Unscented Kalman Filters for Attitude and Orbit Estimation of a Low Earth Orbit CubeSat
In this paper two Unscented Kalman Filters (UKF) are implemented to solve the estimation of a satellite's position in orbit and its orientation relative to Earth's Centered Inertial frame. Their aim is to see if an absolute position accuracy of less than 1 km and an orientation estimation...
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| Format: | Others |
| Language: | English |
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KTH, Rymd- och plasmafysik
2015
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-160616 |