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5th International Conference on Intelligent Systems Design and Applications (ISDA'05)
Fuzzy Flight Control System for Helicopter Intelligence in Hover
Wroclaw, Poland
September 08-September 10
ISBN: 0-7695-2286-6
ASCII Text
x 
 
Michal Lower, Boguslaw Szlachetko, Dariusz Krol, "Fuzzy Flight Control System for Helicopter Intelligence in Hover," Intelligent Systems Design and Applications, International Conference on, pp. 370-374, 5th International Conference on Intelligent Systems Design and Applications (ISDA'05), 2005.
 
 
BibTex
x
 
@article{ 10.1109/ISDA.2005.48,
author = {Michal Lower and Boguslaw Szlachetko and Dariusz Krol},
title = {Fuzzy Flight Control System for Helicopter Intelligence in Hover},
journal ={Intelligent Systems Design and Applications, International Conference on},
volume = {0},
year = {2005},
isbn = {0-7695-2286-6},
pages = {370-374},
doi = {http://doi.ieeecomputersociety.org/10.1109/ISDA.2005.48},
publisher = {IEEE Computer Society},
address = {Los Alamitos, CA, USA},
}
 
 
RefWorks Procite/RefMan/Endnote
x 
 
TY - CONF
JO - Intelligent Systems Design and Applications, International Conference on
TI - Fuzzy Flight Control System for Helicopter Intelligence in Hover
SN - 0-7695-2286-6
SP370
EP374
A1 - Michal Lower,
A1 - Boguslaw Szlachetko,
A1 - Dariusz Krol,
PY - 2005
KW - null
VL - 0
JA - Intelligent Systems Design and Applications, International Conference on
ER -
 
Michal Lower, Wroclaw University of Technology, Poland
Boguslaw Szlachetko, Wroclaw University of Technology, Poland
Dariusz Krol, Wroclaw University of Technology, Poland
This paper relates to a fuzzy flight control system in spot hovering for a single-rotor helicopter PZL Kania1. The model of the fuzzy control system was developed on the basis of computer simulation experiments done by the expert?s analysis (pilot?s knowledge). The helicopter?s mathematical model and its fuzzy flight control system were simulated using Matlab software package. In a series of numerous computer simulations the operation of the fuzzy control system was investigated and the system itself was tuned up. Simulation tests have been performed for the helicopter both in fixed hovering, and in hovering with disturbances. Disturbances were related to a gust of wind or to an accidental motion of one of the rudders. Obtained results give the good promise for building the Web simulator.
Citation:
Michal Lower, Boguslaw Szlachetko, Dariusz Krol, "Fuzzy Flight Control System for Helicopter Intelligence in Hover," isda, pp.370-374, 5th International Conference on Intelligent Systems Design and Applications (ISDA'05), 2005
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