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 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.