An Over-Actuated Hexacopter Tilt-Rotor UAV Prototype for Agriculture of Precision: Modeling and Control

This paper focuses on the modeling, control, and simulation of an over-actuated hexacopter tilt-rotor (HTR). This configuration implies that two of the six actuators are independently tilted using servomotors, which provide high maneuverability and reliability. This approach is predicted to maintain...

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Main Authors: Gabriel Oliveira Pimentel, Murillo Ferreira dos Santos, José Lima, Paolo Mercorelli, Fernanda Mara Fernandes
Format: Article
Language:English
Published: MDPI AG 2025-01-01
Series:Sensors
Subjects:
Online Access:https://www.mdpi.com/1424-8220/25/2/479
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author Gabriel Oliveira Pimentel
Murillo Ferreira dos Santos
José Lima
Paolo Mercorelli
Fernanda Mara Fernandes
author_facet Gabriel Oliveira Pimentel
Murillo Ferreira dos Santos
José Lima
Paolo Mercorelli
Fernanda Mara Fernandes
author_sort Gabriel Oliveira Pimentel
collection DOAJ
description This paper focuses on the modeling, control, and simulation of an over-actuated hexacopter tilt-rotor (HTR). This configuration implies that two of the six actuators are independently tilted using servomotors, which provide high maneuverability and reliability. This approach is predicted to maintain zero pitch throughout the trajectory and is expected to improve the aircraft’s steering accuracy. This arrangement is particularly beneficial for precision agriculture (PA) applications where accurate monitoring and management of crops are critical. The enhanced maneuverability allows for precise navigation in complex vineyard environments, enabling the unmanned aerial vehicle (UAV) to perform tasks such as aerial imaging and crop health monitoring. The employed control architecture consists of cascaded proportional (P)-proportional, integral and derivative (PID) controllers using the successive loop closure (SLC) method on the five controlled degrees of freedom (DoFs). Simulated results using Gazebo demonstrate that the HTR achieves stability and maneuverability throughout the flight path, significantly improving precision agriculture practices. Furthermore, a comparison of the HTR with a traditional hexacopter validates the proposed approach.
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issn 1424-8220
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series Sensors
spelling doaj-art-cabee3a716ef4f6d81197205d205b77f2025-01-24T13:49:05ZengMDPI AGSensors1424-82202025-01-0125247910.3390/s25020479An Over-Actuated Hexacopter Tilt-Rotor UAV Prototype for Agriculture of Precision: Modeling and ControlGabriel Oliveira Pimentel0Murillo Ferreira dos Santos1José Lima2Paolo Mercorelli3Fernanda Mara Fernandes4Department of Electroelectronics, Federal Center of Technological Education of Minas Gerais (CEFET-MG), Leopoldina 36700-001, BrazilDepartment of Electroelectronics, Federal Center of Technological Education of Minas Gerais (CEFET-MG), Leopoldina 36700-001, BrazilResearch Centre in Digitalization and Intelligent Robotics (CeDRI), Sustainability and Technology in Mountain Regions (SusTEC), Instituto Politécnico de Bragança (IPB), 5300-253 Bragança, PortugalInstitute for Production Technology and Systems (IPTS), Leuphana Universität Lüneburg, 21335 Lüneburg, GermanyFaculty of Minas Gerais (FAMINAS), Muriaé 36888-233, BrazilThis paper focuses on the modeling, control, and simulation of an over-actuated hexacopter tilt-rotor (HTR). This configuration implies that two of the six actuators are independently tilted using servomotors, which provide high maneuverability and reliability. This approach is predicted to maintain zero pitch throughout the trajectory and is expected to improve the aircraft’s steering accuracy. This arrangement is particularly beneficial for precision agriculture (PA) applications where accurate monitoring and management of crops are critical. The enhanced maneuverability allows for precise navigation in complex vineyard environments, enabling the unmanned aerial vehicle (UAV) to perform tasks such as aerial imaging and crop health monitoring. The employed control architecture consists of cascaded proportional (P)-proportional, integral and derivative (PID) controllers using the successive loop closure (SLC) method on the five controlled degrees of freedom (DoFs). Simulated results using Gazebo demonstrate that the HTR achieves stability and maneuverability throughout the flight path, significantly improving precision agriculture practices. Furthermore, a comparison of the HTR with a traditional hexacopter validates the proposed approach.https://www.mdpi.com/1424-8220/25/2/479hexacopterover-actuated UAVtilt-rotor
spellingShingle Gabriel Oliveira Pimentel
Murillo Ferreira dos Santos
José Lima
Paolo Mercorelli
Fernanda Mara Fernandes
An Over-Actuated Hexacopter Tilt-Rotor UAV Prototype for Agriculture of Precision: Modeling and Control
Sensors
hexacopter
over-actuated UAV
tilt-rotor
title An Over-Actuated Hexacopter Tilt-Rotor UAV Prototype for Agriculture of Precision: Modeling and Control
title_full An Over-Actuated Hexacopter Tilt-Rotor UAV Prototype for Agriculture of Precision: Modeling and Control
title_fullStr An Over-Actuated Hexacopter Tilt-Rotor UAV Prototype for Agriculture of Precision: Modeling and Control
title_full_unstemmed An Over-Actuated Hexacopter Tilt-Rotor UAV Prototype for Agriculture of Precision: Modeling and Control
title_short An Over-Actuated Hexacopter Tilt-Rotor UAV Prototype for Agriculture of Precision: Modeling and Control
title_sort over actuated hexacopter tilt rotor uav prototype for agriculture of precision modeling and control
topic hexacopter
over-actuated UAV
tilt-rotor
url https://www.mdpi.com/1424-8220/25/2/479
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