Preliminary structural integrity investigation for quadcopter frame to be deployed for pest control

Please use this identifier to cite or link to this item: http://ir.futminna.edu.ng:8080/jspui/handle/123456789/9863

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DC Field	Value	Language
dc.contributor.author	Sulaiman, Ibrahim	-
dc.contributor.author	Babawuya, Alkali	-
dc.contributor.author	adedipe, Oyewale	-
dc.contributor.author	Salihu, Bala Alhaji	-
dc.contributor.author	Aliyu, Alhaji Abdullahi	-
dc.contributor.author	Ibrahim, Aku G.	-
dc.date.accessioned	2021-07-16T09:08:16Z	-
dc.date.available	2021-07-16T09:08:16Z	-
dc.date.issued	2020-12	-
dc.identifier.issn	978-967-2454-36-6	-
dc.identifier.uri	http://repository.futminna.edu.ng:8080/jspui/handle/123456789/9863	-
dc.description.abstract	– Quadcopters are one of the most versatile unmanned aerial vehicles deployed for various purposes. In this study it is going to be used as part of a system used for bird control therefore the structural integrity is investigated. The aim of the paper is to investigate the structural and aerodynamic behaviour of a quadcopter intended for bird control. A model of the drone has been developed in SolidWorks, then structural along with flow analysis carried out using ANSYS software. The structural analysis shows promising results as the stress built up due to the loads applied are within the safe range.	en_US
dc.language.iso	en	en_US
dc.publisher	Universiti teknikal Malaysia Maleka	en_US
dc.relation.ispartofseries	;MERD '20 ID 124	-
dc.subject	Quadcopters	en_US
dc.subject	structure	en_US
dc.subject	Analysis	en_US
dc.title	Preliminary structural integrity investigation for quadcopter frame to be deployed for pest control	en_US
dc.type	Article	en_US
Appears in Collections:	Mechatronics Engineering

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