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Optimal Altitude Determination for a Flying Drone in an Underground Mine Environment

  • Lukman Alabede
  • , Samuel Maimako
  • , Hassan Khaniani
  • , Pedram Roghanchi
  • , Navid Mojtabai
  • , Mostafa Hassanalian

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Scopus citations

Abstract

The nature of the task performed by quadrotors in underground mining operations places them in proximity to other objects and surfaces, generating external forces and torques due to aerodynamic effects. Flying a quadrotor at a lower altitude in an underground mining operation risks its efficiency being affected by ground effects. Flying at a high altitude poses a threat of crashing into the ceiling due to ceiling effects. This study investigates these interactions by employing a single-motor dynamometer mounted on a stepper motor, simulating UAV movements in proximity to various obstacles within an underground mine. The experiments assess the impact of altitude, surface proximity, and ventilation airflow on aerodynamic performance. The results show that the influence of ground effects is not significant when the quadrotor's altitude from the ground is equivalent to 2.7 times the radii of the propeller blade used in its design when operating within the proximity of ground and wall effects.

Original languageEnglish
Title of host publicationAIAA AVIATION FORUM AND ASCEND, 2025
DOIs
StatePublished - 2025
EventAIAA AVIATION FORUM AND ASCEND, 2025 - Las Vegas, United States
Duration: Jul 21 2025Jul 25 2025

Publication series

NameAIAA Aviation Forum and ASCEND, 2025

Conference

ConferenceAIAA AVIATION FORUM AND ASCEND, 2025
Country/TerritoryUnited States
CityLas Vegas
Period7/21/257/25/25

Bibliographical note

Publisher Copyright:
© 2025, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

Funding

This study was funded by the National Institute for Occupational Safety and Health (NIOSH) under the award #U60OH012351. The views, opinions and recommendations expressed herein are solely those of the authors and do not necessarily reflect the views of NIOSH. Mention of trade names, commercial products or organizations does not imply endorsement by the authors nor the funding organization.

Funders
National Institute for Occupational Safety and Health

    Keywords

    • Aerodynamic Performance
    • Aerodynamic Properties
    • Airspeed
    • Dynamometer
    • Electric Motors
    • Flow Visualization Techniques
    • Propeller Blades
    • Quadrotor
    • Unmanned Aerial Vehicle
    • Ventilation System

    ASJC Scopus subject areas

    • Space and Planetary Science
    • Energy Engineering and Power Technology
    • Nuclear Energy and Engineering
    • Aerospace Engineering

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