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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| المؤلفون الرئيسيون: | , , , , , , |
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| التنسيق: | Working Paper |
| اللغة: | English |
| منشور في: |
Universiti Malaysia Perlis (UniMAP)
2012
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| الوصول للمادة أونلاين: | http://dspace.unimap.edu.my/xmlui/handle/123456789/20506 |
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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 |
13.251813 |