• DocumentCode
    1794960
  • Title

    Minimum jerk trajectory generation of a quadrotor based on the differential flatness

  • Author

    Jing Yu ; Zhihao Cai ; Yingxun Wang

  • Author_Institution
    Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China
  • fYear
    2014
  • fDate
    8-10 Aug. 2014
  • Firstpage
    832
  • Lastpage
    837
  • Abstract
    In order to improve smoothness of task trajectories, this paper describe algorithms to generate smooth-optimal trajectories based on the differential flatness of quadrotor. B-spline is used to parameterize the selected flat outputs, and the dynamic constraints or kinematical constraints on quadrotor are transferred to the control point constraints of B-spline. The trajectory generation is then considered an optimal control problem by adopting the integral of squared jerk. And then the optimal solution is solved by transforming the optimal control problem into a nonlinear programming problem. At last the smoothness-optimal trajectories are generated. Simulation results show that, this method can smooth out movements and minimize the accumulative jerk which can decrease trajectory tracking errors effectively.
  • Keywords
    helicopters; nonlinear programming; optimal control; splines (mathematics); trajectory control; B-spline; differential flatness; dynamic constraints; kinematical constraints; minimum jerk trajectory generation; nonlinear programming problem; optimal control problem; quadrotor; smooth-optimal trajectories; trajectory tracking errors; Aerospace electronics; Equations; Optimal control; Programming; Splines (mathematics); Trajectory; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
  • Conference_Location
    Yantai
  • Print_ISBN
    978-1-4799-4700-3
  • Type

    conf

  • DOI
    10.1109/CGNCC.2014.7007318
  • Filename
    7007318