IDEAS home Printed from https://ideas.repec.org/a/hin/jnlmpe/284869.html
   My bibliography  Save this article

Sliding Mode Control for Mass Moment Aerospace Vehicles Using Dynamic Inversion Approach

Author

Listed:
  • Xiao-Yu Zhang
  • Yu-Xin Zhao
  • De-Xin Xu
  • Kun-Peng He

Abstract

The moving mass actuation technique offers significant advantages over conventional aerodynamic control surfaces and reaction control systems, because the actuators are contained entirely within the airframe geometrical envelope. Modeling, control, and simulation of Mass Moment Aerospace Vehicles (MMAV) utilizing moving mass actuators are discussed. Dynamics of the MMAV are separated into two parts on the basis of the two time-scale separation theory: the dynamics of fast state and the dynamics of slow state. And then, in order to restrain the system chattering and keep the track performance of the system by considering aerodynamic parameter perturbation, the flight control system is designed for the two subsystems, respectively, utilizing fuzzy sliding mode control approach. The simulation results describe the effectiveness of the proposed autopilot design approach. Meanwhile, the chattering phenomenon that frequently appears in the conventional variable structure systems is also eliminated without deteriorating the system robustness.

Suggested Citation

  • Xiao-Yu Zhang & Yu-Xin Zhao & De-Xin Xu & Kun-Peng He, 2013. "Sliding Mode Control for Mass Moment Aerospace Vehicles Using Dynamic Inversion Approach," Mathematical Problems in Engineering, Hindawi, vol. 2013, pages 1-11, October.
    • Handle: RePEc:hin:jnlmpe:284869
    DOI: 10.1155/2013/284869
    as

    Download full text from publisher

    File URL: http://downloads.hindawi.com/journals/MPE/2013/284869.pdf
    Download Restriction: no
    File URL: http://downloads.hindawi.com/journals/MPE/2013/284869.xml
    Download Restriction: no
    File URL: https://libkey.io/10.1155/2013/284869?utm_source=ideas
    LibKey link: if access is restricted and if your library uses this service, LibKey will redirect you to where you can use your library subscription to access this item
    ---><---

    More about this item

    Statistics

    Access and download statistics

    Corrections

    All material on this site has been provided by the respective publishers and authors. You can help correct errors and omissions. When requesting a correction, please mention this item's handle: RePEc:hin:jnlmpe:284869. See general information about how to correct material in RePEc.

    If you have authored this item and are not yet registered with RePEc, we encourage you to do it here. This allows to link your profile to this item. It also allows you to accept potential citations to this item that we are uncertain about.

    We have no bibliographic references for this item. You can help adding them by using this form .

    If you know of missing items citing this one, you can help us creating those links by adding the relevant references in the same way as above, for each refering item. If you are a registered author of this item, you may also want to check the "citations" tab in your RePEc Author Service profile, as there may be some citations waiting for confirmation.

    For technical questions regarding this item, or to correct its authors, title, abstract, bibliographic or download information, contact: Mohamed Abdelhakeem (email available below). General contact details of provider: https://www.hindawi.com .

    Please note that corrections may take a couple of weeks to filter through the various RePEc services.

    IDEAS is a RePEc service. RePEc uses bibliographic data supplied by the respective publishers.