International Journal of Vehicle Structures and Systems

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Study and Realization of a Prototype Octocopter System with PID Controller


Affiliations
1 Dept. of Engg., Mohamed Boudiaf University of Sci. and Tech., Oran, Algeria
2 Laboratory City, Architecture and Heritage Polytechnique School of Architecture and Town planning, Algeria
 

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In this work, the mechanical and electrical components are designed and realised for an octocopter. The designed system dynamic model is supported with Euler-Lagrangian model and Newton-Euler model respectively for the rotational and transnational movements of the drone. The prototype octocopter is also equipped with a proportional integral derivative controller to feedback both location and respond to the external environment.

Keywords

Octocopter, Aerodynamics, System Dynamics, Brushless DC Electric Motor, Proportional Integral Derivative Controller.
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  • Y.Z. Boudjelthia and I. Settouti. 2013. Modeling and Control of a Four-rotor in Six Degrees of Freedom, Master Thesis, University Hassiba Benbouali of Chlef.

  • B. Musabyimana and B. Bouheraoua. 2016. Control of Systems by a PID Corrector of Fractional Order Application: Quadri-rotor Control, Master Thesis, Hassiba Benbouali University of Chlef.

  • H. Khebache. 2012. Fault Tolerance via the Back Stepping Method of Nonlinear Systems, Application: Quadrirotor type UAV system, Master Thesis, University Ferhat Abbas de Setif.

  • R. Ayad. 2010. Design and Construction of a Quadrirotor Drone, Master Thesis, University of Sci. and Tech. Mh. Boudiaf d'Oran.


Abstract Views: 304

PDF Views: 148




  • Study and Realization of a Prototype Octocopter System with PID Controller

Abstract Views: 304  |  PDF Views: 148

Authors

Saidi Hemza
Dept. of Engg., Mohamed Boudiaf University of Sci. and Tech., Oran, Algeria
Djebri Boualem
Laboratory City, Architecture and Heritage Polytechnique School of Architecture and Town planning, Algeria

Abstract


In this work, the mechanical and electrical components are designed and realised for an octocopter. The designed system dynamic model is supported with Euler-Lagrangian model and Newton-Euler model respectively for the rotational and transnational movements of the drone. The prototype octocopter is also equipped with a proportional integral derivative controller to feedback both location and respond to the external environment.

Keywords


Octocopter, Aerodynamics, System Dynamics, Brushless DC Electric Motor, Proportional Integral Derivative Controller.

References





DOI: https://doi.org/10.4273/ijvss.10.4.09