MARC表示: Mathematical model attitude estimation using Kalman filter technique for low earth orbit satellite

Mathematical model attitude estimation using Kalman filter technique for low earth orbit satellite

International Conference on Man Machine Systems (ICoMMS 2012) organized by School of Mechatronic Engineering, co-organized by The Institute of Engineer, Malaysia (IEM) and Society of Engineering Education Malaysia, 27th - 28th February 2012 at Bayview Beach Resort, Penang, Malaysia.

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書誌詳細
主要な著者:	Nor Hazadura, Hamzah, Sazali, Yaacob, Prof. Dr., Teoh, Vil Cherd, Siti Maryam, Harun, Hariharan, Muthusamy, Mohamad Nazri, Dol Bahar, Norhizam, Hamzah
その他の著者:	hazadura@unimap.edu.my
フォーマット:	Working Paper
言語:	English
出版事項:	Universiti Malaysia Perlis (UniMAP) 2012
主題:	Mathematical model Satellite attitude control Gravity gradient moment Attitude estimation Karman Filter
オンライン･アクセス:	http://dspace.unimap.edu.my/xmlui/handle/123456789/20506
タグ:	タグ追加タグなし, このレコードへの初めてのタグを付けませんか!

id	my.unimap-20506
record_format	dspace
spelling	my.unimap-205062012-07-20T03:03:08Z Mathematical model attitude estimation using Kalman filter technique for low earth orbit satellite Nor Hazadura, Hamzah Sazali, Yaacob, Prof. Dr. Teoh, Vil Cherd Siti Maryam, Harun Hariharan, Muthusamy Mohamad Nazri, Dol Bahar Norhizam, Hamzah hazadura@unimap.edu.my Mathematical model Satellite attitude control Gravity gradient moment Attitude estimation Karman Filter International Conference on Man Machine Systems (ICoMMS 2012) organized by School of Mechatronic Engineering, co-organized by The Institute of Engineer, Malaysia (IEM) and Society of Engineering Education Malaysia, 27th - 28th February 2012 at Bayview Beach Resort, Penang, Malaysia. In space, the attitude analysis of a satellite is constantly being computed within the system of the satellite. In this paper, the linear mathematical model of the satellite attitude control with gravity gradient moment, which is inherent in low-orbit satellite is derived. Additionally, attitude estimation using the Kalman Filter technique is employed to predict the actual satellite’s attitude despite the disturbance presence in the system. As for demonstration purpose, a simulation of the satellite’s attitude under gravity gradient moment, and the attitude estimation via Kalman Filter is carried out using MATLAB software. The simulation results show that the initial conditions affect the satellite’s attitude, and attitude estimation process is important to estimate the actual satellite’s attitude despite of disturbance presence. 2012-07-20T03:03:08Z 2012-07-20T03:03:08Z 2012-02-27 Working Paper http://hdl.handle.net/123456789/20506 en Proceedings of the International Conference on Man-Machine Systems (ICoMMS 2012 Universiti Malaysia Perlis (UniMAP) School of Mechatronic Engineering
institution	Universiti Malaysia Perlis
building	UniMAP Library
collection	Institutional Repository
continent	Asia
country	Malaysia
content_provider	Universiti Malaysia Perlis
content_source	UniMAP Library Digital Repository
url_provider	http://dspace.unimap.edu.my/
language	English
topic	Mathematical model Satellite attitude control Gravity gradient moment Attitude estimation Karman Filter
spellingShingle	Mathematical model Satellite attitude control Gravity gradient moment Attitude estimation Karman Filter Nor Hazadura, Hamzah Sazali, Yaacob, Prof. Dr. Teoh, Vil Cherd Siti Maryam, Harun Hariharan, Muthusamy Mohamad Nazri, Dol Bahar Norhizam, Hamzah Mathematical model attitude estimation using Kalman filter technique for low earth orbit satellite
description	International Conference on Man Machine Systems (ICoMMS 2012) organized by School of Mechatronic Engineering, co-organized by The Institute of Engineer, Malaysia (IEM) and Society of Engineering Education Malaysia, 27th - 28th February 2012 at Bayview Beach Resort, Penang, Malaysia.
author2	hazadura@unimap.edu.my
author_facet	hazadura@unimap.edu.my Nor Hazadura, Hamzah Sazali, Yaacob, Prof. Dr. Teoh, Vil Cherd Siti Maryam, Harun Hariharan, Muthusamy Mohamad Nazri, Dol Bahar Norhizam, Hamzah
format	Working Paper
author	Nor Hazadura, Hamzah Sazali, Yaacob, Prof. Dr. Teoh, Vil Cherd Siti Maryam, Harun Hariharan, Muthusamy Mohamad Nazri, Dol Bahar Norhizam, Hamzah
author_sort	Nor Hazadura, Hamzah
title	Mathematical model attitude estimation using Kalman filter technique for low earth orbit satellite
title_short	Mathematical model attitude estimation using Kalman filter technique for low earth orbit satellite
title_full	Mathematical model attitude estimation using Kalman filter technique for low earth orbit satellite
title_fullStr	Mathematical model attitude estimation using Kalman filter technique for low earth orbit satellite
title_full_unstemmed	Mathematical model attitude estimation using Kalman filter technique for low earth orbit satellite
title_sort	mathematical model attitude estimation using kalman filter technique for low earth orbit satellite
publisher	Universiti Malaysia Perlis (UniMAP)
publishDate	2012
url	http://dspace.unimap.edu.my/xmlui/handle/123456789/20506
_version_	1643793093555650560
score	13.250246

Mathematical model attitude estimation using Kalman filter technique for low earth orbit satellite

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