Attitude Control System for InnoSAT
To develop attitude control algorithms software; ACS is the part of the ADCS payload. The ACS has Adaptive Predictive Fuzzy Logic. The objective of this project is to develop attitude control algorithms that are going to be tested when the InnoSAT is in the orbit. Upon deployment in the near Equitor...
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| Format: | Other |
| Language: | English |
| Published: |
Universiti Malaysia Perlis
2009
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| Online Access: | http://dspace.unimap.edu.my/xmlui/handle/123456789/5514 |
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