Design and Development of a Mini Drone for Educational Applications

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This is an unedited manuscript accepted for publication and provided as an Article in Press for early access at the author’s request. The article will undergo copyediting, typesetting, and galley proof review before final publication. Please be aware that errors may be identified during production that could affect the content. All legal disclaimers of the journal apply.

Year : 2026 | Volume : 16 | 01 | Page :
    By

    Anup Kumar Sharma,

  • Dr Rachit Srivastava,

  1. Student, Department of Electrical Engineering Bansal Institute of Engineering and Technology Lucknow, Uttar Pradesh, India
  2. Assistant Professor, Department of Electrical Engineering Bansal Institute of Engineering and Technology Lucknow, Uttar Pradesh, India

Abstract

This paper describe the complete process of designing, building, and testing a small unmanned aerial vehicle (UAV), normally referred to as a drone. The plan combines key concept from aerodynamics, electronics, control engineering, and embedded programming to produce a functional sample. The drone was developed using trivial structural materials and affordable components, including brushless DC motors, electronic speed controller (ESCs), a flight controller, various sensors, and a lithium-polymer (Li-Po) battery. To ensure cost, ease of assembly, and suitability for educational use, lightweight and reasonably priced structural materials were used in the construction of the UAV. The goal was to reduce total weight while preserving enough structural strength to endure flight stresses. Brushless DC motors and electronic speed controllers (ESCs), which provide accurate motor control and effective thrust generation, made up the propulsion system. Because of its high energy density and appropriateness for aerial applications, a lithium- polymer (Li-Po) battery was chosen as the power source. To enable real-time attitude estimate and stabilization, the drone also included a microcontroller- based flight controller and a number of onboard sensors, including accelerometers, gyroscopes, and magnetometers. The development workflow included invented story review, mechanical assembly, electronic amalgamation, software setup, and a series of test flights. concert evaluation determined on parameters such as stability, control response, and power usage. The investigational results showed that the drone was capable of maintain a steady hover, responding smoothly to directional directives, and functioning with good energy efficiency. This work highlights the value of mini-drones as an effective enlightening tool for erudition across multiple STEM domains. It also points toward future improvements such as incorporate GPS-based navigation, computer vision modules, and self-directed flight wherewithal to enhance functionality and real- world applicability.

Keywords: Mini Drone, brushless DC motors, lithium-polymer

How to cite this article:
Anup Kumar Sharma, Dr Rachit Srivastava. Design and Development of a Mini Drone for Educational Applications. Journal of Aerospace Engineering & Technology. 2026; 16(01):-.
How to cite this URL:
Anup Kumar Sharma, Dr Rachit Srivastava. Design and Development of a Mini Drone for Educational Applications. Journal of Aerospace Engineering & Technology. 2026; 16(01):-. Available from: https://journals.stmjournals.com/joaet/article=2026/view=238993


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Ahead of Print Subscription Review Article
Volume 16
01
Received 04/12/2025
Accepted 11/12/2025
Published 21/03/2026
Publication Time 107 Days
72

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