International Journal of Vehicle Structures and Systems

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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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