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...

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Bibliographic Details
Main Author: Aruneshwaran Rajashekaran.
Other Authors: School of Mechanical and Aerospace Engineering
Format: Theses and Dissertations
Language:English
Published: 2013
Subjects:
Online Access:http://hdl.handle.net/10356/53483
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Institution: Nanyang Technological University
Language: English

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