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Aerodynamic effect for collision-free reactive navigation of a small quadcopter

Research output: Journal Publications and ReviewsRGC 21 - Publication in refereed journalpeer-review

22 Downloads (CityUHK Scholars)

Abstract

The small footprint of tiny multirotor vehicles is advantageous for accessing tight spaces, but their limited payload and endurance impact the ability to carry powerful sensory and computing units for navigation. This article reports an aerodynamics-based strategy for a ducted rotorcraft to avoid wall collisions and explore unknown environments. The vehicle uses the minimal sensing system conventionally conceived only for hovering. The framework leverages the duct-strengthened interaction between the propeller wake and vertical surfaces. When incorporated with the flight dynamics, the derived momentum-theory-based model allows the robot to estimate the obstacle’s distance and direction without range sensors or vision. To this end, we devised a flight controller and reactive navigation methods for the robot to fly safely in unexplored environments. Flight experiments validated the detection and collision avoidance ability. The robot successfully identified and followed the wall contour to negotiate a staircase and evaded detected obstacles in proof-of-concept flights.

© The Author(s) 2023 
Original languageEnglish
Article number2
Journalnpj Robotics
Volume1
Online published26 Oct 2023
DOIs
Publication statusPublished - 2023

Funding

The work described in this paper was supported by the Research Grants Council of the Hong Kong Special Administrative Region, China (project no. CityU 11207621) and the Shenzhen-Hongkong-Macau Science and Technology Project (Category C) (project no. SGDX20220530111401009).

Publisher's Copyright Statement

  • This full text is made available under CC-BY 4.0. https://creativecommons.org/licenses/by/4.0/

RGC Funding Information

  • RGC-funded

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