Vision-Based Nonlinear Control of Quadrotors Using the Photogrammetric Technique

Author:

Guillén-Bonilla José Trinidad1ORCID,Vaca García Claudia Carolina2ORCID,Di Gennaro Stefano34ORCID,Sánchez Morales María Eugenia2ORCID,Acosta Lúa Cuauhtémoc24ORCID

Affiliation:

1. Centro Universitario de Ciencias Exactas e Ingeniería–UdG, Blvd. Gral. Marcelino García Barragán 1421, Olímpica, 44430, Guadalajara, Jalisco, Mexico

2. Departamento de Ciencias Tecnológicas, Universidad de Guadalajara, Centro Universitario de La Ciénega, Av. Universidad 1115, 47820, Ocotlán, Jalisco, Mexico

3. Department of Information Engineering, Computer Science and Mathematics, University of L’Aquila, Via Vetoio, L’Aquila, Coppito, 67100, Italy

4. Center of Excellence DEWS, University of L’Aquila, Via Vetoio, L’Aquila, Coppito, 67100, Italy

Abstract

This paper presents a controller designed via the backstepping technique, for the tracking of a reference trajectory obtained via the photogrammetric technique. The dynamic equations used to represent the motion of the quadrotor helicopter are based on the Newton–Euler model. The resulting quadrotor model has been divided into four subsystems for the altitude, longitudinal, lateral, and yaw motions. A control input is designed for each subsystem. Furthermore, the photogrammetric technique has been used to obtain the reference trajectory to be tracked. The performance and effectiveness of the proposed nonlinear controllers have been tested via numerical simulations using the Pixhawk Pilot Support Package developed for Matlab/Simulink.

Funder

European Project ECSEL–JURIA–2018

Publisher

Hindawi Limited

Subject

General Engineering,General Mathematics

Reference31 articles.

1. Dynamical modeling and boundary vibration control of a rigid–flexible wing system;W. He;IEEE/ASME Transaction on Mechatronics,2020

2. Design and control of an indoor micro quadrotor;S. Bouabdallah

3. Parameter identification for unmanned four–rotor helicopter with nonlinear model;Y. Zeng

4. Control and Navigation Framework for Quadrotor Helicopters

5. Experimental validation of a quaternion–based attitude estimation with direct input to a quadcopter control system;O. Magnussen

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