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Eisa Musa, Ahmed Yosreldin (2016) AEROSTAT EFFECT ON UAV STABILITY. IRC, Universiti Teknologi PETRONAS. (Submitted)

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The current generation of UAVs lack extended hovering and flight capabilities. Equipping a quadrotor with an inflatable structure enhances energy efficiency. In this work, the aerostat size effect on a UAV quadrotor system is investigated, and the stability of the Lighter-than-Air system is contrasted by creating a flight dynamics model. A mathematical model of the AR DRONE 2.0 with an aerostat is formulated and simulated with Matlab in hovering mode. The mathematical model is validated by comparison to real-life flight data. A validated dynamic model describing the behavior of the drone in hovering mode was developed and used for simulation.

Item Type: Final Year Project
Academic Subject : Academic Department - Mechanical Engineering - Petroleum
Subject: T Technology > TJ Mechanical engineering and machinery
Divisions: Engineering > Mechanical
Depositing User: Ahmad Suhairi Mohamed Lazim
Date Deposited: 19 Oct 2016 09:17
Last Modified: 25 Jan 2017 09:34
URI: http://utpedia.utp.edu.my/id/eprint/16930

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