The problem of designing fine-pointing controllers is considered for large, flexible space structures using modern multivariable synthesis methods. The first method is an iterative procedure which utilizes frequency-domain singular-value techniques, and is found to yield satisfactory performance and robustness. For the second method, which is based on coprime factorizations, a particular bicoprime is obtained, and the steps in the design process are described. This method is still under development.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Controller synthesis for flexible spacecraft using multivariable loop-shaping and factorization methods


    Additional title:

    Reglersynthese fuer ein flexibles Raumfahrzeug mit Hilfe der Mehrgroessenregelung und des Faktorisierungsverfahrens


    Contributors:
    Joshi, S.M. (author)


    Publication date :

    1987


    Size :

    2 Seiten, 6 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Flight controller design using multivariable loop shaping

    Hyde, R. A. / Glover, K. / Institute of Mathematics and its Applications et al. | British Library Conference Proceedings | 1994


    Multivariable Aircraft Engine Controller Design Using an Optimal Loop Shaping Approach

    Adade Filho, Alberto / Silva, Douglas F R / Barbosa, Joao | SAE Technical Papers | 2011



    Slewing Flexible Spacecraft with Deflection-Limiting Input Shaping

    William E. Singhose / Arun K. Banerjee / Warren P. Seering | AIAA | 1997