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 |
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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 |
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Land/Gebiet | Italien |
Ort | Florence |
Zeitraum | 13/09/05 → 15/09/05 |