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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: | Thesis |
| Language: | English |
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Department of Mechanical Engineering
2020
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