Modeling and PID Control of a Quadrotor Aerial Robot

This paper elucidates the modeling of a + quadrotor configuration aerial vehicle and the design of its attitude and altitude controllers. The aircraft model consists of four fixed pitch angle propeller, each driven by an electric DC motor. The hovering flight of the quadrotor is governed by the Newt...

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Bibliographic Details
Main Authors: Ismail, Mohd Khairuddin, Anwar, P. P. A. Majeed, Abdul Aziz, Jaafar, Jessnor Arif, Mat Jizat
Format: Article
Language:English
Published: Trans Tech Publications, Switzerland 2014
Subjects:
Online Access:http://umpir.ump.edu.my/id/eprint/5545/1/scan0011.pdf
http://umpir.ump.edu.my/id/eprint/5545/
http://www.scientific.net/AMR.903.327
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