This study attempts to present a new and comprehensive cycle for the design of fixed wing
micro air vehicles. The idea is to propose a complete cycle containing all micro air vehicles …

An optimized and comprehensive method is used to design and manufacture a fixed wing
micro air vehicle (MAV) with Zimmerman planform. The design process includes four stages …

In this paper, the design process of a fixed-wing Micro Air Vehicle (MAV) is presented. The
design cycle begins with mission requirements, followed by collecting statistical data from …

ABSTRACT Micro Air Vehicles have been the subject of continued interest and development
over the last several years. The majority of current vehicle concepts rely on rigid fixed wings …

It is useful to combine hover and forward flight capability of air vehicles into a hybrid design.
This paper discusses the development of one such hybrid air vehicle: Quadrotor biplane …

Airfoil selection procedure, wind tunnel testing and an implementation of 6-DOF model on
flying wing micro aerial vehicle (FWMAV) has been proposed in this research. The selection …

Micro air vehicles (MAV) are essentially characterized by very stringent dimensional
constraints (typically 6–8 in or 15–20 cm) which the need suggests to maximize the wing …

An optimized and comprehensive method is proposed in order to design an efficient micro
unmanned air vehicle with morphing and growing capabilities. In the sizing process, to …

DURING the past several years there has been a growing interest in the design and
development of very small aircraft that are generally referred to as micro air vehicles (MAVs) …

Abstract Development of Mini/Micro UAV is a reason for renewed interest in aerodynamics of
low Reynolds numbers. Configurations with enhanced lift-carrying capabilities are …