Vývoj a realizace letounu VUT 001 Marabu pro ověření systémů UAV

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F08%3APU80001" target="_blank" >RIV/00216305:26210/08:PU80001 - 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

Development and Realization of VUT 001 MARABU Aircraft for Experimental Verification of UAV Systems

Popis výsledku v původním jazyce

Recent trend in the development of UAVs (Unmanned Aerial Vehicles) for civil sector is confronted with non-existence of regulatory requirements for their design and operations. Development of an UAV is practically always connected also with development of ground control station. Simultaneous development of both major elements (aerial vehicle and ground control station) makes first flight tests risky with high probability of aerial vehicle destruction. Such development approach is possible only for verysmall UAVs (micro UAVs) or for military aircraft (where producers have special ranges available for tests). European airspace is limited for such tests. Furthermore, such development can be very expensive. On the other hand, adaptation of existing designs into OPV (Optionally Piloted Vehicles) cannot utilize full potential of the airframe for UAV missions. Information gained during participation of Institute of Aerospace Engineering (IAE) in European projects created base for realization

Název v anglickém jazyce

Development and Realization of VUT 001 MARABU Aircraft for Experimental Verification of UAV Systems

Popis výsledku anglicky

Recent trend in the development of UAVs (Unmanned Aerial Vehicles) for civil sector is confronted with non-existence of regulatory requirements for their design and operations. Development of an UAV is practically always connected also with development of ground control station. Simultaneous development of both major elements (aerial vehicle and ground control station) makes first flight tests risky with high probability of aerial vehicle destruction. Such development approach is possible only for verysmall UAVs (micro UAVs) or for military aircraft (where producers have special ranges available for tests). European airspace is limited for such tests. Furthermore, such development can be very expensive. On the other hand, adaptation of existing designs into OPV (Optionally Piloted Vehicles) cannot utilize full potential of the airframe for UAV missions. Information gained during participation of Institute of Aerospace Engineering (IAE) in European projects created base for realization

Druh

A - Audiovizuální tvorba

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

<a href="/cs/project/FI-IM3%2F041" target="_blank" >FI-IM3/041: *Návrh a realizace letounu VUT 001 Marabu pro podporu využití bezpilotních létajících prostředků v civilním sektoru (Fakulta strojního inženýrství).</a><br>

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2008

Kód důvěrnosti údajů

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

ISBN

978-80-902522-2-6

Místo vydání

Ústav letadlové techniky, ČVUT v Praze, FS Ka

Název nakladatele resp. objednatele

Česká odborná společnost letecká

Verze

Neuveden

Identifikační číslo nosiče

neuvedeno