一种四旋翼无人机目标环绕抗干扰控制方法

By constructing the relative kinematic equations and extended state observers between a quadrotor UAV and a moving target, and combining robust integral control technology, an anti-interference controller for the attitude loop of a quadrotor UAV was designed. This solved the problems of insufficient UAV autonomy and environmental interference in traditional methods, and achieved stable tracking results.

CN114967724BActive Publication Date: 2026-07-17GUILIN UNIV OF AEROSPACE TECH

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
GUILIN UNIV OF AEROSPACE TECH
Filing Date
2022-07-04
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Traditional quadcopter UAV target tracking methods lack autonomous intelligence, are prone to crashes and deviations from the flight path due to operational errors, and do not consider the impact of environmental interference on target orbiting missions.

Method used

The relative kinematic equations between a quadrotor UAV and a moving target are constructed. By combining an extended state observer and robust integral control technology, an anti-interference controller for the attitude loop of the quadrotor UAV is designed to achieve stable tracking of the maneuvering target.

Benefits of technology

Despite inaccurate target acceleration information and environmental interference, the quadcopter UAV achieved continuous and stable tracking of maneuvering targets, demonstrating good anti-interference capabilities and rapid convergence.

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Abstract

本发明涉及一种四旋翼无人机目标环绕抗干扰控制方法,首先构建四旋翼无人机与移动目标之间对应坐标的相对运动学方程,即四旋翼无人机目标跟踪基本模型;接着构建四旋翼无人机速度分量与速度导航向量之间的误差动态方程;然后采用扩张状态干扰观测器对目标加速度信息和四旋翼无人机所遭受的集总扰动进行精准高效的实时估计,并以此构建四旋翼无人机轨迹回路目标环绕跟踪动态反馈控制器;最后构建基于鲁棒积分控制技术的四旋翼无人机姿态回路抗干扰控制器;整个设计方法是一种具有良好抗干扰性、可快速收敛的无人机环绕控制策略,能够在目标加速度信息无法精确获取和具有外部环境干扰的情况下对机动目标进行持续稳定跟踪。
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