Nonlinear dynamic inversion controller for a ducted-fan UAV
Small ducted fan aerial unmanned aerial vehicles possess hover and vertical take-off and landing capabilities in addition to normal high speed flight. With autonomous flight control system these vehicles have several applications especially for mission in urban environment. This thesis is about deve...
| Hoofdauteur: | |
|---|---|
| Andere auteurs: | |
| Formaat: | Thesis |
| Taal: | English |
| Gepubliceerd in: |
2013
|
| Onderwerpen: | |
| Online toegang: | http://hdl.handle.net/10356/53483 |