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.
Original language | English |
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Pages | 1-9 |
Number of pages | 9 |
Publication status | Published - 2005 |
Event | 31st European Rotorcraft Forum - Florence, Italy Duration: 13 Sept 2005 → 15 Sept 2005 |
Conference
Conference | 31st European Rotorcraft Forum |
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Country/Territory | Italy |
City | Florence |
Period | 13/09/05 → 15/09/05 |