Model free adaptive control design for a tilt trirotor unmanned aerial vehicle with quaternion feedback: Theory and implementation
Author:
Affiliation:
1. The Institute of Robotics and Autonomous System, School of Electrical and Information Engineering Tianjin University Tianjin China
2. School of Electronic and Communication Engineering Guiyang University Guiyang China
Funder
National Natural Science Foundation of China
Publisher
Wiley
Subject
Electrical and Electronic Engineering,Signal Processing,Control and Systems Engineering
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/acs.3344
Reference27 articles.
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4. EscarenoJ SanchezA GarciaO LozanoR.Triple tilting rotor mini‐UAV: modeling and embedded control of the attitude. Proceedings of the 2008 American Control Conference; 2008:3476‐3481. doi:10.1109/ACC.2008.4587031
5. Salazar‐CruzS LozanoR.Stabilization and nonlinear control for a novel trirotor mini‐aircraft. Proceedings of the 2005 IEEE International Conference on Robotics and Automation; 2005:2612‐2617. doi:10.1109/ROBOT.2005.1570507
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