Design, development and assessment of a DUCTED RUAV

Frank Buysschaert; Patrick Hendrick; Jean François Aernouts; Raphaël Evariste; Alexandre Abadie; Sébastien Roche; Pierre Slangen; Bruno Liévin

Design, development and assessment of a DUCTED RUAV

Frank Buysschaert, Patrick Hendrick, Jean François Aernouts, Raphaël Evariste, Alexandre Abadie, Sébastien Roche, Pierre Slangen, Bruno Liévin

Fluid Dynamics

Publikation: Unpublished contribution to conference › Papier › Begutachtung

Abstract

The paper describes the design, development and assessment of a rotary wing uav, which has as primary mission the observation and registration of targets at close range and which is commanded by a one-man-portable, three person operated ground control system. The chosen system configuration, the mission profiles and the in accordance developed design protocol are explained. Different construction methods are elucidated as well, allowing complex structures to be made without having important detrimental influences on weight.

Originalsprache	Englisch
Seiten	1-9
Seitenumfang	9
Publikationsstatus	Veröffentlicht - 2005
Veranstaltung	31st European Rotorcraft Forum - Florence, Italien Dauer: 13 Sept. 2005 → 15 Sept. 2005

Konferenz

Konferenz	31st European Rotorcraft Forum
Land/Gebiet	Italien
Ort	Florence
Zeitraum	13/09/05 → 15/09/05

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AU - Buysschaert, Frank

AU - Hendrick, Patrick

AU - Aernouts, Jean François

AU - Evariste, Raphaël

AU - Abadie, Alexandre

AU - Roche, Sébastien

AU - Slangen, Pierre

AU - Liévin, Bruno

PY - 2005

Y1 - 2005

N2 - The paper describes the design, development and assessment of a rotary wing uav, which has as primary mission the observation and registration of targets at close range and which is commanded by a one-man-portable, three person operated ground control system. The chosen system configuration, the mission profiles and the in accordance developed design protocol are explained. Different construction methods are elucidated as well, allowing complex structures to be made without having important detrimental influences on weight.

AB - The paper describes the design, development and assessment of a rotary wing uav, which has as primary mission the observation and registration of targets at close range and which is commanded by a one-man-portable, three person operated ground control system. The chosen system configuration, the mission profiles and the in accordance developed design protocol are explained. Different construction methods are elucidated as well, allowing complex structures to be made without having important detrimental influences on weight.

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M3 - Paper

AN - SCOPUS:33746644233

SP - 1

EP - 9

T2 - 31st European Rotorcraft Forum

Y2 - 13 September 2005 through 15 September 2005

ER -

Design, development and assessment of a DUCTED RUAV

Abstract

Konferenz

Andere Dateien und Links

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