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Sliding Mode Control of Quadrotor based on Differential Flatness

机译:基于差动平面度的四旋翼滑模控制

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In this work, the differential flatness property and the sliding mode controller design are proposed for a quadrotor in order to track a predefined reference trajectory despite the presence of uncertain parameters. Firstly, differential flatness is utilized to resolve the problem for trajectory generation and tracking for the quadrotor. Next, a sliding controller is combined with a flatness design to guarantee the robustness of the tracking strategy. The numerical simulations of quadrotor system are done in order to evaluate the performance of the suggested control scheme.
机译:在这项工作中,尽管存在不确定的参数,但为四旋翼飞机提出了差分平坦度特性和滑模控制器设计,以便跟踪预定义的参考轨迹。首先,利用差分平面度来解决四旋翼的轨迹生成和跟踪问题。接下来,将滑动控制器与平面度设计相结合,以确保跟踪策略的鲁棒性。为了评估建议的控制方案的性能,对四旋翼系统进行了数值模拟。

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