• DocumentCode
    3527748
  • Title

    Trajectory generation and control of a quadrotor with a cable-suspended load - A differentially-flat hybrid system

  • Author

    Sreenath, Koushil ; Michael, Nathan ; Kumar, Vipin

  • fYear
    2013
  • fDate
    6-10 May 2013
  • Firstpage
    4888
  • Lastpage
    4895
  • Abstract
    A quadrotor with a cable-suspended load with eight degrees of freedom and four degrees underactuation is considered and the system is established to be a differentially-flat hybrid system. Using the flatness property, a trajectory generation method is presented that enables finding nominal trajectories with various constraints that not only result in minimal load swing if required, but can also cause a large swing in the load for dynamically agile motions. A control design is presented for the system specialized to the planar case, that enables tracking of either the quadrotor attitude, the load attitude or the position of the load. Stability proofs for the controller design and experimental validation of the proposed controller are presented.
  • Keywords
    aircraft control; attitude control; control system synthesis; helicopters; stability; trajectory control; cable-suspended load; control design; differentially-flat hybrid system; dynamically agile motions; flatness property; load attitude; nominal trajectories; quadrotor attitude; quadrotor control; stability proofs; trajectory generation method; Attitude control; Dynamics; Load modeling; Three-dimensional displays; Tracking; Trajectory; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Robotics and Automation (ICRA), 2013 IEEE International Conference on
  • Conference_Location
    Karlsruhe
  • ISSN
    1050-4729
  • Print_ISBN
    978-1-4673-5641-1
  • Type

    conf

  • DOI
    10.1109/ICRA.2013.6631275
  • Filename
    6631275