Guidance, navigation and control of a small, unmanned blended wing body aircraft
The purpose of this research is to document the design and optimisation of a full suite of guidance, navigation and control (GNC) algorithms for a small unmanned aerial vehicle (UAV), the Skywalker X8. This was performed so as to fill a void in the available literature on the selected airframe, whic...
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Format: | Dissertation |
Language: | English |
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Faculty of Engineering and the Built Environment
2020
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Online Access: | http://hdl.handle.net/11427/32426 |