, Md Azlin
Development Of Attitude Determination For Student Pico-Satellite INNOSAT.
description Information of satellite’s attitude is very useful in autonomous satellite control system. For a small satellite particularly, attitude sensor cannot be installed in the satellite because of the limited weight and power consumption.
format Conference or Workshop Item
author M, Fadly
Sidek, Dr.Othman
Md Said, Md Azlin
author_facet M, Fadly
Sidek, Dr.Othman
Md Said, Md Azlin
author_sort M, Fadly
title Development Of Attitude Determination For Student Pico-Satellite INNOSAT.
title_short Development Of Attitude Determination For Student Pico-Satellite INNOSAT.
title_full Development Of Attitude Determination For Student Pico-Satellite INNOSAT.
title_fullStr Development Of Attitude Determination For Student Pico-Satellite INNOSAT.
title_full_unstemmed Development Of Attitude Determination For Student Pico-Satellite INNOSAT.
title_sort development of attitude determination for student pico-satellite innosat.
publishDate 2010
url http://eprints.usm.my/19413/1/Paper_518.pdf
http://eprints.usm.my/19413/
_version_ 1643704101652922368
score 13.211869

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