• DocumentCode
    3510214
  • Title

    Simulation of Dynamic Inversion with Neural Network and its Applications to MAV

  • Author

    He Guang-Lin ; Wu Guo-hui

  • Author_Institution
    Sch. of Aerosp. Sci. & Technol., Beijing Inst. of Technol., Beijing
  • fYear
    2008
  • fDate
    1-3 Nov. 2008
  • Firstpage
    60
  • Lastpage
    63
  • Abstract
    The MAV accurate modes are typically unavailable. Most traditional methods for system design are complex and can not get satisfactory effect. Recent work in dynamic inversion with neural network may be applied to control a MAV where the reference commands include position, velocity, attitude and angular rate. This control technology can provide the MAV with an admirably command follow and steady control capability. Neural networks are used directly as the controller as well as indirect designs that are based on a neural network process model. The emulator is compiled by using NNCTRL20 and NNSYSID20 in MATLAB. Then the main result of this simulation is presented. It indicates that the method has high precision and strong stability, which can serve the control of MAV. Thereafter, an amendment about controlling system with dynamic inversion of the MAV is described.
  • Keywords
    aircraft control; neurocontrollers; stability; MATLAB; MAV; NNCTRL20; NNSYSID20; dynamic inversion; neural network; steady control capability; Aerodynamics; Aerospace control; Aircraft; Algorithm design and analysis; Attitude control; Control systems; Intelligent networks; Mathematical model; Neural networks; Nonlinear dynamical systems; MATLAB; MAV; dynamic inversion; neural network;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Networks and Intelligent Systems, 2008. ICINIS '08. First International Conference on
  • Conference_Location
    Wuhan
  • Print_ISBN
    978-0-7695-3391-9
  • Electronic_ISBN
    978-0-7695-3391-9
  • Type

    conf

  • DOI
    10.1109/ICINIS.2008.56
  • Filename
    4683168