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A geometric approach for quadrotor trajectory tracking control

机译:四旋翼轨迹跟踪控制的几何方法

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This paper investigates the trajectory tracking problem for quadrotor with attitude finite-time convergence via geometric approach. First, a global geometric dynamic description is presented on the special Euclidean group (SE(3)), and the trajectory tracking control is decomposed into two cascaded tracking control loops: the position tracking control loop and the attitude tracking control loop. Then, based on the fact that the attitude tracking loop is a fast loop, a finite-time controller based on the exponential coordinate is proposed to speed up the response rate of the attitude control loop, so that the artificial singularity and redundancy can be avoided. In addition, a backstepping controller is designed for the position tracking loop to construct the thrust magnitude control input for the position dynamics and the reference rotation matrix for the attitude tracking loop. Finally, the numerical simulation results are presented to demonstrate the effectiveness of this trajectory tracking strategy.
机译:本文通过几何方法研究了姿态有限时间收敛的四旋翼的轨迹跟踪问题。首先,在特殊的欧几里得群(SE(3))上给出了全局几何动力学描述,并且将轨迹跟踪控制分解为两个级联的跟踪控制环:位置跟踪控制环和姿态跟踪控制环。然后,基于姿态跟踪回路是一个快速回路这一事实,提出了一种基于指数坐标的有限时间控制器,以加快姿态控制回路的响应速度,从而避免了人工的奇异性和冗余性。 。另外,为位置跟踪环设计了一个反推控制器,以构造用于位置动力学的推力幅度控制输入和用于姿态跟踪环的参考旋转矩阵。最后,数值仿真结果表明了该轨迹跟踪策略的有效性。

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