In this paper, the newly developed statistical control theory is revisited to autonomously control the satellite attitude as well as to provide a means of actively attenuating impulsive disturbances caused by servicing dock and space debris. Simulations are performed using several docking and collision scenarios. The simulation results indicate that the existing attitude control system with an innovative and robust statistical controller design shows significant promise for use in attitude hold mode operation despite the presence of impulsive disturbances.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Statistical Control Paradigm for Aerospace Structures Under Impulsive Disturbances


    Contributors:

    Publication date :

    2006


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Adaptive Control of Aerospace Structures with Persistent Disturbances

    Balas, M. J. / International Federation of Automatic Control | British Library Conference Proceedings | 2002


    Adaptive control of persistent disturbances for aerospace structures

    Balas, Mark / Fuentes, Robert / Erwin, R. | AIAA | 2000


    Impulsive disturbances on car electric circuitry

    Galliano, P.G. | Tema Archive | 1977