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首页> 外文期刊>IEEE Transactions on Aerospace and Electronic Systems >Almost-Global Finite-Time Trajectory Tracking Control for Quadrotors in the Exponential Coordinates
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Almost-Global Finite-Time Trajectory Tracking Control for Quadrotors in the Exponential Coordinates

机译:指数坐标系中四旋翼的几乎全局有限时间轨迹跟踪控制

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摘要

This paper investigates the trajectory tracking problem for quadrotors with finite-time convergence via homogeneous feedback approach. Based on the inherent underactuated cascaded properties of a quadrotor, the tracking control is decomposed into the outer position tracking control loop and the inner attitude tracking control loop. And the orientation of the four thrust inputs for the position loop is determined by the attitude loop. Therefore, an inner geometric tracking controller based on exponential coordinates for the attitude loop is first proposed, which avoids kinematic singularity and redundancy. Then, a homogeneous feedback plus dynamics compensation scheme is utilized to construct the thrust magnitude control input for the position dynamics, which also provides a reference rotation matrix for the attitude tracking loop. The almost global finite time stability of the whole tracking control system is clearly proved. Numerical results are also presented to demonstrate the effectiveness of this finite-time control strategy.
机译:本文通过齐次反馈方法研究了具有有限时间收敛性的四旋翼飞行器的轨迹跟踪问题。基于四旋翼固有的欠驱动级联特性,将跟踪控制分解为外部位置跟踪控制环和内部姿态跟踪控制环。位置环的四个推力输入的方向由姿态环确定。因此,首先提出了一种基于指数坐标的姿态环内部几何跟踪控制器,该控制器避免了运动学上的奇异和冗余。然后,采用均匀反馈加动力学补偿方案来构造用于位置动力学的推力幅值控制输入,该输入还为姿态跟踪回路提供参考旋转矩阵。整个跟踪控制系统的几乎全局的有限时间稳定性已得到明确证明。数值结果也被证明以证明这种有限时间控制策略的有效性。

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