Design And Develop A Vertical Take-Off And Landing Fixed-Wing Hybrid Unmanned Aerial Vehicle

Chan, Albert Bao Der (2019) Design And Develop A Vertical Take-Off And Landing Fixed-Wing Hybrid Unmanned Aerial Vehicle. Project Report. Universiti Teknikal Malaysia Melaka, Melaka, Malaysia. (Submitted)

Text (24 Pages) Design And Develop A Vertical Take-Off And Landing Fixed-Wing Hybrid Unmanned Aerial Vehicle.pdf - Submitted Version Download (1MB)

Abstract

Applications using Unmanned Aerial Vehicle (UAV) is growing since the past decade in both civilians and military industry. This robot has promising advantages in performing various tasks, especially without risking any single human life. Meanwhile, different requirement of various tasks leads to various types of UAV being designed to overcome with. This project focused on design and develop UAV with combination between the fixed-wing aircraft and the multirotor drone, named as fixed-wing hybrid type of UAV. Reviews on others work relevant to design and develop fixed-wing hybrid UAV has been done to come out with solid ideas to complete this project. There are plenty types of configurations available, thus they have been analyzed for selection of suitable ones to be involved according to design requirement established in early stage of this project. The results obtained in this project is a fixed-wing hybrid with a quadcopter UAV is designed and built to fly. All the calculations, fabrication steps, materials chosen and electronics components are included in this report. At the end of this project, flight evaluation is done on the flight test of UAV. There are a few suggested future work stated as well for further improvement for this project.

Actions (login required)

View Item