Name
Abstract | ||
|---|---|---|
The purpose of this paper is to present a new configuration of a vectored-thrust coaxial UAV(V-co-aX). The main characteristic of this vehicle is that it uses thrust vectoring for control in hover mode. A functional description of this mechanism is given and the Newton-Euler approach is applied to obtain the dynamic model of the flight platform. A non-linear controller based on saturation functions is proposed for stabilizing the vehicle in hover flight. Results presented include those from flight simulation of this configuration, and from experimentation obtained in real-time during the autonomous flight. |
Year | Venue | Keywords |
|---|---|---|
2009 | Control Conference | aerospace simulation,aircraft control,autonomous aerial vehicles,nonlinear control systems,robot dynamics,stability,newton-euler approach,v-co-ax dynamics,autonomous flight,dynamic model,flight platform,hover flight simulation,hover mode control,nonlinear controller,saturation functions,unmanned aerial vehicle,vectored-thrust coaxial uav control,vectored-thrust coaxial uav modelling,vehicle characteristic,vehicle stabilization,vehicle dynamics,torque,aerodynamics,mathematical model |
Field | DocType | ISBN |
Control theory,Thrust vectoring,Torque,Coaxial,Aerospace engineering,Vehicle dynamics,Flight simulator,Engineering,Thrust,Aerodynamics | Conference | 978-3-9524173-9-3 |
Citations | PageRank | References |
0 | 0.34 | 0 |
Authors | ||
4 | ||
Name | Order | Citations | PageRank |
|---|---|---|---|
| Octavio Garcia | 1 | 12 | 4.26 |
| Anand Sanchez | 2 | 33 | 6.24 |
| k c wong | 3 | 0 | 0.68 |
| Rogelio Lozano | 4 | 914 | 166.62 |