• DocumentCode
    2616821
  • Title

    Trajectory planning for a quadrotor helicopter

  • Author

    Bouktir, Y. ; Haddad, M. ; Chettibi, T.

  • Author_Institution
    Lab. of Struct. Mech., Algiers
  • fYear
    2008
  • fDate
    25-27 June 2008
  • Firstpage
    1258
  • Lastpage
    1263
  • Abstract
    A simple direct method able to generate time-optimal trajectories for a micro quadrotor helicopter is presented. It is based on modeling the quadrotor trajectory as a composition of a parametric function P(lambda) defining the quadrotor path, and a monotonically increasing function lambda(t), specifying the motion on this path. The optimal evolutions of P(lambda) and lambda(t), which are approximated using B-spline functions, are found using a nonlinear optimization technique. The proposed method accounts for the most important constraints inherent to the system behavior, such as underactuation, obstacles avoidance and limits on actuator torques and speeds.
  • Keywords
    aerospace control; collision avoidance; helicopters; nonlinear programming; splines (mathematics); B-spline function; actuator speed; actuator torque; microquadrotor helicopter; nonlinear optimization; obstacles avoidance; optimal evolution; parametric function; quadrotor trajectory; time-optimal trajectories; trajectory planning; unmanned air vehicles; Helicopters; Linear feedback control systems; Motion control; Nonlinear dynamical systems; Predictive models; Robots; Sliding mode control; Trajectory; Unmanned aerial vehicles; Vehicle dynamics; dynamics; nonlinear optimization; quadrotor; trajectory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Automation, 2008 16th Mediterranean Conference on
  • Conference_Location
    Ajaccio
  • Print_ISBN
    978-1-4244-2504-4
  • Electronic_ISBN
    978-1-4244-2505-1
  • Type

    conf

  • DOI
    10.1109/MED.2008.4602025
  • Filename
    4602025