• DocumentCode
    3349434
  • Title

    Vector field guidance for three-dimensional curved path following with fixed-wing UAVs

  • Author

    Yueqian Liang ; Yingmin Jia ; Junping Du ; Jun Zhang

  • Author_Institution
    Seventh Res. Div. & the Center for Inf. & Control, Beihang Univ. (BUAA), Beijing, China
  • fYear
    2015
  • fDate
    1-3 July 2015
  • Firstpage
    1187
  • Lastpage
    1192
  • Abstract
    This paper investigates the three-dimensional (3D) curved path following problem using fixed-wing unmanned aerial vehicles (UAVs) in the presence of constant wind disturbance. Vector field based approaches are used as the solution. Two vector fields are first developed, one is the tangent vector field based on path tangent vector and coordinate transformation, and the other is the combined vector field based on the combination of a conservative vector field and a solenoidal vector field. A unified jointly saturated course rate and saturated climb rate controller is designed based on the proposed vector fields. Simulations are conducted to demonstrate the effectiveness of the proposed approach.
  • Keywords
    autonomous aerial vehicles; position control; simulation; vectors; conservative vector field; coordinate transformation; fixed-wing UAV; fixed-wing unmanned aerial vehicles; path tangent vector; simulations; solenoidal vector field; three-dimensional curved path following problem; vector field guidance; wind disturbance; Convergence; Electronic mail; Kinematics; Mathematical model; Target tracking; Three-dimensional displays; Trajectory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference (ACC), 2015
  • Conference_Location
    Chicago, IL
  • Print_ISBN
    978-1-4799-8685-9
  • Type

    conf

  • DOI
    10.1109/ACC.2015.7170894
  • Filename
    7170894