A Roll Controlling Approach for a Simple Dual-Actuated Flapping Aerial Vehicle Model

A Roll Controlling Approach for a Simple Dual-Actuated Flapping Aerial Vehicle Model

Aerial vehicles have been investigated recently in different contexts, due to their high potential of utilization in multiple application areas. Different mechanisms can be used for aerial vehicles actuation, such as the rotating multi-blade systems (Multi-Copters) and more recently flapping wings....

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Main Authors: Labib Omar El-Farouk E., El-Safty Sarah W., El-Kouly Mohamed H., Ramadan Mohamed M., Shehata Omar M., Morgan ElSayed I.
Format: Article
Language:English
Published: EDP Sciences 2016-01-01
Series:MATEC Web of Conferences
Online Access:http://dx.doi.org/10.1051/matecconf/20166810004
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spelling doaj-317776a76ec24d6d91f1b4cdd0453fad2021-04-02T09:07:53ZengEDP SciencesMATEC Web of Conferences2261-236X2016-01-01681000410.1051/matecconf/20166810004matecconf_iciea2016_10004A Roll Controlling Approach for a Simple Dual-Actuated Flapping Aerial Vehicle ModelLabib Omar El-Farouk E.El-Safty Sarah W.El-Kouly Mohamed H.Ramadan Mohamed M.Shehata Omar M.Morgan ElSayed I.Aerial vehicles have been investigated recently in different contexts, due to their high potential of utilization in multiple application areas. Different mechanisms can be used for aerial vehicles actuation, such as the rotating multi-blade systems (Multi-Copters) and more recently flapping wings. Flapping wing robots have attracted much attention from researchers in recent years. In this study, a simple dual-actuated flapping mechanism is proposed for actuating a flapping wing robot. The mechanism is designed, simulated and validated in both simulation and experiments. A roll controlling approach is proposed to control the roll angle of the robot via controlling the speeds of both motors actuating each of the wings. The results achieved are validated experimentally, and are promising opening the door for further investigation using our proposed systemhttp://dx.doi.org/10.1051/matecconf/20166810004
collection DOAJ
language English
format Article
sources DOAJ
author Labib Omar El-Farouk E.
El-Safty Sarah W.
El-Kouly Mohamed H.
Ramadan Mohamed M.
Shehata Omar M.
Morgan ElSayed I.
spellingShingle Labib Omar El-Farouk E.
El-Safty Sarah W.
El-Kouly Mohamed H.
Ramadan Mohamed M.
Shehata Omar M.
Morgan ElSayed I.
A Roll Controlling Approach for a Simple Dual-Actuated Flapping Aerial Vehicle Model
MATEC Web of Conferences
author_facet Labib Omar El-Farouk E.
El-Safty Sarah W.
El-Kouly Mohamed H.
Ramadan Mohamed M.
Shehata Omar M.
Morgan ElSayed I.
author_sort Labib Omar El-Farouk E.
title A Roll Controlling Approach for a Simple Dual-Actuated Flapping Aerial Vehicle Model
title_short A Roll Controlling Approach for a Simple Dual-Actuated Flapping Aerial Vehicle Model
title_full A Roll Controlling Approach for a Simple Dual-Actuated Flapping Aerial Vehicle Model
title_fullStr A Roll Controlling Approach for a Simple Dual-Actuated Flapping Aerial Vehicle Model
title_full_unstemmed A Roll Controlling Approach for a Simple Dual-Actuated Flapping Aerial Vehicle Model
title_sort roll controlling approach for a simple dual-actuated flapping aerial vehicle model
publisher EDP Sciences
series MATEC Web of Conferences
issn 2261-236X
publishDate 2016-01-01
description Aerial vehicles have been investigated recently in different contexts, due to their high potential of utilization in multiple application areas. Different mechanisms can be used for aerial vehicles actuation, such as the rotating multi-blade systems (Multi-Copters) and more recently flapping wings. Flapping wing robots have attracted much attention from researchers in recent years. In this study, a simple dual-actuated flapping mechanism is proposed for actuating a flapping wing robot. The mechanism is designed, simulated and validated in both simulation and experiments. A roll controlling approach is proposed to control the roll angle of the robot via controlling the speeds of both motors actuating each of the wings. The results achieved are validated experimentally, and are promising opening the door for further investigation using our proposed system
url http://dx.doi.org/10.1051/matecconf/20166810004
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