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Design, Manufacturing and Experiment...

Balta Manich, Miquel.

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Design, Manufacturing and Experimental Investigations of Flapping Wing Micro Air Vehicles.

Record Type:	Electronic resources : Monograph/item
Title/Author:	Design, Manufacturing and Experimental Investigations of Flapping Wing Micro Air Vehicles./
Author:	Balta Manich, Miquel.
Published:	Ann Arbor : ProQuest Dissertations & Theses, : 2018,
Description:	194 p.
Notes:	Source: Masters Abstracts International, Volume: 80-10.
Contained By:	Masters Abstracts International80-10.
Subject:	Fluid mechanics. -
Online resource:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=13418958
ISBN:	9781392001691

Design, Manufacturing and Experimental Investigations of Flapping Wing Micro Air Vehicles.
Balta Manich, Miquel.

Design, Manufacturing and Experimental Investigations of Flapping Wing Micro Air Vehicles. - Ann Arbor : ProQuest Dissertations & Theses, 2018 - 194 p.

Source: Masters Abstracts International, Volume: 80-10.

Thesis (M.S.)--University of California, Irvine, 2018.

This item must not be sold to any third party vendors.

Flapping Wing Micro Air Vehicles (FWMAVs) are micro bioinspired systems which use flapping wings actuation to move in the environment. Stringent size, weight, and power constraints make their design quite challenging. In particular, the flapping actuation mechanism represents a corner stone in the design of the whole vehicle, if not the most challenging task. In this thesis, we provide a review about several designs of flapping wing vehicles in literature. The main idea stems from a double crank rocker mechanism that passively controls the pitch angle. Implementing a new design methodology and some manufacturing iterations, we develop a novel mechanism actively controls both the wing flapping (back and forth) and pitching motions using only one drive motor. We developed three experimental setups to test different aspects of the mechanisms. A one-degree-of-freedom (DoF) pendulum-like to determine the average lift and power. The load cell and laser to measure the lift time history during the cycle, which allow validation of our un-steady aerodynamic model. Finally, a flow visualization setup sheds some light on the in-teraction between the FWMAV dynamics and flow vertical dynamics.

ISBN: 9781392001691Subjects--Topical Terms:

528155
Fluid mechanics.
Subjects--Index Terms:

Active control

Design, Manufacturing and Experimental Investigations of Flapping Wing Micro Air Vehicles.
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100 1 $a Balta Manich, Miquel. $3 3544998
245 1 0 $a Design, Manufacturing and Experimental Investigations of Flapping Wing Micro Air Vehicles.
260 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2018
300 $a 194 p.
500 $a Source: Masters Abstracts International, Volume: 80-10.
500 $a Publisher info.: Dissertation/Thesis.
500 $a Advisor: Taha, Haithem E.
502 $a Thesis (M.S.)--University of California, Irvine, 2018.
506 $a This item must not be sold to any third party vendors.
520 $a Flapping Wing Micro Air Vehicles (FWMAVs) are micro bioinspired systems which use flapping wings actuation to move in the environment. Stringent size, weight, and power constraints make their design quite challenging. In particular, the flapping actuation mechanism represents a corner stone in the design of the whole vehicle, if not the most challenging task. In this thesis, we provide a review about several designs of flapping wing vehicles in literature. The main idea stems from a double crank rocker mechanism that passively controls the pitch angle. Implementing a new design methodology and some manufacturing iterations, we develop a novel mechanism actively controls both the wing flapping (back and forth) and pitching motions using only one drive motor. We developed three experimental setups to test different aspects of the mechanisms. A one-degree-of-freedom (DoF) pendulum-like to determine the average lift and power. The load cell and laser to measure the lift time history during the cycle, which allow validation of our un-steady aerodynamic model. Finally, a flow visualization setup sheds some light on the in-teraction between the FWMAV dynamics and flow vertical dynamics.
590 $a School code: 0030.
650 4 $a Fluid mechanics. $3 528155
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Mechanical engineering. $3 649730
653 $a Active control
653 $a Flapping wing micro air vehicles
653 $a Mechanism
653 $a Micro air vehicles
653 $a Passive control
653 $a Pitching angle
690 $a 0204
690 $a 0538
690 $a 0548
710 2 $a University of California, Irvine. $b Mechanical and Aerospace Engineering. $3 2093977
773 0 $t Masters Abstracts International $g 80-10.
790 $a 0030
791 $a M.S.
792 $a 2018
793 $a English
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=13418958