• DocumentCode
    736719
  • Title

    Four-axis gimbal system application based on gimbal self-adaptation adjustment

  • Author

    Jie, Ma ; Qinbei, Xu

  • Author_Institution
    Harbin Institute of Technology, Harbin 150001, P.R. China
  • fYear
    2015
  • fDate
    28-30 July 2015
  • Firstpage
    8866
  • Lastpage
    8871
  • Abstract
    Gimbal lock is a common physical phenomenon in the gimbal system. As for the three-axis gimbal system, gimbal lock could not be avoided when two axes are driven into being collinear with each other. As a result, it will lead to the loss of one degree of rotational freedom. This paper analyses the limitation of three-axis gimbal system in flight attitude motion simulation and introduces a new system of four-axis gimbal set, which contains a redundant forth axis. And then, a kind of gimbal angle algorithm based on base gimbal self-adaptation adjustment was presented to successfully solve the running angles of the four gimbals. According to theoretical analysis and MATLAB simulation result, this application scheme could drive four-axis gimbal system to simulate wide attitude motion of the flight vehicle rather than suffering singularity.
  • Keywords
    Computers; Kinematics; Mathematical model; Payloads; Simulation; Trajectory; Vehicles; Attitude algorithm; Four-axis gimbal; Gimbal lock; Redundant degree of freedom; Singularity;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2015 34th Chinese
  • Conference_Location
    Hangzhou, China
  • Type

    conf

  • DOI
    10.1109/ChiCC.2015.7261040
  • Filename
    7261040