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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主要作者: Adam Ain, Mohd Poin Keui
格式: Thesis
語言:English
出版: 2014
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在線閱讀:http://eprints.usm.my/28966/1/ATTITUDE_DETERMINATION_SYSTEM_FOR_NANO_SATELLITE_USING_EXTENDED_KALMAN_FILTER_ON_ARM7TDMI_PLATFORM.pdf
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