Evaluation of a Flight-guidance System for Ultra-Light Aircraft
The result's identifiers
Result code in 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>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Evaluation of a Flight-guidance System for Ultra-Light Aircraft
Original language description
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.
Czech name
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Czech description
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Classification
Type
O - Miscellaneous
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
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Continuities
S - Specificky vyzkum na vysokych skolach
Others
Publication year
2012
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů