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String-based flapping mechanism and modularized trailing edge control system for insect-type FWMAV
Author(s) -
Gong DuHyun,
Lee DaWoon,
Shin SangJoon,
Kim SangYong
Publication year - 2019
Publication title -
international journal of micro air vehicles
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.324
H-Index - 21
eISSN - 1756-8307
pISSN - 1756-8293
DOI - 10.1177/1756829319842547
Subject(s) - flapping , mechanism (biology) , trailing edge , string (physics) , lift (data mining) , enhanced data rates for gsm evolution , engineering , leading edge , process (computing) , computer science , aerospace engineering , wing , structural engineering , physics , telecommunications , quantum mechanics , data mining , operating system
This paper presents the design process and experimental results of a brand new flapping and trailing edge control mechanism for a flapping wing micro air vehicle. The flapping mechanism, whose main components are fabricated from string, is suggested and optimized further by a modified pattern search method. The trailing edge control mechanisms for pitching and rolling moments are designed to be attached onto the present flapping mechanism in a modularized fashion. Prototypes of both mechanisms are fabricated and experimentally tested in order to examine the feasibility of the designs. It is expected that the present flapping mechanism will generate enough lift for the total weight of the vehicle. The present control mechanism is found to be able to supply sufficient control moment.

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