Method for piloting a rotary-wing drone with multiple rotors with curved steering.

摘要

The method involves generating setpoint values for a drone control loop. The setpoint values are used to control horizontal linear speed and inclination of a drone (10) relative to a reference frame associated with a ground to make the drone to follow a curvilinear path (C) at predetermined tangential speed, where the drone is a quadricopter type drone having multiple rotors. The controlling step is realized based on a command comprising right or left turn direction parameter and a setpoint defining parameter for instantaneous radius of curvature. An independent claim is also included for a software comprising a set of instructions for implementing a method for piloting a rotary wing drone.