Development of a nano-satellite – attitude control system

NTU Satellite Research center initiates the Nano-­‐satellite project in 2009 to develop a pico and Nano-­‐satellite pair known as VELOX-­‐I. Since then, many FYP, URECA and DIP students have been involved in...

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Main Author: Li, Bing Xuan.
Other Authors: Low Kay Soon
Format: Final Year Project
Language:English
Published: 2011
Subjects:
Online Access:http://hdl.handle.net/10356/45391
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-453912023-07-07T16:19:16Z Development of a nano-satellite – attitude control system Li, Bing Xuan. Low Kay Soon School of Electrical and Electronic Engineering DRNTU::Engineering::Electrical and electronic engineering::Satellite telecommunication NTU Satellite Research center initiates the Nano-­‐satellite project in 2009 to develop a pico and Nano-­‐satellite pair known as VELOX-­‐I. Since then, many FYP, URECA and DIP students have been involved in the conceptualization, design and prototyping of various subsystems of the nanosatellite. This project is part of the Attitude Determination and Control System (ADCS) development work. The project involves in the development of a satellite attitude simulator to facilitate the development of the ADCS. The simulator provides a GUI for input the testing specifications. The simulation result base on various environment and system models will be displayed in a 3D animation video. The simulation of sensor data will also be included in the simulator, and the result will be used to test the attitude determination algorithm in the future ADCS projects. Three substantial attitude control strategies, namely PID, BDOT, and MPC, have been implemented in the simulator for test and tuning. Bachelor of Engineering 2011-06-13T04:50:46Z 2011-06-13T04:50:46Z 2011 2011 Final Year Project (FYP) http://hdl.handle.net/10356/45391 en Nanyang Technological University 100 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::Satellite telecommunication
spellingShingle DRNTU::Engineering::Electrical and electronic engineering::Satellite telecommunication
Li, Bing Xuan.
Development of a nano-satellite – attitude control system
description NTU Satellite Research center initiates the Nano-­‐satellite project in 2009 to develop a pico and Nano-­‐satellite pair known as VELOX-­‐I. Since then, many FYP, URECA and DIP students have been involved in the conceptualization, design and prototyping of various subsystems of the nanosatellite. This project is part of the Attitude Determination and Control System (ADCS) development work. The project involves in the development of a satellite attitude simulator to facilitate the development of the ADCS. The simulator provides a GUI for input the testing specifications. The simulation result base on various environment and system models will be displayed in a 3D animation video. The simulation of sensor data will also be included in the simulator, and the result will be used to test the attitude determination algorithm in the future ADCS projects. Three substantial attitude control strategies, namely PID, BDOT, and MPC, have been implemented in the simulator for test and tuning.
author2 Low Kay Soon
author_facet Low Kay Soon
Li, Bing Xuan.
format Final Year Project
author Li, Bing Xuan.
author_sort Li, Bing Xuan.
title Development of a nano-satellite – attitude control system
title_short Development of a nano-satellite – attitude control system
title_full Development of a nano-satellite – attitude control system
title_fullStr Development of a nano-satellite – attitude control system
title_full_unstemmed Development of a nano-satellite – attitude control system
title_sort development of a nano-satellite – attitude control system
publishDate 2011
url http://hdl.handle.net/10356/45391
_version_ 1772825499503951872