Study on Capability of the Octocopter Configuration in Finite Element Analysis Simulation Environment

Authors: Benil Mathew Baby, Leonid Shpanin, Misko Abramiuk

Abstract:

High-voltage energy production on board the unmanned aerial vehicle (UAV) is one of the most rapidly growing emerging technologies for different applications in aerospace. Different energy harvesting and production techniques have already been investigated in multirotor drones, where the energy collected comes from the systems surrounding the ambient environment and typically involves the conversion of solar, kinetic, or thermal energies into electrical energy. In this contribution, a UAV structure is proposed for the production of a few tens of kilovolts on board of the UAV. The high voltage production mechanism on board of the UAV has not been investigated previously. The UAV geometry using the multirotor drone for production the high voltage on board of the UAV has been investigated theoretically using the ANSYS and MATLAB Finite Element Analysis (FEA) simulation tools. The industrially made MANTIS X8-PRO octocopter frame kit was used to explore the octocopter operation which was modelled for simulation studies. The high voltage electric circuit and components using octocopter geometry are developed through the integration of the mechanical parts on board of the UAV. Analysis of the modelled octocopter geometry and its performance is presented via a graphical representation of simulated parameters. The possibility of not using the landing gear in the proposed octocopter geometry is demonstrated. The conducted study evaluates the octocopter’s high voltage control technique and its impact on UAV energy consumption. FEA simulation results of the modelled high voltage electric circuit on board of the octocopter are presented exploring the performance of the octocopter and the structural challenges of its configuration. Applications of the proposed octocopter structure are discussed.

Keywords: high voltage production, energy harvesting, object modeling and control, unmanned aerial vehicle