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Frequency : 12 issues per year
Subject : Computer Applications and Technology
ISSN : 2319–8656 (Online)
Home Archives Volume 13 Issue 12 ijcatr13121001

IJCATR Volume 13 Issue 12

Design Parameters Effects on a Quadrotor Mini-UAV Consumed Energy

E. F. Herinantenaina, E. Rastefano
10.7753/IJCATR1312.1001
keywords : piloting mode, cubic minidrone, oblate spheroid minidrone, energy-consuming, shape choice

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This article focuses on the influence that a selection of design parameters has on the energy consumption of a quadcopter minidrone. The minidrone was modeled as a rigid body of the cylinder type with a 30 cm of radius, a 1,47 kg of weight and a 20 cm of height to assess the impacts of the piloting mode. To determine the mass and size effects, 250 g of loads were added, radius and height were increased 5 cm. A cubic minidrone and an oblate spheroid minidrone were studied to understand the influence of the shape choice. It was found that the oblate spheroid minidrone is the least energy-consuming, if we refer to the traveled distance and the maximum reached altitude with the same consumed energy. MATLAB-SIMULINK are used for the simulation.
@artical{e13122024ijcatr13121001,
Title = "Design Parameters Effects on a Quadrotor Mini-UAV Consumed Energy ",
Journal ="International Journal of Computer Applications Technology and Research(IJCATR)",
Volume = "13",
Issue ="12",
Pages ="1 - 4",
Year = "2024",
Authors ="E. F. Herinantenaina, E. Rastefano"}
  • The paper proposes a technique for identifying quadcopter minidrone design parameters impacts on energy consumption.
  • Hypotheses are adopted to characterize the used parameters.
  • Shape, size and weight are used to identify the least energy consuming minidrone.
  • In the simulation, a performance evaluation of the model is carried out.
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