Towards a Unified Model-Free Control Architecture for Tailsitter Micro Air Vehicles: Flight Simulation Analysis and Experimental Flights
Author:
Affiliation:
1. French Civil Aviation University
2. Higher Institute of Aeronautics and Space
3. University of Lorraine
4. École Polytechnique
Publisher
American Institute of Aeronautics and Astronautics
Reference33 articles.
1. A discrete robust adaptive control of a tilt-rotor UAV for an enlarged flight envelope
2. Unified Velocity Control and Flight State Transition of Unmanned Tilt-Wing Aircraft
3. Development and experimental verification of a hybrid vertical take-off and landing (VTOL) unmanned aerial vehicle(UAV)
4. A Simple Controller for the Transition Maneuver of a Tail-Sitter Drone
5. Aerodynamic Characteristics of a Low Aspect Ratio Wing and Propeller Interaction for a Tilt-Body MAV
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1. Model-Free Control-Based Trajectory Tracking Control of a Tail-Sitter UAV in Hovering Mode;IEEE Transactions on Instrumentation and Measurement;2024
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3. Fault tolerance evaluation of model-free controllers with application to unmanned aerial vehicles;Drone Systems and Applications;2023-01-01
4. Implementation of a Neural Network for Nonlinearities Estimation in a Tail-Sitter Aircraft;Journal of Intelligent & Robotic Systems;2021-09-06
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