Development of an attitude control system for InnoSAT satellite /
The purpose of this work was to develop control scheme for one, two and three axis stabilization of a magnetic actuated satellite for InnoSAT. This was achieved by a combination of a two mode system theory. The de-tumbling mode by means of a passive 1st phase controller for quick response and 2nd ph...
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| Формат: | Дисертація Книга |
| Мова: | English |
| Опубліковано: |
Perlis, Malaysia
School of Mechatronic Engineering
2011.
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