Design and analysis performance of fixed wing VTOL UAV
Mainly there is two type of UAV, multirotor and fixed wing and each of this type have their own advantages. Combination of both type UAV can enhance the capability of UAV. The problem to this idea are the effect of modification on thrust performance as the wing loading increase. This study presents...
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Journal of Transport System Engineering
2018
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my.utm.823142019-11-24T04:46:08Z http://eprints.utm.my/id/eprint/82314/ Design and analysis performance of fixed wing VTOL UAV Ab. Wahid, Mastura Othman, Norazila Md. Zain, Mohd. Zarhamdy Mohd. Nasir, Mohd. Nazri Jamaludin, Mohd. Fadhil TJ Mechanical engineering and machinery Mainly there is two type of UAV, multirotor and fixed wing and each of this type have their own advantages. Combination of both type UAV can enhance the capability of UAV. The problem to this idea are the effect of modification on thrust performance as the wing loading increase. This study presents a conceptual design of fixed wing vertical take-off and landing (VTOL) UAV based on ready-to-fly (RTF) fixed wing UAV. This mean the UAV has ability not only to take-off, landing or hover as multirotor aircraft but also able to cruise similar to the fixed wing UAV. This paper discussed on the design modification of fixed wing UAV and thrust performance for take-off, hover and landing during multirotor mode. Mass balance analysis is performed to ensure that addition and placement of motors and other equipment are in such way the center of gravity does not change from the original UAV to retain its original stability. For the thrust performance, thrust required for multirotor mode is compared with the thrust available produce by the motors obtained by doing the thrust test. Based on the analysis, the capability of UAV to fulfil the mission requirement is determined. Journal of Transport System Engineering 2018 Article PeerReviewed Ab. Wahid, Mastura and Othman, Norazila and Md. Zain, Mohd. Zarhamdy and Mohd. Nasir, Mohd. Nazri and Jamaludin, Mohd. Fadhil (2018) Design and analysis performance of fixed wing VTOL UAV. Journal of Transport System Engineering, 5 (1). pp. 17-25. ISSN 2289-9790 https://jtse.utm.my |
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TJ Mechanical engineering and machinery Ab. Wahid, Mastura Othman, Norazila Md. Zain, Mohd. Zarhamdy Mohd. Nasir, Mohd. Nazri Jamaludin, Mohd. Fadhil Design and analysis performance of fixed wing VTOL UAV |
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Mainly there is two type of UAV, multirotor and fixed wing and each of this type have their own advantages. Combination of both type UAV can enhance the capability of UAV. The problem to this idea are the effect of modification on thrust performance as the wing loading increase. This study presents a conceptual design of fixed wing vertical take-off and landing (VTOL) UAV based on ready-to-fly (RTF) fixed wing UAV. This mean the UAV has ability not only to take-off, landing or hover as multirotor aircraft but also able to cruise similar to the fixed wing UAV. This paper discussed on the design modification of fixed wing UAV and thrust performance for take-off, hover and landing during multirotor mode. Mass balance analysis is performed to ensure that addition and placement of motors and other equipment are in such way the center of gravity does not change from the original UAV to retain its original stability. For the thrust performance, thrust required for multirotor mode is compared with the thrust available produce by the motors obtained by doing the thrust test. Based on the analysis, the capability of UAV to fulfil the mission requirement is determined. |
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Article |
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Ab. Wahid, Mastura Othman, Norazila Md. Zain, Mohd. Zarhamdy Mohd. Nasir, Mohd. Nazri Jamaludin, Mohd. Fadhil |
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Ab. Wahid, Mastura Othman, Norazila Md. Zain, Mohd. Zarhamdy Mohd. Nasir, Mohd. Nazri Jamaludin, Mohd. Fadhil |
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Ab. Wahid, Mastura |
title |
Design and analysis performance of fixed wing VTOL UAV |
title_short |
Design and analysis performance of fixed wing VTOL UAV |
title_full |
Design and analysis performance of fixed wing VTOL UAV |
title_fullStr |
Design and analysis performance of fixed wing VTOL UAV |
title_full_unstemmed |
Design and analysis performance of fixed wing VTOL UAV |
title_sort |
design and analysis performance of fixed wing vtol uav |
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Journal of Transport System Engineering |
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2018 |
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http://eprints.utm.my/id/eprint/82314/ https://jtse.utm.my |
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13.18916 |