Abstract

Development of Automatic Take Off and Smooth Landing Control System for Quadrotor UAV

Highlights

  • This paper covers the development of automatic takeoff and smooth landing control system for Unmanned Aerial Vehicle (UAV) Quadrotor

  • The development of automatic takeoff and smooth landing system is very crucial for safety system in Quadrotor

  • We need thrust force equal to quadrotor mass to lift up quadrotor

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Summary

Introduction

This paper covers the development of automatic takeoff and smooth landing control system for UAV Quadrotor. The Quadrotor is one of the Unmanned Aerial Vehicle (UAV) that use four propeller for flying They are four unit of brushless DC motor that mount at each of end quadrotor structure The advantages of this system are totally eliminate the use of the pilot to airborne the UAV and it is more secure and reliable for autonomous flight. Installment of automatic takeoff and smooth landing system can make new user to handle quadrotor and can avoid air crash (Tanveer, 2013). The development of automatic takeoff will help new user to solve this problem Another problem in this project is to make quadrotor maintain its stability in air. This input will be process by microcontroller and generate new output for quadrotor to change the speed of quadrotor to make it stable

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