An aerial deployed unmanned glider for cross-Channel flight

This paper describes the technical and operational challenges of the first cross-Channel flight performed by an unmanned autonomous glider. The glider chosen for the attempt was a quarter scale Slingsby Type 45 Swallow. It was found to have a lift-to-drag ratio of 8, as verified by wind tunnel force...

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Main Author: Jabbal, Mark
Format: Article
Published: Marques Aviation Press 2015
Online Access:https://eprints.nottingham.ac.uk/46297/
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author Jabbal, Mark
author_facet Jabbal, Mark
author_sort Jabbal, Mark
building Nottingham Research Data Repository
collection Online Access
description This paper describes the technical and operational challenges of the first cross-Channel flight performed by an unmanned autonomous glider. The glider chosen for the attempt was a quarter scale Slingsby Type 45 Swallow. It was found to have a lift-to-drag ratio of 8, as verified by wind tunnel force balance tests. Essential retrospective aerodynamic refinements to the design, including modifications of the wing root and tip sections and wing aspect ratio, were modelled analytically and found to increase the aircraft’s lift-to-drag ratio to 19. The launch mechanism devised for the modified glider featured a bespoke crate suspended under an airborne helicopter at an altitude of 10,000 ft, from which the aircraft was released from an internal recess. The glider was pre-programmed to fly autonomously via waypoint navigation and completed the 22 mile mission in less than one hour at an average ground speed of 27 knots, a sink rate of 3 ft/s and with 3,500 ft altitude to spare. The successful flight, which was filmed from onboard cameras and a chase helicopter, represents a unique first in autonomous aviation and is unofficially the longest straight distance flight for an unmanned engineless glider.
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spelling nottingham-462972020-05-04T17:09:18Z https://eprints.nottingham.ac.uk/46297/ An aerial deployed unmanned glider for cross-Channel flight Jabbal, Mark This paper describes the technical and operational challenges of the first cross-Channel flight performed by an unmanned autonomous glider. The glider chosen for the attempt was a quarter scale Slingsby Type 45 Swallow. It was found to have a lift-to-drag ratio of 8, as verified by wind tunnel force balance tests. Essential retrospective aerodynamic refinements to the design, including modifications of the wing root and tip sections and wing aspect ratio, were modelled analytically and found to increase the aircraft’s lift-to-drag ratio to 19. The launch mechanism devised for the modified glider featured a bespoke crate suspended under an airborne helicopter at an altitude of 10,000 ft, from which the aircraft was released from an internal recess. The glider was pre-programmed to fly autonomously via waypoint navigation and completed the 22 mile mission in less than one hour at an average ground speed of 27 knots, a sink rate of 3 ft/s and with 3,500 ft altitude to spare. The successful flight, which was filmed from onboard cameras and a chase helicopter, represents a unique first in autonomous aviation and is unofficially the longest straight distance flight for an unmanned engineless glider. Marques Aviation Press 2015-07-01 Article PeerReviewed Jabbal, Mark (2015) An aerial deployed unmanned glider for cross-Channel flight. International Journal of Unmanned Systems Engineering, 3 (3). pp. 1-20. ISSN 2052-112X http://www.ijuseng.com/#/ijuseng-3-3-1-20-2015/4589235982 doi:10.14323/ijuseng.2015.9 doi:10.14323/ijuseng.2015.9
spellingShingle Jabbal, Mark
An aerial deployed unmanned glider for cross-Channel flight
title An aerial deployed unmanned glider for cross-Channel flight
title_full An aerial deployed unmanned glider for cross-Channel flight
title_fullStr An aerial deployed unmanned glider for cross-Channel flight
title_full_unstemmed An aerial deployed unmanned glider for cross-Channel flight
title_short An aerial deployed unmanned glider for cross-Channel flight
title_sort aerial deployed unmanned glider for cross-channel flight
url https://eprints.nottingham.ac.uk/46297/
https://eprints.nottingham.ac.uk/46297/
https://eprints.nottingham.ac.uk/46297/