Bio-inspired distributed strain and airflow sensing for small unmanned air vehicle flight control
Bio-inspired distributed strain and airflow sensing for small unmanned air vehicle flight control
Flying animals such as birds, bats and insects all have extensive arrays of sensory or- gans distributed in their wings which provide them with detailed information about the airflow over their wings and the forces generated by this airflow. Using two small modified unmanned air vehicle platforms (UAVs), one with a distributed array of 12 strain gauge sensors and one with a chord-wise array of 4 pressure sensors, we have examined the dis- tribution of the strain and air pressure signals over the UAV wings in relation to flight conditions, including wind tunnel testing, indoor free flight and outdoor free flight. We have also characterised the signals provided by controlled gusts and natural turbulence. These sensors were then successfully used to control roll motions in the case of the strain sensor platform and pitch motions in the case of the pressure sensor platform. These results suggest that distributed mechanosensing and airflow sensing both offer advantages beyond traditional flight control based on rigid body state estimation using inertial sensing. These advantages include stall detection, gust alleviation and model-free measurement of aerodynamic forces. These advantages are likely to be important in the development of future aircraft with increasing numbers of degrees of freedom both through flexibility and active morphing.
American Institute of Aeronautics and Astronautics
Araujo-Estrada, Sergio A.
87793c63-f2bd-4169-b93d-ec1525909a7a
Salama, Francis
5ff27972-41d4-493c-8436-99d3934765e7
Greatwood, Colin
84322681-5128-47ba-83cb-b9d08a1ffa28
Wood, Kieran
62b723b9-85b5-4efc-9054-35c561e6a2ac
Richardson, Thomas
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Windsor, Shane P.
085351a4-b8c8-4b2d-ac3e-57877c7936d5
9 January 2017
Araujo-Estrada, Sergio A.
87793c63-f2bd-4169-b93d-ec1525909a7a
Salama, Francis
5ff27972-41d4-493c-8436-99d3934765e7
Greatwood, Colin
84322681-5128-47ba-83cb-b9d08a1ffa28
Wood, Kieran
62b723b9-85b5-4efc-9054-35c561e6a2ac
Richardson, Thomas
b2a5cea9-423c-4958-b808-f5d2b69b4e83
Windsor, Shane P.
085351a4-b8c8-4b2d-ac3e-57877c7936d5
Araujo-Estrada, Sergio A., Salama, Francis, Greatwood, Colin, Wood, Kieran, Richardson, Thomas and Windsor, Shane P.
(2017)
Bio-inspired distributed strain and airflow sensing for small unmanned air vehicle flight control.
In AIAA Guidance, Navigation, and Control Conference, 2017.
American Institute of Aeronautics and Astronautics.
19 pp
.
(doi:10.2514/6.2017-1487).
Record type:
Conference or Workshop Item
(Paper)
Abstract
Flying animals such as birds, bats and insects all have extensive arrays of sensory or- gans distributed in their wings which provide them with detailed information about the airflow over their wings and the forces generated by this airflow. Using two small modified unmanned air vehicle platforms (UAVs), one with a distributed array of 12 strain gauge sensors and one with a chord-wise array of 4 pressure sensors, we have examined the dis- tribution of the strain and air pressure signals over the UAV wings in relation to flight conditions, including wind tunnel testing, indoor free flight and outdoor free flight. We have also characterised the signals provided by controlled gusts and natural turbulence. These sensors were then successfully used to control roll motions in the case of the strain sensor platform and pitch motions in the case of the pressure sensor platform. These results suggest that distributed mechanosensing and airflow sensing both offer advantages beyond traditional flight control based on rigid body state estimation using inertial sensing. These advantages include stall detection, gust alleviation and model-free measurement of aerodynamic forces. These advantages are likely to be important in the development of future aircraft with increasing numbers of degrees of freedom both through flexibility and active morphing.
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Araujo_Estrada_2017_BioInspDistStrain&AirflowSensSUAVFlightCtrl_accepted
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Published date: 9 January 2017
Additional Information:
Funding Information:
The authors would like to thank Mr Lee Winter from the University of Bristol wind tunnel laboratory, for his invaluable support and work during the assembly of the pressure ports in the pressure sensing platform used to carry out the experiments presented in this paper. The work presented in this paper was partially funded by the Defence Science and Technology Laboratory (DSTL), under contract numbers DSTLX-1000079686 and DSTLX-1000097967. 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:
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
Venue - Dates:
AIAA Guidance, Navigation, and Control Conference, 2017, , Grapevine, United States, 2017-01-09 - 2017-01-13
Identifiers
Local EPrints ID: 471154
URI: http://eprints.soton.ac.uk/id/eprint/471154
PURE UUID: 33f33f19-9e7c-459e-b392-1a1c2d94bf67
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Date deposited: 28 Oct 2022 16:37
Last modified: 18 Mar 2024 04:06
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Contributors
Author:
Sergio A. Araujo-Estrada
Author:
Francis Salama
Author:
Colin Greatwood
Author:
Kieran Wood
Author:
Thomas Richardson
Author:
Shane P. Windsor
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