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
Related Articles
- EP ID EP147458
- DOI 10.2478/ama-2014-0011
- Views 54
- Downloads 0
Effect of the Atmosphere on the Performances of Aviation Turbine Engines
The paper presents how the parameters defining the state of the atmosphere: pressure, temperature, humidity, are affecting performance of the aircraft turbine engines and their durability. Also negative impact of dust...
Measurement Uncertainty Analysis of the Strain Gauge Based Stabilographic Platform
The present article describes constructing a stabilographic platform which records a standing patient’s deflection from their point of balance. The constructed device is composed of a toughen glass slab propped with 4 fo...
The Parrot UAV Controlled by PID Controllers
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, propelle...