Usability Testing of Interface for Emergency Landing Navigation Assistant

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F12%3A00193120" target="_blank" >RIV/68407700:21230/12:00193120 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Usability Testing of Interface for Emergency Landing Navigation Assistant
Original language description
Emergency landing decision support system (or also navigation assistant) for ultra-light aircraft is a feature for electronic flight instrument systems (EFIS) which are widely used on board of small sport aircrafts. Navigation assistant is intended to navigate pilots in case of a critical situation, mainly engine failure, to the closest possible landing site. To navigate pilot properly it is important to use appropriate interface, which is the topic of this paper. This paper proposes four different navigation paradigms, and presents results from dry-runs. Furthermore it includes methods used for evaluation. As a result a hypothesis regarding which of four interfaces is the best candidate for navigating the pilots is created and future research proposed.
Czech name
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Czech description
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Publication year
2012
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
POSTER 2012 - 16th International Student Conference on Electrical Engineering
ISBN
978-80-01-05043-9
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
1-4
Publisher name
Czech Technical University in Prague
Place of publication
Praha
Event location
Prague
Event date
May 17, 2012
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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