Artificial Neural Network-Based Flight Control Using Distributed Sensors on Fixed-Wing Unmanned Aerial Vehicles
Author:
Affiliation:
1. University of Bristol
Publisher
American Institute of Aeronautics and Astronautics
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2. Wind tunnel testing of an avian-inspired morphing wing with distributed pressure sensing;2022 International Conference on Unmanned Aircraft Systems (ICUAS);2022-06-21
3. Simulation Study of Flow Field Integrated Flight Control in Highly Turbulent Conditions;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2022
4. An Adaptive Aeroservoelastic Model and Wind Tunnel Demonstration --- Pressure Control and Wing Deformation Estimation ---;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2022
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