• DocumentCode
    3485151
  • Title

    Trajectory tracking of unmanned aerial vehicle using servomechanism strategy

  • Author

    Kakirde, Nishant P. ; Davari, Asad ; Wang, Jin

  • Author_Institution
    MS Control Syst., WVU Tech, USA
  • fYear
    2005
  • fDate
    20-22 March 2005
  • Firstpage
    163
  • Lastpage
    166
  • Abstract
    This paper describes the application of servomechanism/output regulation strategy to unmanned aerial vehicles (UAV) for the trajectory tracking. In this paper all the aspects of the UAV tracking control from mathematical modeling to controller implementation are considered. Output regulation strategy is mainly used for the accurate tracking of the reference trajectory. In this paper the kinematic model of UAV is considered for the implementation of controller. Our approach is limited to a single unmanned aerial vehicle trajectory tracking. This strategy enables increased reliability, stability, quality assurance of safety critical UAVs. This output regulation strategy demonstrates the ability of accurate trajectory tracking, so it improves the overall performance of the UAV. In this paper we present the simulation results of implementation of the servomechanism strategy for UAV.
  • Keywords
    aircraft control; remotely operated vehicles; servomechanisms; stability; tracking; vehicle dynamics; kinematic model; output regulation strategy; servomechanism strategy; trajectory tracking; unmanned aerial vehicle; Control systems; Differential algebraic equations; Helicopters; Kinematics; Nonlinear equations; Partial differential equations; Servomechanisms; Trajectory; Unmanned aerial vehicles; Vehicle dynamics;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    System Theory, 2005. SSST '05. Proceedings of the Thirty-Seventh Southeastern Symposium on
  • ISSN
    0094-2898
  • Print_ISBN
    0-7803-8808-9
  • Type

    conf

  • DOI
    10.1109/SSST.2005.1460898
  • Filename
    1460898