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Research on Modeling and Control of a Quadrotor Slung-Load System Based on Kane’s Method
Received date: 2025-04-10
Online published: 2025-11-28
To address the problems of cumbersome modeling procedures, low computational efficiency in conventional methods(Newton-Euler/Lagrange) for quadrotor UAV slung-load systems, and excessive load swing stabilization time, this study first proposes a Kane’s method-based approach for establishing the dynamic model of the quadrotor slung-load system. This method eliminates the need to analyze ideal constraint forces required in Newton-Euler formulations and avoids computations of dynamic functions and their derivatives in Lagrange methods. Building upon this foundation, an anti-swing controller integrating Adaptive Moment Estimation-Neural Network-PID (Adam-NN-PID) is designed, combined with a swing angle-displacement control strategy to achieve rapid load stabilization. Finally, the simulation introduces multiple wind disturbances to investigate the dynamic control performance. Results demonstrate that compared to conventional PID and BPNN-PID swing angle controllers, the proposed Adam-NN-PID anti-swing controller achieves faster load stabilization with reduced swing amplitude.
Key words: Quadrotor suspend; Kane modeling; Load swing control; Adam-NN-PID
ZHOU Jiaxing , YU Zicheng , GAO Dengwei , HUANG Guilan , CHEN Zhigao , DENG Zhao . Research on Modeling and Control of a Quadrotor Slung-Load System Based on Kane’s Method[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2025 , 45(5) : 887 -899 . DOI: 10.15892/j.cnki.djzdxb.2025.05.033
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