The Unified Tracking Controller for a Tilt-Rotor Unmanned Aerial Vehicle Based on the Dual Quaternion
Author:
Affiliation:
1. Sichuan University - Pittsburgh Institute,Department of Mechanical Engineering,Chengdu,China
Funder
National Natural Science Foundation of China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9986510/9986514/09986880.pdf?arnumber=9986880
Reference27 articles.
1. Modeling and Control of port dynamics of a tilt-rotor quadcopter
2. Modeling and Control of a Passively-Coupled Tilt-Rotor Vertical Takeoff and Landing Aircraft
3. Dynamic Model and Control of an Over-actuated Quadrotor UAV
4. Modeling and Control of a Tethered Tilt-Rotor Quadcopter with Atmospheric Wind Model
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