Thrust command based Integrated Reference Model with Envelope Protections for Tilt-rotor VTOL Transition UAV
Author:
Affiliation:
1. Technical University of Munich
Publisher
American Institute of Aeronautics and Astronautics
Reference21 articles.
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2. Attitude Free Position Control of a Quadcopter using Dynamic Inversion
3. Position tracking of a hexacopter using a geometric backstepping control law - Experimental results
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