Design and Development Analysis of Quadcopter

Authors

  • Parihar P Final Year Department of Mechanical Engineering Mandsaur Institute of Technology, Mandsaur (M.P.)
  • Bhawsar P Final Year Department of Mechanical Engineering Mandsaur Institute of Technology, Mandsaur (M.P.)
  • Hargod P Final Year Department of Mechanical Engineering Mandsaur Institute of Technology, Mandsaur (M.P.)

Keywords:

Quadcopter, balancing, drone, multi-rotor

Abstract

UAVs are widely used in military operations as well as industries nowadays because of their reliability, cost effectiveness and multi-functionality. Stage, research have been made on quadcopter by worldwide researchers. Thispaper describes the study of the each components of the Quadcopter and analysis of the Quadcopter‟s assembly with concept of the thrust.This means going through the process of researching previous models, performing calculations, purchasing individual parts, testing those parts, designing the final product. Experimental results show the improvements of the stability of Quadcopter. Our news and features will cover developments in quadcopter technologies, innovative uses for quadcopter and how quadcopter use will impact society.

References

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School of Science Mat-2.4108 Independent research project in applied mathematics Espoo, August 22, 2011

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L. R. G. Carrillo, et al., Quad Rotorcraft Control: VisionBased Hovering and Navigation, Springer, 2012.

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Published

2024-02-26

How to Cite

Parihar, P., Bhawsar, P., & Hargod, P. (2024). Design and Development Analysis of Quadcopter. COMPUSOFT: An International Journal of Advanced Computer Technology, 5(06), 2128–2133. Retrieved from https://ijact.in/index.php/j/article/view/373

Issue

Section

Original Research Article

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