DocumentCode
2836676
Title
Dynamic Modelling and Experimental Identification of Four Rotors Helicopter Parameters
Author
Derafa, L. ; Madani, T. ; Benallegue, A.
Author_Institution
Lab. de Controle et de Commande EMP, Algiers
fYear
2006
fDate
15-17 Dec. 2006
Firstpage
1834
Lastpage
1839
Abstract
In this paper an experimental identification of dynamic parameters of a four rotors mini helicopter is presented. An appropriate model for identification and control synthesis is obtained via modelization procedure where several phenomena are included like gyroscopic effects, aerodynamic friction. A comparison between simulated and real system is made in closed loop system using a same controller. The obtained results show the good estimation of the dynamic model.
Keywords
aerodynamics; aircraft control; automatic guided vehicles; closed loop systems; controllers; friction; helicopters; rotors; aerodynamic friction; autonomous unmanned air vehicles UAV; closed loop system; control synthesis; four rotor helicopters; gyroscopic effects; helicopter controller; Aerodynamics; Friction; Helicopters; Mathematical model; Propellers; Rotors; Turning; Uniform resource locators; Unmanned aerial vehicles; Vehicle dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Technology, 2006. ICIT 2006. IEEE International Conference on
Conference_Location
Mumbai
Print_ISBN
1-4244-0726-5
Electronic_ISBN
1-4244-0726-5
Type
conf
DOI
10.1109/ICIT.2006.372515
Filename
4237837
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