Flies compensate for unilateral wing damage through modular adjustments of wing and body kinematics
Author(s) -
Florian T. Muijres,
Nicole A. Iwasaki,
Michael J. Elzinga,
Johan M. Melis,
Michael H. Dickinson
Publication year - 2016
Publication title -
interface focus
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 1.1
H-Index - 49
eISSN - 2042-8901
pISSN - 2042-8898
DOI - 10.1098/rsfs.2016.0103
Subject(s) - wing , kinematics , flapping , torque , wing loading , washout , wing twist , lift (data mining) , control theory (sociology) , insect flight , mechanics , computer science , structural engineering , simulation , angle of attack , physics , aerodynamics , engineering , classical mechanics , control (management) , artificial intelligence , meteorology , data mining , thermodynamics
Using high-speed videography, we investigated how fruit flies compensate for unilateral wing damage, in which loss of area on one wing compromises both weight support and roll torque equilibrium. Our results show that flies control for unilateral damage by rolling their body towards the damaged wing and by adjusting the kinematics of both the intact and damaged wings. To compensate for the reduction in vertical lift force due to damage, flies elevate wingbeat frequency. Because this rise in frequency increases the flapping velocity of both wings, it has the undesired consequence of further increasing roll torque. To compensate for this effect, flies increase the stroke amplitude and advance the timing of pronation and supination of the damaged wing, while making the opposite adjustments on the intact wing. The resulting increase in force on the damaged wing and decrease in force on the intact wing function to maintain zero net roll torque. However, the bilaterally asymmetrical pattern of wing motion generates a finite lateral force, which flies balance by maintaining a constant body roll angle. Based on these results and additional experiments using a dynamically scaled robotic fly, we propose a simple bioinspired control algorithm for asymmetric wing damage.
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