First flight tests for a quadrotor UAV with tilting propellers

Markus Ryll, Heinrich H. Bulthoff, Paolo Robuffo Giordano

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    80 Citations (Scopus)

    Abstract

    In this work we present a novel concept of a quadrotor UAV with tilting propellers. Standard quadrotors are limited in their mobility because of their intrinsic underactuation (only 4 independent control inputs vs. their 6-dof pose in space). The quadrotor prototype discussed in this paper, on the other hand, has the ability to also control the orientation of its 4 propellers, thus making it possible to overcome the aforementioned underactuation and behave as a fully-actuated flying vehicle. We first illustrate the hardware/software specifications of our recently developed prototype, and then report the experimental results of some preliminary, but promising, flight tests which show the capabilities of this new UAV concept.

    Original languageEnglish
    Title of host publication2013 IEEE International Conference on Robotics and Automation, ICRA 2013
    Pages295-302
    Number of pages8
    DOIs
    Publication statusPublished - 2013
    Event2013 IEEE International Conference on Robotics and Automation, ICRA 2013 - Karlsruhe, Germany
    Duration: 2013 May 62013 May 10

    Publication series

    NameProceedings - IEEE International Conference on Robotics and Automation
    ISSN (Print)1050-4729

    Other

    Other2013 IEEE International Conference on Robotics and Automation, ICRA 2013
    Country/TerritoryGermany
    CityKarlsruhe
    Period13/5/613/5/10

    ASJC Scopus subject areas

    • Software
    • Control and Systems Engineering
    • Artificial Intelligence
    • Electrical and Electronic Engineering

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