摘要
四旋翼无人机具有欠驱动、非线性、强耦合的特点。针对四旋翼无人机轨迹跟踪控制中跟踪精度低,抗外界干扰能力弱的特点,通过对四旋翼无人机进行四元数建模,使用误差四元数作为控制器输入,消除了无人机在机动角度过大时的奇点问题,提出了一种分数阶S面的控制方法,即将分数阶PID控制与S面控制融合,作为一个新的控制器。轨迹跟踪试验表明,分数阶S面控制器在四旋翼无人机控制模型中的累计误差明显小于分数阶PID,证明了该方法具有抗风扰能力强、跟踪精度高的特点。
Quadrotor possess traits such as under-actuation,nonlinearity,and strong coupling.Quaternions are primarily used for attitude calculation in drones,with error quaternions seldom employed directly in the control of specific quadcopter drones.This paper focuses on the low tracking accuracy and weak anti-interference ability of quadcopter drones in trajectory tracking control.By establishing the quadcopter quaternion model,a controller based on quaternion error is designed through a combination of fractional-order PID control with S-plane control.Trajectory tracking experiments demonstrate that:the fractional-order S-surface controller has significantly smaller cumulative errors than the fractional-order PID in the control model of quadcopter drones,proving that this method has strong anti-wind disturbance ability and high tracking accuracy.
作者
李佳成
陈鹏云
常哲
LI Jiacheng;CHEN Pengyun;CHANG Zhe(School of Aerospace Engineering,North University of China,Taiyuan 030000,China)
出处
《兵器装备工程学报》
CAS
CSCD
北大核心
2024年第3期286-292,共7页
Journal of Ordnance Equipment Engineering
基金
国家自然科学基金项目(51909245,62003314)
山西省重点研发计划(202202020101001)
中北大学研究生科技立项资助项目(20221876)。