Differential Flatness of Lifting-Wing Quadcopters Subject to Drag and Lift for Accurate Tracking
Author:
Affiliation:
1. School of Automation Science and Electrical Engineering, Beihang University, Beijing, China
Funder
National Natural Science Foundation of China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Link
http://xplorestaging.ieee.org/ielx7/41/10589453/10438088.pdf?arnumber=10438088
Reference26 articles.
1. A review on the platform design, dynamic modeling and control of hybrid UAVs
2. Review of designs and flight control techniques of hybrid and convertible VTOL UAVs
3. Performance Evaluation and Design Method of Lifting-wing Multicopters
4. Development of a quad rotor tail-sitter VTOL UAV without control surfaces and experimental verification
5. A Lifting Wing Fixed on Multirotor UAVs for Long Flight Ranges
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