Attitude Determination System For Nano Satellite Using Extended Kalman Filter On ARM7TDMI Platform

Extended Kalman Filter (EKF) has been successfully utilized in satellites missions. However, in comparison to other attitude determination methods developed, it is one of the most computationally burdening algorithm and with the new development of using nano satellites which have limited electric...

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Main Author:	Adam Ain, Mohd Poin Keui
Format:	Thesis
Language:	English
Published:	2014
Subjects:	TK1-9971 Electrical engineering. Electronics. Nuclear engineering
Online Access:	http://eprints.usm.my/28966/1/ATTITUDE_DETERMINATION_SYSTEM_FOR_NANO_SATELLITE_USING_EXTENDED_KALMAN_FILTER_ON_ARM7TDMI_PLATFORM.pdf

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author	Adam Ain, Mohd Poin Keui
author_facet	Adam Ain, Mohd Poin Keui
author_sort	Adam Ain, Mohd Poin Keui
collection	USM
description	Extended Kalman Filter (EKF) has been successfully utilized in satellites missions. However, in comparison to other attitude determination methods developed, it is one of the most computationally burdening algorithm and with the new development of using nano satellites which have limited electrical power, mass, space and usually budget, it is essential to design an Attitude Determination System (ADS) which conforms to this limitation. Therefore, in this thesis, as a computational improvement on the InnoSAT project, the RCM3400 microcontroller of the ADS is replaced with the ARM7TDMI based microprocessor to test its capability. Penapisan Kalman Lanjutan (PKL) telah digunakan dengan jayanya di dalam misi satelit. Akan tetapi, jika dibandingkan dengan kaedah penentuan kedudukan lain yang telah dihasilkan, ia adalah salah satu daripada algoritma yang memiliki komputasi yang paling berat dan dengan perkembangan terkini yang menggunakan satelit nano yang mempunyai kuasa elektrik, berat, ruang dan biasanya peruntukan yang terhad, adalah menjadi satu keutamaan untuk merekabentuk sebuah Sistem Penentuan Kedudukan (SPK) yang dapat mematuhi kekangan ini.
first_indexed	2024-03-06T14:48:22Z
format	Thesis
id	usm.eprints-28966
institution	Universiti Sains Malaysia
language	English
last_indexed	2024-03-06T14:48:22Z
publishDate	2014
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spelling	usm.eprints-289662019-04-12T05:26:03Z http://eprints.usm.my/28966/ Attitude Determination System For Nano Satellite Using Extended Kalman Filter On ARM7TDMI Platform Adam Ain, Mohd Poin Keui TK1-9971 Electrical engineering. Electronics. Nuclear engineering Extended Kalman Filter (EKF) has been successfully utilized in satellites missions. However, in comparison to other attitude determination methods developed, it is one of the most computationally burdening algorithm and with the new development of using nano satellites which have limited electrical power, mass, space and usually budget, it is essential to design an Attitude Determination System (ADS) which conforms to this limitation. Therefore, in this thesis, as a computational improvement on the InnoSAT project, the RCM3400 microcontroller of the ADS is replaced with the ARM7TDMI based microprocessor to test its capability. Penapisan Kalman Lanjutan (PKL) telah digunakan dengan jayanya di dalam misi satelit. Akan tetapi, jika dibandingkan dengan kaedah penentuan kedudukan lain yang telah dihasilkan, ia adalah salah satu daripada algoritma yang memiliki komputasi yang paling berat dan dengan perkembangan terkini yang menggunakan satelit nano yang mempunyai kuasa elektrik, berat, ruang dan biasanya peruntukan yang terhad, adalah menjadi satu keutamaan untuk merekabentuk sebuah Sistem Penentuan Kedudukan (SPK) yang dapat mematuhi kekangan ini. 2014 Thesis NonPeerReviewed application/pdf en http://eprints.usm.my/28966/1/ATTITUDE_DETERMINATION_SYSTEM_FOR_NANO_SATELLITE_USING_EXTENDED_KALMAN_FILTER_ON_ARM7TDMI_PLATFORM.pdf Adam Ain, Mohd Poin Keui (2014) Attitude Determination System For Nano Satellite Using Extended Kalman Filter On ARM7TDMI Platform. Masters thesis, Universiti Sains Malaysia.
spellingShingle	TK1-9971 Electrical engineering. Electronics. Nuclear engineering Adam Ain, Mohd Poin Keui Attitude Determination System For Nano Satellite Using Extended Kalman Filter On ARM7TDMI Platform
title	Attitude Determination System For Nano Satellite Using Extended Kalman Filter On ARM7TDMI Platform
title_full	Attitude Determination System For Nano Satellite Using Extended Kalman Filter On ARM7TDMI Platform
title_fullStr	Attitude Determination System For Nano Satellite Using Extended Kalman Filter On ARM7TDMI Platform
title_full_unstemmed	Attitude Determination System For Nano Satellite Using Extended Kalman Filter On ARM7TDMI Platform
title_short	Attitude Determination System For Nano Satellite Using Extended Kalman Filter On ARM7TDMI Platform
title_sort	attitude determination system for nano satellite using extended kalman filter on arm7tdmi platform
topic	TK1-9971 Electrical engineering. Electronics. Nuclear engineering
url	http://eprints.usm.my/28966/1/ATTITUDE_DETERMINATION_SYSTEM_FOR_NANO_SATELLITE_USING_EXTENDED_KALMAN_FILTER_ON_ARM7TDMI_PLATFORM.pdf
work_keys_str_mv	AT adamainmohdpoinkeui attitudedeterminationsystemfornanosatelliteusingextendedkalmanfilteronarm7tdmiplatform

Attitude Determination System For Nano Satellite Using Extended Kalman Filter On ARM7TDMI Platform

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