The Parrot UAV Controlled by PID Controllers

Andrzej Koszewnik

doi:10.2478/ama-2014-0011

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The Parrot UAV Controlled by PID Controllers

Acta Mechanica et Automatica

Volume 8 (2014): Issue 2 (June 2014)

By: Andrzej Koszewnik

Open Access

|Aug 2014

Abstract

The paper presents the process of modeling and designing control laws for four-rotor type of the Parrot UAV. The state space model is obtained by using several phenomena like gyroscopic effects for rigid bodies, propellers and rotors. The obtained model has been used to design PID control laws for roll, pitch, yaw angle and altitude, respectively. The numerical simulations of the closed loop model are shown that system in satisfy way stabilize flight of the quadro-rotor in all considered directions.

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Articles in this issue

DOI: https://doi.org/10.2478/ama-2014-0011 | Journal eISSN: 2300-5319 | Journal ISSN: 1898-4088

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Language: English

Page range: 65 - 69

Published on: Aug 15, 2014

Published by: Bialystok University of Technology

In partnership with: Paradigm Publishing Services

Publication frequency: 4 issues per year

Keywords:

Parrot,

Related subjects:

Electrical engineering,

Electronics,

Mechanical engineering,

Mechanics,

Bioengineering and biomedical engineering,

Biomechanics,

Civil engineering,

Environmental engineering

© 2014 Andrzej Koszewnik, published by Bialystok University of Technology
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

Volume 8 (2014): Issue 2 (June 2014)