Development of an advanced nano-satellite (VELOX-I) – MEMS based attitude sensing system

The satellite research centre (SaRC) of Nanyang Technological University is developing the first nano-satellite in Singapore. This project focuses on the Attitude Determination System of the VELOX-I, more specifically, the Coarse Sun Sensor. As the first part of the project, the photodiodes that was...

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Main Author: Tan, Edwin Jian Rong.
Other Authors: Low Kay Soon
Format: Final Year Project
Language:English
Published: 2013
Subjects:
Online Access:http://hdl.handle.net/10356/54378
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-543782023-07-07T15:50:41Z Development of an advanced nano-satellite (VELOX-I) – MEMS based attitude sensing system Tan, Edwin Jian Rong. Low Kay Soon School of Electrical and Electronic Engineering Satellite Engineering Centre DRNTU::Engineering The satellite research centre (SaRC) of Nanyang Technological University is developing the first nano-satellite in Singapore. This project focuses on the Attitude Determination System of the VELOX-I, more specifically, the Coarse Sun Sensor. As the first part of the project, the photodiodes that was used to implement Coarse Sun Sensor was investigated. The photodiode cosine characteristics were found to have deviations from the true cosine property by up to 5%. The maximum output current from the photodiode at a solar constant, AM0, was found to be 1.3mA. The Coarse Sun Sensor was proven to have a pointing accuracy of 8 degrees which is comparable to other satellites as reported in the literature. An orbit path was also simulated and results reflected a similar result of close to 8 degrees. A significant finding was that maximum error occurs when light shines on only 1 photodiode. Software calibration was proposed to improve it to an estimated accuracy of less than 2 degree. The second part of the project focuses on the study of the effects of Earth Albedo. Using the Reflected Shortwave Radiation data from National Aeronautics and Space Administration (NASA), a Matlab simulation model of Earth Albedo was formed. It provided the necessary albedo information to be used in the orbital simulation. The effect of this Earth Albedo on the Sun pointing accuracy can be as high as 11 degrees and the attitude determination error was found to be as high as 12 degrees in the roll, pitch and yaw. Compensation for this albedo effect was proposed. Last but not least, fault detection for the vector sensors was achieved through the use of the residuals present in the current design of the Kalman Filter. Bachelor of Engineering 2013-06-19T08:13:11Z 2013-06-19T08:13:11Z 2013 2013 Final Year Project (FYP) http://hdl.handle.net/10356/54378 en Nanyang Technological University 99 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering
spellingShingle DRNTU::Engineering
Tan, Edwin Jian Rong.
Development of an advanced nano-satellite (VELOX-I) – MEMS based attitude sensing system
description The satellite research centre (SaRC) of Nanyang Technological University is developing the first nano-satellite in Singapore. This project focuses on the Attitude Determination System of the VELOX-I, more specifically, the Coarse Sun Sensor. As the first part of the project, the photodiodes that was used to implement Coarse Sun Sensor was investigated. The photodiode cosine characteristics were found to have deviations from the true cosine property by up to 5%. The maximum output current from the photodiode at a solar constant, AM0, was found to be 1.3mA. The Coarse Sun Sensor was proven to have a pointing accuracy of 8 degrees which is comparable to other satellites as reported in the literature. An orbit path was also simulated and results reflected a similar result of close to 8 degrees. A significant finding was that maximum error occurs when light shines on only 1 photodiode. Software calibration was proposed to improve it to an estimated accuracy of less than 2 degree. The second part of the project focuses on the study of the effects of Earth Albedo. Using the Reflected Shortwave Radiation data from National Aeronautics and Space Administration (NASA), a Matlab simulation model of Earth Albedo was formed. It provided the necessary albedo information to be used in the orbital simulation. The effect of this Earth Albedo on the Sun pointing accuracy can be as high as 11 degrees and the attitude determination error was found to be as high as 12 degrees in the roll, pitch and yaw. Compensation for this albedo effect was proposed. Last but not least, fault detection for the vector sensors was achieved through the use of the residuals present in the current design of the Kalman Filter.
author2 Low Kay Soon
author_facet Low Kay Soon
Tan, Edwin Jian Rong.
format Final Year Project
author Tan, Edwin Jian Rong.
author_sort Tan, Edwin Jian Rong.
title Development of an advanced nano-satellite (VELOX-I) – MEMS based attitude sensing system
title_short Development of an advanced nano-satellite (VELOX-I) – MEMS based attitude sensing system
title_full Development of an advanced nano-satellite (VELOX-I) – MEMS based attitude sensing system
title_fullStr Development of an advanced nano-satellite (VELOX-I) – MEMS based attitude sensing system
title_full_unstemmed Development of an advanced nano-satellite (VELOX-I) – MEMS based attitude sensing system
title_sort development of an advanced nano-satellite (velox-i) – mems based attitude sensing system
publishDate 2013
url http://hdl.handle.net/10356/54378
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