The main purpose of an orbit control system is to guarantee the tracking of a predefined orbit, despite the effects of disturbances from different nature with specific constrains in terms of orbit correction and tracking errors. In this paper, the problem is formally defined and an innovative solution is proposed using a methodology that involves new approaches in the model definition, in the mathematical characterization and in the application of modern robust controller synthesis techniques. From the simulation results we can see that these approach is used for a low earth orbiter as they recover the earth gravity field.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    A modern approach to drag attenuation in a Hinfinity robust orbit control


    Contributors:
    Prieto, D. (author) / Bona, B. (author)


    Publication date :

    2004


    Size :

    2 Seiten, 5 Quellen




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Hinfinity robust control design for dynamic ship positioning

    Katebi, M.R. / Grimble, M.J. / Zhang, Y. | Tema Archive | 1997



    Robust Hinfinity control of uncertain linear systems via static output feedback

    Köse, I.E. / Schmitendorf, W.E. | Tema Archive | 1995


    Robust Hinfinity control in active vibration control of piezoelectric smart structure

    Zhu, Xiaojin / Liu, Jinsong / Huang, Quanzhen et al. | Tema Archive | 2009


    F-16 nonlinear Hinfinity control

    Kung, Chien-Chung / Yang, Ciann-Dong | Tema Archive | 2002