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Nonlinear ellipsoid based attitude control for aggressive trajectories in a quadrotor: Closed-loop multi-flips implementation

机译:基于非线性椭球的姿态控制的四旋翼飞行器轨迹:闭环多翻转实现

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In this paper a model-free continuous nonlinear control law for the attitude of a quadrotor, based on the Attractive Ellipsoid Method and a saturation term, is proposed. This control law allows the vehicle to track aggressive maneuvers, such as multiple flips about the y axis of the body frame, with high angular velocities. The controller is designed through a singularity-free attitude representation based on a unit quaternion and its gains are computed by solving an optimization problem with LMIs. The proposed controller preserves the advantageous characteristics of the Attractive Ellipsoid Method and increases its robustness properties with the fast response of the nonlinear saturation term, minimizing as much as possible the attitude tracking error and assuring its convergence to a small neighborhood around the origin. A numerical study based on simulations is presented to analyze the advantages of the proposed approach, and experiments are presented to show the performance of the closed-loop system for tracking aggressive multiple flips, even in outdoors.
机译:提出了一种基于吸引力椭圆法和饱和项的四转子姿态无模型连续非线性控制律。该控制定律使车辆能够以较高的角速度跟踪激进的机动动作,例如围绕车身框架y轴的多次翻转。通过基于单元四元数的无奇异姿态表示来设计控制器,并通过解决LMI的优化问题来计算其增益。所提出的控制器保留了有吸引力的椭球方法的优点,并通过非线性饱和项的快速响应提高了其鲁棒性,从而最大程度地减小了姿态跟踪误差,并确保其收敛于原点附近的小邻域。进行了基于仿真的数值研究,以分析该方法的优点,并进行了实验,以展示闭环系统即使在户外也能跟踪剧烈的多次翻转。

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