Nonlinear and Linear PID Controllers-Based Hybrid Flight Control Strategy for a Quadcopter With Slung Load

Nonlinear and Linear PID Controllers-Based Hybrid Flight Control Strategy for a Quadcopter With Slung Load

This paper proposes a new hybrid flight control strategy for a quadcopter with a slung load to achieve a user-defined trajectory following. The high-fidelity coupled nonlinear model involving the quadcopter and slung load is obtained by integrating the nonlinear slung load model with the nonlinear q...

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Bibliographic Details
Main Authors: Abhishek Manalathody, Kishoor Santhana Krishnan, Jisnu Adindtra Subramanian, Sakthivel Thangavel, Jinraj V. Pushpangathan, Hariprasanth Paranjothy
Format: Article
Language:English
Published: IEEE 2025-01-01
Series:IEEE Access
Subjects:
Nonlinear PID controller
quadcopter
slung load
autonomous aerial vehicles (AAVs)
Online Access:https://ieeexplore.ieee.org/document/10927603/
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https://ieeexplore.ieee.org/document/10927603/

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