Attitude determination system for nano-satelite
The thesis focuses on the attitude determination system of a satellite. Attitude determination is the process of computing the spacecraft orientation relative to inertial reference frame such as the Earth center inertial frame. The attitude determination process is critical in satellite operation...
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2014
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sg-ntu-dr.10356-607072023-07-04T15:36:40Z Attitude determination system for nano-satelite Pham, Minh Duc Low Kay Soon School of Electrical and Electronic Engineering DRNTU::Engineering The thesis focuses on the attitude determination system of a satellite. Attitude determination is the process of computing the spacecraft orientation relative to inertial reference frame such as the Earth center inertial frame. The attitude determination process is critical in satellite operation as it is required to control the satellite attitude in a specified direction. Master of Engineering 2014-05-29T06:40:22Z 2014-05-29T06:40:22Z 2013 2013 Thesis http://hdl.handle.net/10356/60707 en 154 p. application/pdf |
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DRNTU::Engineering Pham, Minh Duc Attitude determination system for nano-satelite |
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The thesis focuses on the attitude determination system of a satellite. Attitude determination is the
process of computing the spacecraft orientation relative to inertial reference frame such as the Earth
center inertial frame. The attitude determination process is critical in satellite operation as it is
required to control the satellite attitude in a specified direction. |
author2 |
Low Kay Soon |
author_facet |
Low Kay Soon Pham, Minh Duc |
format |
Theses and Dissertations |
author |
Pham, Minh Duc |
author_sort |
Pham, Minh Duc |
title |
Attitude determination system for nano-satelite |
title_short |
Attitude determination system for nano-satelite |
title_full |
Attitude determination system for nano-satelite |
title_fullStr |
Attitude determination system for nano-satelite |
title_full_unstemmed |
Attitude determination system for nano-satelite |
title_sort |
attitude determination system for nano-satelite |
publishDate |
2014 |
url |
http://hdl.handle.net/10356/60707 |
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1772826008810946560 |