• DocumentCode
    1795268
  • Title

    Distributed control of nonlinear elastic formation of unmanned aerial vehicles

  • Author

    Xu Guangyan ; Li Zheng

  • Author_Institution
    Main Studying Direction is Air Dynamics & Control of Spacecraft & its Formation, Shenyang Aerosp. Univ., Shenyang, China
  • fYear
    2014
  • fDate
    8-10 Aug. 2014
  • Firstpage
    2181
  • Lastpage
    2186
  • Abstract
    For an Unmanned Aerial Vehicle (UAV) formation in “leader-follower” mode, a bran-new concept of nonlinear elastic distance vector is proposed, which helps achieve much more excellent control effect. Based on the nonlinear elastic distance vector, through a big mountain of mathematical work the mathematical model of UAV formation flight is built and linearized skillfully. A new model of UAV formation flight is obtained, which has distinct physical meaning and simple form. And on this basis, by introducing some simplification and symmetry of feedback gain, a fire-new high-efficiency distributed controller of elastic formation is designed. Even better, it expends munch small control cost while providing such better control effect. Then the stability of the controller is proved subtly and a very important theorem offers sufficient conditions for the stability of the model is proposed. Simulation results show that controller can keep the formation much more effectively. In addition, the control quantity is only related to two elements: One is the speed of controlled vehicle itself, the other is the relative distance between controlled vehicle and its neighbor. For this reason, the control problem becomes more simple.
  • Keywords
    autonomous aerial vehicles; control system synthesis; distributed control; feedback; mobile robots; nonlinear control systems; stability; vectors; UAV formation flight mathematical model; distributed control; feedback gain; leader-follower mode; nonlinear elastic distance vector; stability; sufficient conditions; unmanned aerial vehicle nonlinear elastic formation; Acceleration; Aerodynamics; Aerospace control; Educational institutions; Mathematical model; Stability analysis; Vectors; UAV formation; distributed control; nonlinear elastic coefficient;
  • 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.2014.7007511
  • Filename
    7007511