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Design and Analysis of Recovery Net Landing for UAV ALUDRA MR-01

This report discusses the final analysis and finite element analysis (FEA) of chosen topic, which is Design and Analysis of Recovery Net Landing for UAV ALUDRA MR-01. The objective of this research is to design analysis recovery net landing system for ALUDRA MR-01 with maximum take–off weight 40kg w...

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Main Author: Abu, Fadhilatul Hikmah
Format: Final Year Project
Language:English
Published: Universiti Teknologi Petronas 2013
Subjects:
TJ Mechanical engineering and machinery
Online Access:http://utpedia.utp.edu.my/10826/1/FADHILATUL_15529_FINAL_DISSERTATION.pdf
http://utpedia.utp.edu.my/10826/
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spelling my-utp-utpedia.108262017-01-25T09:38:22Z http://utpedia.utp.edu.my/10826/ Design and Analysis of Recovery Net Landing for UAV ALUDRA MR-01 Abu, Fadhilatul Hikmah TJ Mechanical engineering and machinery This report discusses the final analysis and finite element analysis (FEA) of chosen topic, which is Design and Analysis of Recovery Net Landing for UAV ALUDRA MR-01. The objective of this research is to design analysis recovery net landing system for ALUDRA MR-01 with maximum take–off weight 40kg which capability to landing with safely. The aim of this study is to analysis and simulates; recovery net landing system for ALUDRA MR-01, determine the critical location on net during aircraft landing impact, define the minimum diameter of net can sustain from impact energy UAV and to determine the recovery net landing can sustain the ALUDRA MR-01 MTOW 40kg with safely. This report is divided into a few main sections for clarify and easier reference. There are Introduction, Literature Review, Methodology, Conceptual Design, Detail Design and Conclusion and Recommendation. The introduction part will helps the reader to have a general view on what are Recovery System and the reasons recovery net landing had been selected by ALUDRA MR-01. The body of this report will further explain all the literature review and research that being done before regarding the same field of interest. These chapter discusses about two parameters; maximum take – off weight of the aircraft and recovery system that is used in UAV industry. The methodology part will explain on how the sequence will take place in order to complete this project within one year duration. Result and discussions shall discuss on the FEA modelling based on different of position the load are applied on recovery net. The results will give the different value of maximum stress by different nodes. In the end this project will be able to define the minimum diameter of net can sustain from impact energy UAV. The ALUDRA MR-01 with maximum take–off weight 40kg had capability to landing Fulmar recovery net landing system which design for MTOW 20kg with safely. Universiti Teknologi Petronas 2013-09 Final Year Project NonPeerReviewed application/pdf en http://utpedia.utp.edu.my/10826/1/FADHILATUL_15529_FINAL_DISSERTATION.pdf Abu, Fadhilatul Hikmah (2013) Design and Analysis of Recovery Net Landing for UAV ALUDRA MR-01. Universiti Teknologi Petronas. (Unpublished)
institution Universiti Teknologi Petronas
building UTP Resource Centre
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Petronas
content_source UTP Electronic and Digitized Intellectual Asset
url_provider http://utpedia.utp.edu.my/
language English
topic TJ Mechanical engineering and machinery
spellingShingle TJ Mechanical engineering and machinery
Abu, Fadhilatul Hikmah
Design and Analysis of Recovery Net Landing for UAV ALUDRA MR-01
description This report discusses the final analysis and finite element analysis (FEA) of chosen topic, which is Design and Analysis of Recovery Net Landing for UAV ALUDRA MR-01. The objective of this research is to design analysis recovery net landing system for ALUDRA MR-01 with maximum take–off weight 40kg which capability to landing with safely. The aim of this study is to analysis and simulates; recovery net landing system for ALUDRA MR-01, determine the critical location on net during aircraft landing impact, define the minimum diameter of net can sustain from impact energy UAV and to determine the recovery net landing can sustain the ALUDRA MR-01 MTOW 40kg with safely. This report is divided into a few main sections for clarify and easier reference. There are Introduction, Literature Review, Methodology, Conceptual Design, Detail Design and Conclusion and Recommendation. The introduction part will helps the reader to have a general view on what are Recovery System and the reasons recovery net landing had been selected by ALUDRA MR-01. The body of this report will further explain all the literature review and research that being done before regarding the same field of interest. These chapter discusses about two parameters; maximum take – off weight of the aircraft and recovery system that is used in UAV industry. The methodology part will explain on how the sequence will take place in order to complete this project within one year duration. Result and discussions shall discuss on the FEA modelling based on different of position the load are applied on recovery net. The results will give the different value of maximum stress by different nodes. In the end this project will be able to define the minimum diameter of net can sustain from impact energy UAV. The ALUDRA MR-01 with maximum take–off weight 40kg had capability to landing Fulmar recovery net landing system which design for MTOW 20kg with safely.
format Final Year Project
author Abu, Fadhilatul Hikmah
author_facet Abu, Fadhilatul Hikmah
author_sort Abu, Fadhilatul Hikmah
title Design and Analysis of Recovery Net Landing for UAV ALUDRA MR-01
title_short Design and Analysis of Recovery Net Landing for UAV ALUDRA MR-01
title_full Design and Analysis of Recovery Net Landing for UAV ALUDRA MR-01
title_fullStr Design and Analysis of Recovery Net Landing for UAV ALUDRA MR-01
title_full_unstemmed Design and Analysis of Recovery Net Landing for UAV ALUDRA MR-01
title_sort design and analysis of recovery net landing for uav aludra mr-01
publisher Universiti Teknologi Petronas
publishDate 2013
url http://utpedia.utp.edu.my/10826/1/FADHILATUL_15529_FINAL_DISSERTATION.pdf
http://utpedia.utp.edu.my/10826/
_version_ 1739831851278663680
score 13.211869

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