Attitude Determination System For Nano Satellite Using Extended Kalman Filter On ARM7TDMI Platform

Extended Kalman Filter (EKF) has been successfully utilized in satellites missions. However, in comparison to other attitude determination methods developed, it is one of the most computationally burdening algorithm and with the new development of using nano satellites which have limited electric...

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Bibliographic Details
Main Author: Adam Ain, Mohd Poin Keui
Format: Thesis
Language:English
Published: 2014
Subjects:
Online Access:http://eprints.usm.my/28966/1/ATTITUDE_DETERMINATION_SYSTEM_FOR_NANO_SATELLITE_USING_EXTENDED_KALMAN_FILTER_ON_ARM7TDMI_PLATFORM.pdf
http://eprints.usm.my/28966/
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