Filter optimization and sensitivity analysis of pilot behavior tested on flight simulator
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F14%3A00532397" target="_blank" >RIV/60162694:G43__/14:00532397 - isvavai.cz</a>
Výsledek na webu
<a href="http://vavtest.unob.cz/registr" target="_blank" >http://vavtest.unob.cz/registr</a>
DOI - Digital Object Identifier
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Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Filter optimization and sensitivity analysis of pilot behavior tested on flight simulator
Popis výsledku v původním jazyce
This paper describes another option for the evaluation and analysis of data measured on flight simulator using alternative human behavior models - human as a pilot while flying an aircraft. The measured data was then mathematically analyzed in the MATLAB® environment, providing the input and output data for the filter optimization. Paper also describes the original method of mathematical human behavior model sensitivity analysis, or more precisely, pilot's response to a sudden change of flight altitude. The model is in the form of a rational fraction function of 2nd order and is used for all practical experiments. Individual coefficients of the transfer function represent the pilot's ability to fly the aircraft, i.e. all the coefficients have a specific and practical meaning. The main aim of this paper is optimal filter design with obtaining the best transfer function parameters and analyzing relative sensitivities of all the transfer function coefficients of the pilot's behavior model. Another aim of this paper is to determine coefficient ranges of the pilot's behavior model for further practical use. Due to the measurements, filter optimization and sensitivity analysis the pilot behavior model can obtain more realistic shape useful in the aircraft's flight control systems at an early stage of its development.
Název v anglickém jazyce
Filter optimization and sensitivity analysis of pilot behavior tested on flight simulator
Popis výsledku anglicky
This paper describes another option for the evaluation and analysis of data measured on flight simulator using alternative human behavior models - human as a pilot while flying an aircraft. The measured data was then mathematically analyzed in the MATLAB® environment, providing the input and output data for the filter optimization. Paper also describes the original method of mathematical human behavior model sensitivity analysis, or more precisely, pilot's response to a sudden change of flight altitude. The model is in the form of a rational fraction function of 2nd order and is used for all practical experiments. Individual coefficients of the transfer function represent the pilot's ability to fly the aircraft, i.e. all the coefficients have a specific and practical meaning. The main aim of this paper is optimal filter design with obtaining the best transfer function parameters and analyzing relative sensitivities of all the transfer function coefficients of the pilot's behavior model. Another aim of this paper is to determine coefficient ranges of the pilot's behavior model for further practical use. Due to the measurements, filter optimization and sensitivity analysis the pilot behavior model can obtain more realistic shape useful in the aircraft's flight control systems at an early stage of its development.
Klasifikace
Druh
J<sub>x</sub> - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
CEP obor
KA - Vojenství
OECD FORD obor
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Návaznosti výsledku
Projekt
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Návaznosti
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Ostatní
Rok uplatnění
2014
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název periodika
International Journal of Mathematics and Computers in Simulation
ISSN
1998-0159
e-ISSN
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Svazek periodika
8
Číslo periodika v rámci svazku
1/2014
Stát vydavatele periodika
US - Spojené státy americké
Počet stran výsledku
8
Strana od-do
31-38
Kód UT WoS článku
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EID výsledku v databázi Scopus
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