In this paper, the design of nonlinear H/sub /spl infin// controller for autopilot application is presented. The design of nonlinear H/sub /spl infin// control action leads to a partial differential inequality or equation, namely, Hamilton-Jacobi-Isaacs (HJI) inequality. It is too difficult, if not impossible, to find an exact closed form solution for this inequality. However, there are some approximate solutions. In this paper, we will make use of one of the most efficient possible methods, Taylor Series Expansion of nonlinear terms appear in HJI. Simulation results of the proposed method on a missile's autopilot design show the effectiveness of the proposed algorithm.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Robust nonlinear H/sub /spl infin// autopilot design


    Contributors:


    Publication date :

    2003-01-01


    Size :

    267349 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Robust Nonlinear Missile Autopilot Design

    McFarland, M. B. / D'Souza, C. N. / International Federation of Automatic Control | British Library Conference Proceedings | 1995



    Robust backstepping ship autopilot design

    Bhatt, Aditi / Das, Swarup / Talole, S. E. | Taylor & Francis Verlag | 2021


    Robust Nonlinear Design of a High Incidence Missile Autopilot

    White, B. A. / Tsourdos, A. | British Library Conference Proceedings | 2001