Optimal control of the attitude maneuvering for Razaksat class satellite based on rigid and flexible model
The increase in demand for performance for satellite capabilities has pushed the design of the system to be more and more power consuming. This is the case for RazakSAT-2, which is a new satellite program that will be equipped with bigger solar panel to generate sufficient power. Thus, this translat...
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| التنسيق: | أطروحة |
|---|---|
| اللغة: | English |
| الموضوعات: | |
| الوصول للمادة أونلاين: | http://dspace.unimap.edu.my:80/xmlui/bitstream/123456789/78808/1/Page%201-25.pdf http://dspace.unimap.edu.my:80/xmlui/bitstream/123456789/78808/2/Full%20text.pdf http://dspace.unimap.edu.my:80/xmlui/bitstream/123456789/78808/3/Teoh%20Vil%20Cherd.pdf |
| الوسوم: |
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