The research during the second reporting period has focused on robust control design for hypersonic vehicles. An already existing design for the Hypersonic Winged-Cone Configuration has been enhanced. Uncertainty models for the effects of propulsion system perturbations due to angle of attack variations, structural vibrations, and uncertainty in control effectiveness were developed. Using H(sub infinity) and mu-synthesis techniques, various control designs were performed in order to investigate the impact of these effects on achievable robust performance.


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    Title :

    Research in Robust Control for Hypersonic Aircraft


    Contributors:

    Publication date :

    1993


    Size :

    24 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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