Proportional Integral Derivative Based Control For Autonoumous Vertical Take Off And Landing Of Quadcopter System

Since 2009, research on unmanned aerial vehicle (UAV) especially quadcopter system has attracted a considerable attention from researchers in the field. The quadcopter system is actually a class of flying robot that has ability to take off and landing in a vertical condition. Moreover, it has the ad...

Full description

Saved in:
Bibliographic Details
Main Author: Mustapa, Muhammad Zaki
Format: Thesis
Language:English
English
Published: UTeM 2016
Subjects:
Online Access:http://eprints.utem.edu.my/id/eprint/18518/1/Proportional%20Integral%20Derivative%20Based%20Control%20For%20Autonoumous%20Vertical%20Take%20Off%20And%20Landing%20Of%20Quadcopter%20System%2024%20Pages.pdf
http://eprints.utem.edu.my/id/eprint/18518/2/Proportional%20Integral%20Derivative%20Based%20Control%20For%20Autonoumous%20Vertical%20Take%20Off%20And%20Landing%20Of%20Quadcopter%20System.pdf
http://eprints.utem.edu.my/id/eprint/18518/
https://plh.utem.edu.my/cgi-bin/koha/opac-detail.pl?biblionumber=100936
Tags: Add Tag
No Tags, Be the first to tag this record!
Be the first to leave a comment!
You must be logged in first