A STUDY ON THE VIBRATION AND FORCE CHARACTERISTICS OF UNMANNED AERIAL VEHICLES

Abstract

The main purpose of this research is to analyze the vibrations and forces on the drone. The project involves building a quadcopter drone and conducting test to measure the vibration and force it causes in various types of flight. Sensor like accelerometer is used to measure the frequencies of vibration. This study begins with a comprehensive review of the available literature on Drone vibrations and forces and their effects on drone performance. This literature review provides a theoretical framework and serves as a framework for experimental research. The design and construction of drones involves the selection of appropriate materials, consideration of aerodynamic properties, and the use of common damping techniques to minimize external interference. The Design and force analysis of a drone is conducted using Fusion 360. The objective of this mini project is to analyze forces experienced by a drone's components and frame during flight. Fusion 360 offers a comprehensive set of tools and functionalities for designing and simulating mechanical systems, making it an ideal platform for this analysis. The project involves creating a 3D model of the drone, applying appropriate materials and physical properties, and simulating different flight scenarios to evaluate its performance under varying conditions. The vibration analysis of a drone to assess the impact of vibrations on its structural integrity and flight characteristics. The project aims to identify the vibration sources, measure the vibration levels, and propose suitable solutions to minimize their adverse effects.