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...

詳細記述

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書誌詳細
第一著者: Anon
フォーマット: Other
言語:English
出版事項: Universiti Malaysia Perlis 2009
主題:
オンライン・アクセス:http://dspace.unimap.edu.my/xmlui/handle/123456789/5514
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