Simulation of a machine learning based controller for a fixed-wing uav with distributed sensors
Simulation of a machine learning based controller for a fixed-wing uav with distributed sensors
Recent research suggests that the information obtained from arrays of sensors distributed on the wing of a fixed-wing small unmanned aerial vehicle (UAV) can provide information not available to conventional sensor suites. These arrays of sensors are capable of sensing the flow around the aircraft and it has been indicated that they could be a potential tool to improve flight control and overall flight performance. However, more work needs to be carried out to fully exploit the potential of these sensors for flight control. This work presents a 3 degrees-of-freedom longitudinal flight dynamics and control simulation model of a small fixed-wing UAV. Experimental readings of an array of pressure and strain sensors distributed across the wing were integrated in the model. This study investigated the feasibility of using machine learning to control airspeed of the UAV using the readings from the sensing array, and looked into the sensor layout and its effect on the performance of the controller. It was found that an artificial neural network was able to learn to mimic a conventional airspeed controller using only distributed sensor signals, but showed better performance for controlling changes in airspeed for a constant altitude than holding airspeed during changes in altitude. The neural network could control airspeed using either pressure or strain sensor information, but having both improved robustness to increased levels of turbulence. Results showed that some strain sensors and many pressure sensors signals were not necessary to achieve good controller performance, but that the pressure sensors near the leading edge of the wing were required. Future work will focus on replacing other elements of the flight control system with machine learning elements and investigate the use of reinforcement learning in place of supervised learning.
Fixed wing, Unmanned aerial vehicle (UAV), Machine Learning, Pressure sensors, Flight dynamics
18
American Institute of Aeronautics and Astronautics
Guerra-Langan, Ana
edc6a42b-6f6f-4beb-a188-3034b3e1ae97
Araujo-Estrada, Sergio
87793c63-f2bd-4169-b93d-ec1525909a7a
Richards, Arthur
758196b2-bfbd-4f4f-bc7e-1785d0969a42
Windsor, Shane
085351a4-b8c8-4b2d-ac3e-57877c7936d5
5 January 2020
Guerra-Langan, Ana
edc6a42b-6f6f-4beb-a188-3034b3e1ae97
Araujo-Estrada, Sergio
87793c63-f2bd-4169-b93d-ec1525909a7a
Richards, Arthur
758196b2-bfbd-4f4f-bc7e-1785d0969a42
Windsor, Shane
085351a4-b8c8-4b2d-ac3e-57877c7936d5
Guerra-Langan, Ana, Araujo-Estrada, Sergio, Richards, Arthur and Windsor, Shane
(2020)
Simulation of a machine learning based controller for a fixed-wing uav with distributed sensors.
In AIAA Scitech 2020 Forum.
vol. 1 PartF,
American Institute of Aeronautics and Astronautics.
.
(doi:10.2514/6.2020-1239).
Record type:
Conference or Workshop Item
(Paper)
Abstract
Recent research suggests that the information obtained from arrays of sensors distributed on the wing of a fixed-wing small unmanned aerial vehicle (UAV) can provide information not available to conventional sensor suites. These arrays of sensors are capable of sensing the flow around the aircraft and it has been indicated that they could be a potential tool to improve flight control and overall flight performance. However, more work needs to be carried out to fully exploit the potential of these sensors for flight control. This work presents a 3 degrees-of-freedom longitudinal flight dynamics and control simulation model of a small fixed-wing UAV. Experimental readings of an array of pressure and strain sensors distributed across the wing were integrated in the model. This study investigated the feasibility of using machine learning to control airspeed of the UAV using the readings from the sensing array, and looked into the sensor layout and its effect on the performance of the controller. It was found that an artificial neural network was able to learn to mimic a conventional airspeed controller using only distributed sensor signals, but showed better performance for controlling changes in airspeed for a constant altitude than holding airspeed during changes in altitude. The neural network could control airspeed using either pressure or strain sensor information, but having both improved robustness to increased levels of turbulence. Results showed that some strain sensors and many pressure sensors signals were not necessary to achieve good controller performance, but that the pressure sensors near the leading edge of the wing were required. Future work will focus on replacing other elements of the flight control system with machine learning elements and investigate the use of reinforcement learning in place of supervised learning.
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More information
Published date: 5 January 2020
Additional Information:
Funding Information:
This work is funded by the EPSRC Centre for Doctoral Training in Future Autonomous and Robotic Systems (FARSCOPE) at the Bristol Robotics Laboratory. This project has received funding from the European Research Council (ERC) under the European Union’s Horizon 2020 research and innovation programme (grant agreement No 679355).
Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
Venue - Dates:
AIAA Scitech Forum, 2020, , Orlando, United States, 2020-01-06 - 2020-01-10
Keywords:
Fixed wing, Unmanned aerial vehicle (UAV), Machine Learning, Pressure sensors, Flight dynamics
Identifiers
Local EPrints ID: 471094
URI: http://eprints.soton.ac.uk/id/eprint/471094
PURE UUID: a80692fb-57b5-4a27-8bca-528fb72f5789
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Date deposited: 25 Oct 2022 16:44
Last modified: 18 Mar 2024 04:06
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Contributors
Author:
Ana Guerra-Langan
Author:
Sergio Araujo-Estrada
Author:
Arthur Richards
Author:
Shane Windsor
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