State- and Parameter Estimation for Spacecraft with Flexible Appendages using Unscented Kalman Filters
The problem of system identification for dynamic effects on spacecraft has become increasingly relevant with the surge of agile spacecraft, which must perform large amplitude maneuvers at high rates. Precise knowledge of the state of the spacecraft, as well as of the parameters characterizing its mo...
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| Format: | Others |
| Language: | English |
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Luleå tekniska universitet, Institutionen för system- och rymdteknik
2019
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-76320 |