Abstract
This study deals with modeling and flight control of quadrotor type (QRT) unmanned aerial vehicles (UAVs). Rigorous dynamic model of a QRT UAV is obtained both in reference and body frame coordinate systems. A disturbance observer (DOB) based controller using the derived dynamic models is also proposed for robust hovering control. The control input induced by DOB is helpful to use simple equations of motion satisfying accurate derived dynamics. The experimental results show the performance of the proposed control algorithm.
| Original language | English |
|---|---|
| Pages (from-to) | 1260-1265 |
| Number of pages | 6 |
| Journal | Journal of Institute of Control, Robotics and Systems |
| Volume | 14 |
| Issue number | 12 |
| DOIs | |
| State | Published - Dec 2008 |
Keywords
- Hovering control
- QRT (Quadrotor type)
- UAV (Unmanned Aerial Vehicle)
- VTOL (Vertical Take-off and Landing)