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应对风切变的四旋翼轨迹跟踪几何控制方法

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针对存在风切变环境的四旋翼轨迹跟踪问题,提出了结合增量非线性动态逆的几何控制方法.首先,建立了基于SO(3)群的风切变扰动四旋翼动力学模型,并建立风场模型,引入风切变效应.其次,利用四旋翼的微分平坦特性将轨迹跟踪问题转换为状态跟踪问题,并依据微分平坦特性推导参考高阶状态量实现前馈控制.在控制器设计部分,姿态控制采用几何控制,使姿态具有全局不存在奇异点的特性.对于风场扰动带来的阻力与气动力矩,使用增量非线性动态逆方法进行补偿,实现线加速度和角加速度的控制.最后,基于Simulink在多种风速场景中对不同航迹进行了仿真实验,仿真结果验证了所提方法相较传统方法在面对风切变干扰情况下的有效性.
Geometric Control Method for Quadcopter Trajectory Tracking for Wind Shear
This paper proposes a geometric control method combining incremental nonlinear dynamic inversion,which can take into account the wind shear during the trajectory tracking problem of quadcopter.Firstly,we establish a quadcopter dynamics model based on SO(3)group in wind and wind models with wind shear.The trajectory tracking problem is transformed into a state tracking problem by the differential flatness of quadcopters,achieving feed forward control.In the controller design section,the control method of attitude is geometric control,and attitudes do not exhibit singularities.The drag force and aerodynamic torque caused by wind are compensated by incremental nonlinear dynamic inversion.This helps implement linear acceleration control and angular acceleration control.Finally,we simulate different trajectories in dif-ferent wind speed scenarios by Simulink.The simulation results verify that the proposed control method has better tracking performance compared to traditional methods under wind shear interference.

quadcoptergeometric controlincremental nonlinear dynamic inversiondifferential flatness

褚金奎、钱煜晖、张钟元、李金山

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大连理工大学机械工程学院,辽宁 大连 116024

大连理工大学宁波研究院,浙江 宁波 315032

四旋翼 几何控制 增量非线性动态逆 微分平坦

国家自然科学基金资助项目创新研究群体项目

5217526552275281

2024

机械与电子
中国机械工业联合会科技工作部 机械与电子杂志社

机械与电子

CSTPCD
影响因子:0.243
ISSN:1001-2257
年,卷(期):2024.42(9)
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