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- W2010981847 abstract "The design, fabrication, and testing of a hybrid micro air vehicle capable of morphing between a high-hover-endurance rotary-wing mode and a high-cruise-speed fixed-wing mode is described. The micro air vehicle can efficiently perform a mission comprising outdoor flight to a target, followed by indoor surveillance and a return to the launch point. In addition, the micro air vehicle can function as a multirole platform, capable of flying exclusively as a fixed-wing or a rotary-wing vehicle. The key design drivers were 1) minimizing power required to hover, 2) ensuring static longitudinal stability in fixed-wing mode, and 3) minimizing the change in geometry between flight modes. Configuration trade studies were performed using blade element momentum theory for the rotary-wing mode and modified lifting-line theory for the fixed-wing mode. Design drivers for the rotary-wing mode and fixed-wing mode were often conflicting, and the selection of the final vehicle planform was primarily based on longitudinal static stability in fixed-wing mode. Two proof-of-concept prototypes with identical geometries, one for each flight mode, were constructed using off-the-shelf components and tested. Analytical predictions were validated by experimental measurements on the prototype vehicles. The final vehicle design is a flying wing with aft-swept, negatively twisted wings, having a wingspan of 394 mm and a mass of 85 g. The cruise velocity is , and the power required to hover is 11.6 W." @default.
- W2010981847 created "2016-06-24" @default.
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- W2010981847 date "2013-11-01" @default.
- W2010981847 modified "2023-10-16" @default.
- W2010981847 title "High-Speed Hover-Capable Morphing Micro Air Vehicle" @default.
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- W2010981847 doi "https://doi.org/10.2514/1.c032144" @default.
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