The design of a robust and fault-tolerant control system for the attitude control of a satellite launch vehicle is described. The robust controller is designed for the nominal system in order to reduce the effect of disturbances in the system. Finally, a reconfigured controller is designed to stabilise the system by placing the closed-loop poles within a desired region and also to guarantee the disturbance attenuation below a certain level. The linear matrix inequality technique is used to design the controllers. The performance of the nominal and reconfigured controller is presented.


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    Title :

    Robust and fault tolerant controller for attitude control of a satellite launch vehicle


    Contributors:
    Das, R.K. (author) / Sen, S. (author) / DasGupta, S. (author)

    Published in:

    Publication date :

    2007


    Size :

    9 Seiten, 29 Quellen




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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