Aerodynamics of Drones with Auxetic Landing Gears During Perching Conditions

Abstract

This research investigates a quad copter that acts as a contactor of the perching process of birds with its auxetic graspers on the cylindrical surfaces. The perching system generates a time of yaw when a pitch / rolling control input during the drone landing is introduced by two different circumstances (high and forward flight). While in all situations the aggregate need for revolution every minute, pitch and energy consumption vs. flight vs, the auxetic environment enhances drone resistance in the treatment for spontaneous vibration talking. The suggested method stabilises frequency, yawing and rotating period with respect to the variable rate during perching.