Dynamics of a small unmanned aircraft parachute system

Panta, A, Watkins, S and Clothier, R 2018, 'Dynamics of a small unmanned aircraft parachute system', Journal of Aerospace Technology and Management, vol. 10, pp. 1-14.

Document type: Journal Article
Collection: Journal Articles

Title Dynamics of a small unmanned aircraft parachute system
Author(s) Panta, A
Watkins, S
Clothier, R
Year 2018
Journal name Journal of Aerospace Technology and Management
Volume number 10
Start page 1
End page 14
Total pages 14
Publisher Instituto de Aeronautica e Espaco (I A E)
Abstract Parachute Systems (PS) can be readily used by small Unmanned Aircraft Systems (UAS) for risk mitigation and aircraft recovery. To date there has been limited research into the fundamental dynamics of parachutes at low Reynolds numbers, with existing studies focusing on larger parachutes. An understanding of the dynamics is needed to establish sound guidelines for parachute design and for their use during UAS operations. Existing design guidelines are reviewed and the key parachute design parameters are identified. The validity of the existing guidelines applied to lower Reynolds number parachutes is explored through a series of wind-tunnel tests. It was found that existing design guidelines under predict the key parameters of inflation time and peak forces for parachute deployments at typical UAS operating speeds. The ramifications on the design and operation of small UAS are discussed.
Subject Aerodynamics (excl. Hypersonic Aerodynamics)
Flight Dynamics
Keyword(s) Parachute
DOI - identifier 10.5028/jatm.v10.752
ISSN 1984-9648
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Citation counts: TR Web of Science Citation Count  Cited 3 times in Thomson Reuters Web of Science Article | Citations
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