螺旋桨故障情况下四旋翼飞机的紧急降落:基于PID的方法

V. Lippiello, Fabio Ruggiero, Diana Serra
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引用次数: 45

摘要

提出了一种处理四旋翼电机故障的控制器。假设系统已经检测到故障,将四旋翼飞行器建模为带固定螺旋桨的双旋翼飞行器,并控制其按照计划的紧急着陆轨迹飞行。理论表明,在这种构型下,飞行器可以到达笛卡尔空间中的任何位置,从而降低了控制偏航角的可能性。通过仿真验证了所提出的方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Emergency landing for a quadrotor in case of a propeller failure: A PID based approach
A controller dealing with the failure of a quadrotor's motor is presented in this paper. Supposing that the failure has been already detected by the system, the quadrotor is modelled as a birotor with fixed propellers and it is controlled to follow a planned emergency landing trajectory. Theory shows that, in such a configuration, the aerial vehicle is allowed to reach any position in the Cartesian space dropping the possibility to control the yaw angle. Simulations are presented to confirm the presented methodology.
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