• DocumentCode
    574464
  • Title

    Formation flight of unmanned rotorcraft based on robust and perfect tracking approach

  • Author

    Biao Wang ; Xiangxu Dong ; Chen, Ben M. ; Lee, Tong H. ; Swee King Phang

  • Author_Institution
    Dept. of Electr. & Comput. Eng., Nat. Univ. of Singapore, Singapore, Singapore
  • fYear
    2012
  • fDate
    27-29 June 2012
  • Firstpage
    3284
  • Lastpage
    3290
  • Abstract
    The paper presents a control scheme to the formation flight of a pair of unmanned rotorcraft. A leader-follower formation strategy is adopted and it is realized by utilizing the robust and perfect tracking (RPT) control approach. More specifically, individual RPT flight control laws are implemented in each aircraft, while the measurements from its neighbor and its own sensors are both taken into account for feedback to each aircraft system. In addition, a formation command generator is executed on the follower to ensure that it remains in formation with the leader. This control scheme facilitates the construction of formation flight systems and eases the changing of formation scale. Finally, the proposed formation flight strategy is realized and its performance is verified through several flight tests.
  • Keywords
    aerospace testing; autonomous aerial vehicles; helicopters; multi-robot systems; position control; tracking; RPT flight control law; aircraft system; feedback; flight testing; formation command generator; formation flight system; leader-follower formation strategy; perfect tracking control approach; robust tracking control approach; sensor; unmanned rotorcraft; Acceleration; Equations; Helicopters; Lead; Mathematical model; Robustness;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference (ACC), 2012
  • Conference_Location
    Montreal, QC
  • ISSN
    0743-1619
  • Print_ISBN
    978-1-4577-1095-7
  • Electronic_ISBN
    0743-1619
  • Type

    conf

  • DOI
    10.1109/ACC.2012.6315049
  • Filename
    6315049