一种纵列式无人机吊载系统载荷状态估计与控制方法

By using a force sensor-based tandem UAV sling system, combined with a Kalman filter and a nonlinear backstepping controller, the problems of load state monitoring accuracy and disturbance compensation in rotary-wing UAV sling systems were solved, achieving high-precision load state estimation and real-time control.

CN120469310BActive Publication Date: 2026-07-17SHANGHAI JIAOTONG UNIV +4

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
SHANGHAI JIAOTONG UNIV
Filing Date
2025-05-13
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing rotary-wing UAV sling systems suffer from problems in load status monitoring, such as sensor installation affecting motion, outdoor lighting affecting performance, and algorithm failure, making it difficult to achieve high-precision load status estimation and effective disturbance compensation.

Method used

A tandem UAV sling load system based on force sensors is adopted. By establishing a dynamic model, combining a Kalman filter and a nonlinear backstepping controller, and using multi-axis force sensors to measure cable tension, load state estimation is achieved. Furthermore, a control algorithm with disturbance compensation and saturation characteristics is designed.

Benefits of technology

It achieves high-precision load state estimation under complex external disturbances, reduces the complexity of sensor installation, and has real-time performance and robustness. It can effectively cope with external disturbances and complex operating scenarios during the hoisting process and meet the precise control requirements of UAV hoisting systems.

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Abstract

本发明涉及一种纵列式无人机吊载系统载荷状态估计与控制方法,包括以下步骤:基于牛顿运动定律建立无人机吊载系统的动力学模型,包括分别基于两个不同的状态变量的动力学模型;基于第一状态变量对应的动力学模型构建基于卡尔曼滤波器的观测器,利用多轴力传感器测量作用在载荷上的缆绳张力并作为所述观测器的已知输入,实现载荷状态估计;将第一状态变量下的载荷状态估计结果转换到第二状态变量下,并结合第二状态变量对应的动力学模型构建带饱和机制的非线性反步控制器,实现对无人机吊载系统的轨迹追踪控制。与现有技术相比,本发明能够精准捕捉载荷状态的变化特性,避免了传感器安装布线带来的复杂性,具有实时性强、控制精度高等优点。
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