Automatic unhooking control method and device, electronic equipment and storage medium

By calculating the decoupling driving torque and horizontal force adjustment value in real time by the decision controller, the problem of decoupling instability caused by extreme environment in multi-UAV intelligent collaborative tower erection is solved, and efficient and safe decoupling control in complex environment is achieved.

CN122403288APending Publication Date: 2026-07-17国网四川省电力公司电力应急中心
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
国网四川省电力公司电力应急中心
Filing Date
2026-06-11
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

In the construction of power transmission lines in complex terrains such as mountains and plateaus, the existing automatic uncoupling control methods in multi-UAV intelligent collaborative tower erection technology have failed to effectively cope with extreme environmental factors, such as low temperature, low air pressure and strong wind, resulting in frozen mechanical parts, electronic system signal interference and poor uncoupling stability, which affects the continuity and stability of the operation.

Method used

An automatic unhooking control method is adopted. The decision controller receives sensor data from the bolt installation drone and the hoisting drone, calculates the unhooking driving torque and horizontal force adjustment value in real time, and ensures that unhooking is carried out after the alignment accuracy and bolt preload meet the conditions. Dynamic compensation is also performed in combination with atmospheric density, wind speed and wind direction to achieve coordinated and synchronous unhooking of multiple drones.

Benefits of technology

It improves the accuracy, stability and safety of unhooking in multi-drone collaborative hoisting scenarios, reduces the risk of mechanism jamming and impact disturbance, and ensures the continuity and efficiency of tower erection construction.

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Abstract

本申请涉及一种自动脱钩控制方法、装置、电子设备和存储介质,方法包括:接收螺栓安装无人机发送的螺栓孔的对准精度和螺栓预紧力;接收各个所述吊装无人机发送的当前气象参数和拉力值;基于所述对准精度、所述螺栓预紧力、所述大气密度、所述风速、所述风向和所述拉力值确定各个所述吊装无人机的脱钩驱动力矩和各个所述吊装无人机的水平方向力调整值;将各个所述吊装无人机的脱钩驱动力矩和各个所述吊装无人机的水平方向力调整值发送至对应的所述吊装无人机,以使得各个所述吊装无人机一同执行脱钩。本申请的实施使脱钩控制量与高原低压及载荷变化等工况相匹配,降低机构卡滞、脱钩失败及冲击扰动风险。
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