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...

Szczegółowa specyfikacja

Opis bibliograficzny
1. autor: Aruneshwaran Rajashekaran.
Kolejni autorzy: School of Mechanical and Aerospace Engineering
Format: Praca dyplomowa
Język:English
Wydane: 2013
Hasła przedmiotowe:
Dostęp online:http://hdl.handle.net/10356/53483

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