多重事件触发机制下四旋翼飞行器的姿态跟踪控制

Abstract

In order to reduce the loss of internal resources of the quadrotor during its flight, based on the dynamic model of the quadrotor, the controller is designed by the backstepping method and it realizes the attitude tracking control of the aircraft. On this basis, an eventtriggered controller is constructed by introducing an event-triggered mechanism, thereby reducing the resource loss of the quadrotor and increasing its flight time.