CONTROLLING AIRCRAFT USING THRUST DIFFERENTIAL TRIM

Systems and methods for stabilizing an aircraft in response to a yaw movement are provided. In one embodiment, a method includes detecting a yaw movement of the aircraft. The yaw movement can cause a front portion of the aircraft to move towards a first side of the aircraft. The method can further include, in response to the yaw movement, initiating a trim process resulting in a thrust differential. The trim process can include increasing thrust in one or more engines on the first side of the aircraft and decreasing thrust in one or more engines on a second side of the aircraft. The method can include controlling the trim process based at least in part on a detected yaw movement of the aircraft. 本发明提供响应于偏航运动稳定飞行器的系统和方法。在个实施例中，所述方法包括检测飞行器的偏航运动。偏航运动可能使得飞行器的前部部分朝向飞行器的第侧运动。所述方法还可以包括：响应于偏航运动，启动修整过程以产生推力差。修整过程可以包括：增大飞行器的第侧上的个或多个发动机中的推力，并减小飞行器的第二侧上的个或多个发动机中的推力。所述方法可以包括：至少部分地基于检测到飞行器的偏航运动控制修整过程。