• DocumentCode
    181487
  • Title

    Influence of number of measured states on accuracy and robustness of flight control system

  • Author

    Klipa, A.M. ; Sydorenko, A.D.

  • Author_Institution
    Aircraft Control Syst. Dept., Nat. Aviation Univ., Kiev, Ukraine
  • fYear
    2014
  • fDate
    14-17 Oct. 2014
  • Firstpage
    125
  • Lastpage
    128
  • Abstract
    Recently in many countries the efforts of researchers are directed to the design of low cost, accurate and robust controllers for small Unmanned Aerial Vehicle (UAV) using the minimum number of on-board sensors. The basic problem of such kind of design is to restore the unknown (unmeasured) states. The approach proposed in the paper consists of two procedures: state restoration by the reduced-order observer (Luenberger filter) and optimal deterministic controller design. This technique was applied to the “benchmark” model of UAV longitudinal motion (there were considered two cases: with three and two on-board sensors only) and results of its application are presented.
  • Keywords
    aircraft control; autonomous aerial vehicles; control system synthesis; observers; optimal control; Luenberger filter; UAV longitudinal motion; flight control system; measured states; on-board sensors; optimal deterministic controller design; reduced-order observer; state restoration; unmanned aerial vehicle; Aerospace control; Aircraft; Mathematical model; Observers; Robustness; Sensors; Vectors; aircraft and actuator dynamics; incomplete measurements; longitudinal motion; optimal deterministic controller; small UAV; state restoration;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Methods and Systems of Navigation and Motion Control (MSNMC), 2014 IEEE 3rd International Conference on
  • Conference_Location
    Kiev
  • Print_ISBN
    978-1-4799-6578-6
  • Type

    conf

  • DOI
    10.1109/MSNMC.2014.6979749
  • Filename
    6979749