Maneuverability improved airborne vehicle and a method implemented for this purpose

摘要

Providing improved yaw maneuverability to an aerial vehicle of the multi-blade type, that enables modifying the pitch angle (α) of its rotors blades, and a method of implementation for this purpose, wherein the axis of movement of at least two pairs of the aerial vehicle's rotors are tilted in a symmetrical configuration in relation to the aerial vehicle's yaw plane, so that each pair converges towards another point on the same level along a longitudinal axis plane of the aerial vehicle while creating an angle (ϒ) between the rotation planes of the rotors of each pair, which is less than 180° and greater than 140°.