Development of a passive attitude control system for the VELOX-LYON-1 student CubeSat

The goal of this report is to summarize the ideas, designs, methodologies and data of this final year project. This final year project report gives a fundamental understanding of the attitude control system of a Cube Satellite (CubeSat) and the detailed explanation of the various experimentations...

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Main Author: Li, Chang
Other Authors: Amal Chandran
Format: Final Year Project
Language:English
Published: 2019
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Online Access:http://hdl.handle.net/10356/78325
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-783252023-07-07T15:56:23Z Development of a passive attitude control system for the VELOX-LYON-1 student CubeSat Li, Chang Amal Chandran School of Electrical and Electronic Engineering DRNTU::Engineering::Electrical and electronic engineering The goal of this report is to summarize the ideas, designs, methodologies and data of this final year project. This final year project report gives a fundamental understanding of the attitude control system of a Cube Satellite (CubeSat) and the detailed explanation of the various experimentations conducted on the selections and sizing of the hardware components. The type of attitude control system chosen for this satellite project is passive magnetic attitude control system which is a pure passive control system ideal for nanosatellites such as CubeSats. This attitude control system is designed for VELOX-LYON-1 3U CubeSat from Satellite Research Centre at Nanyang Technological University. Passive Magnetic Attitude Control system (PMAC) mainly consists of bar magnets and hysteresis rods. In this report, characterizations of the permanent bar magnets and hysteresis rods are performed experimentally. Bar magnets with 3 different dipole moments were characterized. The hysteresis rod material chosen is HyMu-80 Permalloy. Various experiments are conducted with the goal of evaluation the actual magnetic behaviours of both the magnets and the hysteresis rods. As for the bar magnets, actual dipole moments should be examined while for hysteresis rods, its magnetic parameters such as remanence, coercivity and saturation have to be studied. Before the sizing and selections of the hardware, basic aerodynamic theories were being introduced and discussed as the space environmental torques are seen as a form of disturbances to the CubeSat which will affect the attitude determination and control. Space environmental torques are computed and the sizing of the bar magnets depends on the calculated values. The data collected has been further processed and analysed. The results of the experiments are also been discussed in-depth. Bachelor of Engineering (Electrical and Electronic Engineering) 2019-06-18T02:53:42Z 2019-06-18T02:53:42Z 2019 Final Year Project (FYP) http://hdl.handle.net/10356/78325 en Nanyang Technological University 93 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::Electrical and electronic engineering
spellingShingle DRNTU::Engineering::Electrical and electronic engineering
Li, Chang
Development of a passive attitude control system for the VELOX-LYON-1 student CubeSat
description The goal of this report is to summarize the ideas, designs, methodologies and data of this final year project. This final year project report gives a fundamental understanding of the attitude control system of a Cube Satellite (CubeSat) and the detailed explanation of the various experimentations conducted on the selections and sizing of the hardware components. The type of attitude control system chosen for this satellite project is passive magnetic attitude control system which is a pure passive control system ideal for nanosatellites such as CubeSats. This attitude control system is designed for VELOX-LYON-1 3U CubeSat from Satellite Research Centre at Nanyang Technological University. Passive Magnetic Attitude Control system (PMAC) mainly consists of bar magnets and hysteresis rods. In this report, characterizations of the permanent bar magnets and hysteresis rods are performed experimentally. Bar magnets with 3 different dipole moments were characterized. The hysteresis rod material chosen is HyMu-80 Permalloy. Various experiments are conducted with the goal of evaluation the actual magnetic behaviours of both the magnets and the hysteresis rods. As for the bar magnets, actual dipole moments should be examined while for hysteresis rods, its magnetic parameters such as remanence, coercivity and saturation have to be studied. Before the sizing and selections of the hardware, basic aerodynamic theories were being introduced and discussed as the space environmental torques are seen as a form of disturbances to the CubeSat which will affect the attitude determination and control. Space environmental torques are computed and the sizing of the bar magnets depends on the calculated values. The data collected has been further processed and analysed. The results of the experiments are also been discussed in-depth.
author2 Amal Chandran
author_facet Amal Chandran
Li, Chang
format Final Year Project
author Li, Chang
author_sort Li, Chang
title Development of a passive attitude control system for the VELOX-LYON-1 student CubeSat
title_short Development of a passive attitude control system for the VELOX-LYON-1 student CubeSat
title_full Development of a passive attitude control system for the VELOX-LYON-1 student CubeSat
title_fullStr Development of a passive attitude control system for the VELOX-LYON-1 student CubeSat
title_full_unstemmed Development of a passive attitude control system for the VELOX-LYON-1 student CubeSat
title_sort development of a passive attitude control system for the velox-lyon-1 student cubesat
publishDate 2019
url http://hdl.handle.net/10356/78325
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