Design, Modeling and Control of an Over-actuated Hexacopter Tilt-Rotor-Reference-Cited by-同舟云学术

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Design, Modeling and Control of an Over-actuated Hexacopter Tilt-Rotor

Published:2023-06-12 Issue: Volume: Page:
ISSN:
Container-title:2023 24th International Carpathian Control Conference (ICCC)
language:
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Author:

Pimentel Gabriel Oliveira¹,Dos Santos Murillo Ferreira¹,Honório Leonardo de Mello²,Mercorelli Paolo³,Da Silva Mathaus Ferreira²,Moreira António Paulo Gomes Mendes⁴

Affiliation:

1. CEFET-MG,Department of Electroelectronics,Leopoldina,Brasil

2. UFJF,Department of Energy,Juiz de Fora,Brasil

3. Leuphana University of Lüneburg,Institute for Production Technology and Systems (IPTS),Germany

4. INESC TEC - FEUP,iiLab - Industry and Innovation Lab,Porto,Portugal

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10178879/10178882/10178948.pdf?arnumber=10178948

Reference28 articles.

1. Active Fault Tolerant Control of a quadrotor UAV based on gainscheduled PID control

2. Robust fault-tolerant method in the ducted fan uav attitude control;ren;International Conference on Automatic Control and Artificial Intelligence (ACAI 2012),2012

3. Fast real-time control allocation applied to over-actuated quadrotor tilt-rotor;santos;Journal of Intelligent & Robotic Systems,2021

4. Analysis of a fast control allocation approach for nonlinear over-actuated systems;santos;ISA Transactions,2021

5. Adaptive control of a quadrotor with unknown model parameters;rashid;International Bhurban Conference on Applied Sciences & Technology (IBCAST),2012

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