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    Velocity-Based Gain-Scheduled Lateral Auto-Pilot For An Agile Missile

    Leith, Douglas J. and Tsourdos, A. and White, B.A. and Leithead, W.E. (2000) Velocity-Based Gain-Scheduled Lateral Auto-Pilot For An Agile Missile. Control Engineering Practice, 9. pp. 1079-1093. ISSN 0967-0661

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    This paper investigates the application of velocity-based gain-scheduling techniques to a demanding, highly nonlinear, missile control design task. Scheduling on instantaneous incidence (a rapidly varying quantity) is well known to lead to considerable difficulties with conventional gain-scheduling methods. Moreover, the missile dynamics do not have well-defined relative degree at operating points where the lateral velocity is zero and thus conventional feedback linearisation methods cannot be applied to design a controller.

    Item Type: Article
    Keywords: Agile Missile;
    Academic Unit: Faculty of Science and Engineering > Research Institutes > Hamilton Institute
    Item ID: 1867
    Depositing User: Hamilton Editor
    Date Deposited: 24 Feb 2010 16:00
    Journal or Publication Title: Control Engineering Practice
    Publisher: Elsevier
    Refereed: Yes
      Use Licence: This item is available under a Creative Commons Attribution Non Commercial Share Alike Licence (CC BY-NC-SA). Details of this licence are available here

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