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Authors
Affiliations
1 Dept. of Engg., Mohamed Boudiaf University of Sci. and Tech., Oran, DZ
2 Laboratory City, Architecture and Heritage Polytechnique School of Architecture and Town planning, DZ
Source
International Journal of Vehicle Structures and Systems, Vol 10, No 4 (2018), Pagination: 273-277
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.
Full Text
References
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