publication . Article . 2014

The Parrot UAV Controlled by PID Controllers

Andrzej Koszewnik;
Open Access
  • Published: 01 Aug 2014 Journal: Acta Mechanica et Automatica, volume 8, pages 65-69 (eissn: 2300-5319, Copyright policy)
  • Publisher: Walter de Gruyter GmbH
Abstract
<jats:title>Abstract</jats:title> <jats:p>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.</jats:p>
Subjects
free text keywords: PID controller, Control theory, Propeller, Euler angles, symbols.namesake, symbols, Engineering, business.industry, business, Control engineering, History of engineering, Gyroscope, law.invention, law, State-space representation, PID Control, Parrot, Quadro-Rotor, Modeling, Mechanics of engineering. Applied mechanics, TA349-359
Related Organizations
Powered by OpenAIRE Research Graph
Any information missing or wrong?Report an Issue