DocumentCode :
2934088
Title :
Modelling and Control of a Complex Multi-physic System: Case of Helicopter Flight Axis Control
Author :
Martin, Miquel ; Gomand, Julien ; Malburet, F. ; Barre, P.
fYear :
2012
fDate :
14-16 Nov. 2012
Firstpage :
103
Lastpage :
108
Abstract :
A helicopter flight axis control, which is a complex multi-physic system, is modelled using an energetic based graphical tool. Element of the system are mainly composed of passive technologies and their number tends to increase years after years to improve the pilots comfort by adding new functions. Thanks to the recent march in electronic fields and in order to simplify flight structures, new active systems have come out in aeronautical systems, a specific sector which requires extreme rigors and approved technology. In this paper, a simplified helicopter flight axis control is modelled with the intention of controlling the helicopter stick force feedback. Using the Energetic Macroscopic Representation the detailed methodology presented in this paper is helpful to determine an adequate control for active systems with sampled signals.
Keywords :
aircraft control; control system analysis computing; force feedback; helicopters; signal sampling; active systems; adequate control; aeronautical systems; complex multiphysic system control; complex multiphysic system modelling; electronic fields; energetic based graphical tool; energetic macroscopic representation; flight structures; helicopter flight axis control; helicopter stick force feedback control; passive technologies; pilot comfort; sampled signals; Force; Force feedback; Helicopters; Mathematical model; Shock absorbers; Springs; Valves; Energetic Macroscopic Representation; Helicopter; Naslin polynomial; control; modelling; sampled signals;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Modeling and Simulation (EMS), 2012 Sixth UKSim/AMSS European Symposium on
Conference_Location :
Valetta
Print_ISBN :
978-1-4673-4977-2
Type :
conf
DOI :
10.1109/EMS.2012.77
Filename :
6410136
Link To Document :
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