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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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Detalhes bibliográficos
Principais autores: Abhishek Manalathody, Kishoor Santhana Krishnan, Jisnu Adindtra Subramanian, Sakthivel Thangavel, Jinraj V. Pushpangathan, Hariprasanth Paranjothy
Formato: Artigo
Idioma:Inglês
Publicado em: IEEE 2025-01-01
Colecção:IEEE Access
Assuntos:
Acesso em linha:https://ieeexplore.ieee.org/document/10927603/
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