• DocumentCode
    2705040
  • Title

    Design of hovering altitude holding control system for helicopter

  • Author

    Wang, Xiaoyan ; Wang, Xinmin ; Yao, Congchao

  • Author_Institution
    Dept. of Autom., Northwestern Polytech. Univ., Xi´´an, China
  • fYear
    2012
  • fDate
    6-8 June 2012
  • Firstpage
    180
  • Lastpage
    183
  • Abstract
    Effected by sea wave and other noises, altitude holding becomes difficult when helicopter is hovering or rescuing near the sea face. In this paper, according to the integrated height system of radio altimeter and vertical accelerometer, a Kalman filter is designed to get the accurate altitude signals of the helicopter hovering over the sea. Then, two altitude holding control structures are developed based on helicopter explicit model following control system (EMFCS), which has excellent operation characteristics. In order to simulate the real situation and to design the filter, sea wave model is established by using the rational spectrum modeling method. Simulation results show that the two control systems designed both can realize helicopter hovering altitude holding efficiently, and have good resistance to vertical wind disturbance or parametric perturbations.
  • Keywords
    Kalman filters; aircraft control; helicopters; ocean waves; position control; EMFCS; Kalman filter; helicopter explicit model following control system; helicopter hovering; hovering altitude holding control system; integrated height system; parametric perturbations; radio altimeter; rational spectrum modeling method; sea wave model; vertical accelerometer; vertical wind disturbance; Filtering theory; Helicopters; Mathematical model; Noise measurement; Sea measurements; White noise; altitude holding; filter; helicopter; hovering; wave model;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Information and Automation (ICIA), 2012 International Conference on
  • Conference_Location
    Shenyang
  • Print_ISBN
    978-1-4673-2238-6
  • Electronic_ISBN
    978-1-4673-2236-2
  • Type

    conf

  • DOI
    10.1109/ICInfA.2012.6246804
  • Filename
    6246804