The take-off control of UAV with fly wing layout is limited by its relatively lower pitch moment. This paper gained the state parameters of a few groups of taking off model by means of numerical simulation. The influence of different models on take-off distance, take-off angle of attack (AOA), take-off safe speed and c.g. location was then analyzed. Based on the analysis, a new fly wing constitution was designed and the corresponding take-off control scheme was suggested as well. Finally, the flight test results shows that this fly wing constitution can gain better take-off control characteristics.
Research on Improving Take-Off Characteristics of Fly Wing with a New Constitution
Advanced Materials Research ; 462 ; 265-270
2012-02-10
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Research on Improving Take-Off Characteristics of Fly Wing with a New Constitution
Tema Archiv | 2012
|NTRS | 2002
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