Modelling, attitude controller design and flight experiments of a novel micro-ducted-fan aircraft
This research concerns a novel micro-ducted-fan aircraft. A structured attitude controller is designed for a novel unmanned aerial vehicle in the presence of strong state coupling and system perturbation. The novel unmanned aerial vehicle is equipped with two tandem ducted fans to provide the main t...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
SAGE Publishing
2018-03-01
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| Series: | Advances in Mechanical Engineering |
| Online Access: | https://doi.org/10.1177/1687814018765569 |