Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite
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Institute of Engineering Mathematics, Universiti Malaysia Perlis
2015
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my.unimap-406632018-07-24T01:52:21Z Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite Teoh, Vil Cherd Shahriman, Abu Bakar Norhizam, Hamzah Sazali, Yaacob Ruslizam, Daud Rakhmad Arief, Siregar vaticano87@hotmail.com Satellite Flexible Rigid Model Comparison Link to publisher's homepage at http://amci.unimap.edu.my Rigid body assumption of a satellite model has been a common practice in spacecraft attitude manoeuvring. However, with the increasing demand for greater functionality of space activities, requires bigger and wider solar panels to cater the power needs. In this paper, simple rigid and flexible multi-body satellite model is derived using basic Newton’s second law and Assumed Mode Method. The response from both model are then simulated using MATLAB software while comparison is done to illustrate the significance of the flexible behaviour that inherited in the satellite system. With the negligence of flexible interference in the rigid model, it is likely to execute an exact attitude motion while the flexible model would yield a harmonic motion that is due to the vibratory motion of the solar panels. 2015-12-30T04:32:10Z 2015-12-30T04:32:10Z 2014 Article Applied Mathematics and Computational Intelligence (AMCI), vol.3 (1), 2014, pages 229-240 2289-1323 (online) 2289-1315 (print) http://amci.unimap.edu.my http://dspace.unimap.edu.my:80/xmlui/handle/123456789/40663 en Institute of Engineering Mathematics, Universiti Malaysia Perlis |
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English |
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Satellite Flexible Rigid Model Comparison |
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Satellite Flexible Rigid Model Comparison Teoh, Vil Cherd Shahriman, Abu Bakar Norhizam, Hamzah Sazali, Yaacob Ruslizam, Daud Rakhmad Arief, Siregar Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite |
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Link to publisher's homepage at http://amci.unimap.edu.my |
| author2 |
vaticano87@hotmail.com |
| author_facet |
vaticano87@hotmail.com Teoh, Vil Cherd Shahriman, Abu Bakar Norhizam, Hamzah Sazali, Yaacob Ruslizam, Daud Rakhmad Arief, Siregar |
| format |
Article |
| author |
Teoh, Vil Cherd Shahriman, Abu Bakar Norhizam, Hamzah Sazali, Yaacob Ruslizam, Daud Rakhmad Arief, Siregar |
| author_sort |
Teoh, Vil Cherd |
| title |
Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite |
| title_short |
Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite |
| title_full |
Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite |
| title_fullStr |
Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite |
| title_full_unstemmed |
Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite |
| title_sort |
comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite |
| publisher |
Institute of Engineering Mathematics, Universiti Malaysia Perlis |
| publishDate |
2015 |
| url |
http://dspace.unimap.edu.my:80/xmlui/handle/123456789/40663 |
| _version_ |
1643804041929555968 |