• DocumentCode
    2427998
  • Title

    Robust helicopter position control at hover

  • Author

    Weilenmann, Martin F. ; Christen, Urs ; Geering, Hans P.

  • Author_Institution
    Measure. & Control Lab., Swiss Federal Inst. of Technol., Zurich, Switzerland
  • Volume
    3
  • fYear
    1994
  • fDate
    29 June-1 July 1994
  • Firstpage
    2491
  • Abstract
    Position control for a radio controlled helicopter at hover is carried out using H2 and H∞ methods. Various problems arising in real-world tests are stated and solved by different means: prefilters are used to achieve step responses without overshoot. For plants with more outputs than inputs; a special H∞ design scheme is used. The implicit inversion of the plant in the H∞ controller can cause problems. This inversion can be avoided by a new scheme for weighting the sensitivity.
  • Keywords
    H∞ control; aircraft control; control system synthesis; helicopters; position control; robust control; step response; H∞ methods; H2 methods; hover; prefilters; robust helicopter position control; sensitivity weighting; step responses; Delay; Helicopters; Hydrogen; Laboratories; Position control; Position measurement; Radio control; Robust control; Rotors; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1994
  • Print_ISBN
    0-7803-1783-1
  • Type

    conf

  • DOI
    10.1109/ACC.1994.735007
  • Filename
    735007
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2427998