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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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Bibliographic Details
Main Authors: Nor Hazadura, Hamzah, Sazali, Yaacob, Prof. Dr., Teoh, Vil Cherd, Siti Maryam, Harun, Hariharan, Muthusamy, Mohamad Nazri, Dol Bahar, Norhizam, Hamzah
Other Authors: hazadura@unimap.edu.my
Format: Working Paper
Language:English
Published: Universiti Malaysia Perlis (UniMAP) 2012
Subjects:
Mathematical model
Satellite attitude control
Gravity gradient moment
Attitude estimation
Karman Filter
Online Access:http://dspace.unimap.edu.my/xmlui/handle/123456789/20506
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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 13.211869

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