Modeling and control simulation of an unmanned aerial vehicle with multi-axisymmetric thrust vectoring nozzles
New breeds of high altitude vehicles are pushing the air traffic altitude boundary for higher flight efficiency and the atmospheric environment at higher altitudes will become thinner until it reaches the inoperable flight regime of traditional propeller and air breathing jet propulsion. Thrust Vect...
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| Format: | Thesis |
| Language: | English |
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2018
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| Online Access: | http://hdl.handle.net/10356/76130 |