Abstract
This paper presents attitude recovery control for a quad tilt rotor UAV. The quad tilt rotor UAV has ability of flying with completely independent 3 DOF position and 3 DOF attitude control by changing the thrust directions. This type of UAV is expected to perform better response to the disturbance by virtue of the mechanism of changing the thrust directions compared to the conventional multi-rotor UAV. This paper proposes disturbance detection method using IMU sensor and develops attitude recovery control against impact disturbance. The numerical simulation and fundamental flight experiments were carried out to evaluate the effectiveness of the proposed method compared to the conventional PID control.
| Original language | English |
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| Title of host publication | ICCAS 2016 - 2016 16th International Conference on Control, Automation and Systems, Proceedings |
| Publisher | IEEE Computer Society |
| Pages | 709-712 |
| Number of pages | 4 |
| ISBN (Electronic) | 9788993215120 |
| DOIs | |
| Publication status | Published - 2017 Jan 24 |
| Event | 16th International Conference on Control, Automation and Systems, ICCAS 2016 - Gyeongju, Korea, Republic of Duration: 2016 Oct 16 → 2016 Oct 19 |
Other
| Other | 16th International Conference on Control, Automation and Systems, ICCAS 2016 |
|---|---|
| Country/Territory | Korea, Republic of |
| City | Gyeongju |
| Period | 16/10/16 → 16/10/19 |
Keywords
- Attitude recovery flight
- Impact disturbance
- Tilt rotor aircraft
- Unmanned Aerial Vehicle (UAV)
ASJC Scopus subject areas
- Artificial Intelligence
- Computer Science Applications
- Control and Systems Engineering
- Electrical and Electronic Engineering