The Parrot UAV Controlled by PID Controllers
Journal Title: Acta Mechanica et Automatica - Year 2014, Vol 8, Issue 2
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.
Authors and Affiliations
Andrzej Koszewnik
Keywords
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- EP ID EP147458
- DOI 10.2478/ama-2014-0011
- Views 36
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