Parameter Estimation of Transfer Function of Pilot Behavior Model from Measured Data

Kód výsledku v IS VaVaI

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Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Parameter Estimation of Transfer Function of Pilot Behavior Model from Measured Data

Popis výsledku v původním jazyce

This paper describes calculations and results of time constants of mathematical model of a pilot' s behavior. Pilot was tested to a sudden altitude change whilst he controlled an aircraft. For calculations were used two different methods of measured dataprocessing. Firstly the method using System IdentificationToolbox(TM) from programming environment MATLAB(R) was applied. The second method used the identification algorithm to identify parameters of a transfer function of dynamic system which has beencreated by authors few years ago. The analytical model of human behavior from the basic element of an automated regulation was created. Experimental measurements were made on the Cessna 152 cockpit simulator at the University of Hertfordshire, Hatfield.The tested pilots were pilot students with several tens of flight hours in real planes. The pilot?s response to a sudden aircraft altitude change was measured.

Název v anglickém jazyce

Parameter Estimation of Transfer Function of Pilot Behavior Model from Measured Data

Popis výsledku anglicky

This paper describes calculations and results of time constants of mathematical model of a pilot' s behavior. Pilot was tested to a sudden altitude change whilst he controlled an aircraft. For calculations were used two different methods of measured dataprocessing. Firstly the method using System IdentificationToolbox(TM) from programming environment MATLAB(R) was applied. The second method used the identification algorithm to identify parameters of a transfer function of dynamic system which has beencreated by authors few years ago. The analytical model of human behavior from the basic element of an automated regulation was created. Experimental measurements were made on the Cessna 152 cockpit simulator at the University of Hertfordshire, Hatfield.The tested pilots were pilot students with several tens of flight hours in real planes. The pilot?s response to a sudden aircraft altitude change was measured.

Druh

D - Stať ve sborníku

CEP obor

KA - Vojenství

OECD FORD obor

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Projekt

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Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2012

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

Recent Researches in Automatic Control, Systems Science and Communications.

ISBN

978-1-61804-103-6

ISSN

1790-5117

e-ISSN

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Počet stran výsledku

5

Strana od-do

144-148

Název nakladatele

WSEAS Press

Místo vydání

Porto

Místo konání akce

Porto

Datum konání akce

1. 1. 2012

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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