Name
Title | ||
|---|---|---|
Robust control design for a class of Unmanned Aerial Vehicle with parametric uncertainty |
Abstract | ||
|---|---|---|
In this paper, the modeling and robust control design of a vertical flight attitude control for a mini tail-sitter with variable pitch propeller is discussed. Tail-sitters Vertical Take-off and Landing - Unmanned Aerial Vehicles (VTOL-UAVs) have operational flexibility of typical helicopters while having the cruise performance of fixed wing airplanes. The configuration proposed in this work is highly unstable in its natural flight state in vertical mode. A simplified dynamic model is presented and a robust control design to stabilize the decoupled attitude systems in presence of uncertainty and time-delay is developed. The results are supported by simulation tests. |
Year | Venue | Keywords |
|---|---|---|
2009 | Control Conference | attitude control,autonomous aerial vehicles,control system synthesis,delays,helicopters,robust control,uncertain systems,vtol-uav,cruise performance,decoupled attitude systems,fixed wing airplanes,mini tail-sitter,natural flight state,operational fleńbility,parametric uncertainty,robust control design,simplified dynamic model,tail-sitters vertical take-off and landing,time-delay,unmanned aerial vehicle,variable pitch propeller,vertical flight attitude control,iron,decision support systems,uncertainty |
Field | DocType | ISBN |
Variable pitch propeller,Wing,Control theory,Decision support system,Attitude control,Control engineering,Parametric statistics,Engineering,Robust control,Cruise | Conference | 978-3-9524173-9-3 |
Citations | PageRank | References |
0 | 0.34 | 0 |
Authors | ||
5 | ||
Name | Order | Citations | PageRank |
|---|---|---|---|
| jairo a guerrero | 1 | 0 | 0.34 |
| gustavo e romero | 2 | 0 | 0.34 |
| David Lara | 3 | 3 | 1.20 |
| Rogelio Lozano | 4 | 914 | 166.62 |
| k c wong | 5 | 0 | 0.68 |