Robust control system development forVTOL-to-fixed wing flight transition withthe EcoSoar UAV : A masters thesis in Automatic Control
A non switching, non linear, quaternion based attitude P2 controller, together with a sensitivitynormalizing function for the control surfaces has been simulated and implemented on a flying fixedwing with non vectored engines. In simulations the controller worked well in all flight modes,hovering, t...
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| Format: | Others |
| Language: | English |
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Luleå tekniska universitet, Institutionen för system- och rymdteknik
2020
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-81000 |