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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書目詳細資料
主要作者: Anon
格式: Other
語言:English
出版: Universiti Malaysia Perlis 2009
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在線閱讀:http://dspace.unimap.edu.my/xmlui/handle/123456789/5514
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