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Research on Trajectory Planning and Tracking of Hexa-copter

机译:直升机的轨迹规划与跟踪研究

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In this paper, the flight control problem of hexa-copter is studied in detail from threedimensional trajectory planning to tracking. Then the cubic spline interpolation method is used to generate the trajectory by using these time marked waypoints. The flight trajectory curve produced by this method is smooth, twice differentiable, and it is easy to control implementation. The flight dynamics model of the UAV has the characteristics of multi-input multi-output, strong coupling, under-actuation, severe nonlinearity and external environmental disturbance. In order to improve the accuracy of flight trajectory and the stability of attitude control, a multi-loop sliding mode variable structure control method is proposed to achieve the hexa-copter flight trajectory tracking. The simulation results show that this method can track the predetermined flight trajectory and keep the attitude stability of the UAV normally.
机译:从三维轨迹规划到跟踪,对六翼飞机的飞行控制问题进行了详细的研究。然后使用三次样条插值方法通过使用这些带有时间标记的航路点来生成轨迹。用这种方法产生的飞行轨迹曲线是平滑的,可以二次微分,并且易于控制实现。无人机的飞行动力学模型具有多输入多输出,强耦合,欠驱动,严重非线性和外部环境干扰的特点。为了提高飞行轨迹的精度和姿态控制的稳定性,提出了一种多环滑模变结构控制方法来实现六直升机飞行轨迹的跟踪。仿真结果表明,该方法能够跟踪预定的飞行轨迹,并能正常保持无人机的姿态稳定性。

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