Evaluation of a Flight-guidance System for Ultra-Light Aircraft

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F12%3A00196530" target="_blank" >RIV/68407700:21230/12:00196530 - isvavai.cz</a>

Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Evaluation of a Flight-guidance System for Ultra-Light Aircraft

Popis výsledku v původním jazyce

This early stage research paper describes the methodology for evaluation of a flight guidance system of an emergency landing decision support system for ultra-light aircraft. This system is intended to be used in small sport aircraft in order to help pilots cope with critical situations such as engine failure. Paper is focused on evaluation of first dry-run round, where four different metaphors were tested. As a result a hypothesis is formed and a direction of future research is proposed.

Název v anglickém jazyce

Evaluation of a Flight-guidance System for Ultra-Light Aircraft

Popis výsledku anglicky

This early stage research paper describes the methodology for evaluation of a flight guidance system of an emergency landing decision support system for ultra-light aircraft. This system is intended to be used in small sport aircraft in order to help pilots cope with critical situations such as engine failure. Paper is focused on evaluation of first dry-run round, where four different metaphors were tested. As a result a hypothesis is formed and a direction of future research is proposed.

Druh

O - Ostatní výsledky

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

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Návaznosti

S - Specificky vyzkum na vysokych skolach

Rok uplatnění

2012

Kód důvěrnosti údajů

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