• DocumentCode
    133127
  • Title

    MIMO closed-loop subspace model identification and hovering control of a 6-DOF coaxial miniature helicopter

  • Author

    Kojio, Jyunki ; Ishibashi, Haruka ; Inoue, Ryo ; Ushida, Shun ; Oku, Hideki

  • Author_Institution
    Osaka Inst. of Technol., Osaka, Japan
  • fYear
    2014
  • fDate
    9-12 Sept. 2014
  • Firstpage
    1679
  • Lastpage
    1684
  • Abstract
    This paper concerns black-box modeling of a radio-controlled (RC) coxial miniature helicopter by closed-loop subspace model identification with a multi-input and multi-output (MIMO) state space model, as well as model-based control design of hovering flight using the identified black-box model. The RC helicopter has 6 degrees of freedom (6-DOF) in its motions, namely, the lateral (left/right), vertical (up/down), longitudinal (fore/aft), pitching, rolling and yawing axes. These 6 parameters of the position and posture, as the outputs of the RC helicopter, are measured by a motion capture system with 6 high-speed cameras. The helicopter maneuvers, as the inputs, are done by the aileron, elevator, rudder and throttle. A closed-loop system identification experiment of the hovering RC helicopter is performed. CL-MOESP, which is one of closed-loop subspace model identification methods, is applied to the sampled closed-loop data in order to obtain a state-space model with an estimated order. Using the identified model, an LQ controller with a full-state observer is designed. Finally, as verification of the identified model, an experiment of hovering flight of the helicopter is performed with the implementation of the feedback controller.
  • Keywords
    MIMO systems; aircraft control; closed loop systems; control system synthesis; feedback; helicopters; 6-DOF coaxial miniature helicopter; MIMO closed-loop subspace model identification; closed-loop system; feedback controller; hovering control; hovering flight; model-based control design; multiinput and multioutput state space model; radio-controlled coxial miniature helicopter; Adaptive control; Control design; Helicopters; MIMO; Mathematical model; Observers; Position measurement; autonomous flight control; closed-loop identification; miniture helicopter; subspace method; system identification experiment;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    SICE Annual Conference (SICE), 2014 Proceedings of the
  • Conference_Location
    Sapporo
  • Type

    conf

  • DOI
    10.1109/SICE.2014.6935291
  • Filename
    6935291