Controlador lineal y no lineal para un micro vehículo aéreo no tripulado con configuración de quadrotor
Linear quadratic regulator and nonlinear backstepping control design are studied for a micro unmanned aerial vehicle named quadrotor. The controller design is based on a nonlinear mathematical model, which is linearized for the case of lineal control design. The study of the obtained dynamics is eva...
Uloženo v:
| Vydáno v: | Revista INGENIERÍA UC |
|---|---|
| Hlavní autoři: | , |
| Médium: | Artigo |
| Jazyk: | Espanhol |
| Vydáno: |
Universidad de Carabobo
2016
|
| Témata: | |
| On-line přístup: | https://www.redalyc.org/articulo.oa?id=70748810003 |
| Tagy: |
Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!
|