Abstract
The present proposal refers to a wing type micro unmanned aerial vehicle that provides low operation risk to people and instalations (Micro-Brosh). The UAV is intended for aerospace use, having dimensions less than 30 cm and a weight less than 200 g, what guarantees low danger to the handler and physical installations if compared to traditional aircrafts in operation. The proposal also has low production and maintenance costs, with takeoff by manual launch and landing without the need for appropriate runways, in addition to low RCS (Radar Cross Section) or radar signature, what makes it useful in military applications. We show the design details, depicting the used techniques for determining sustainability, minimum flight velocity, maximum time of flight (autonomy) and other solved issues related to the development. The experiments and results include tests done with the platform for proving its navegability. This work is a good starting point to researchers that intend to enter this area nowadays.
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