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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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Bibliographic Details
Main Author: Anon
Format: Other
Language:English
Published: Universiti Malaysia Perlis 2009
Subjects:
InnoSAT
Attitude control algorithms
UniMAP > Research and development
Higher education > Research and development
UniMAP > Achievement, Research
Online Access:http://dspace.unimap.edu.my/xmlui/handle/123456789/5514
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http://dspace.unimap.edu.my/xmlui/handle/123456789/5514

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