This fourth monthly progress report again contains corrections and additions to the previously submitted reports. The additions include a simplified SRB model that is directly incorporated into the estimation algorithm and provides the required partial derivatives. The resulting partial derivatives are analytical rather than numerical as would be the case using the SOBER routines. The filter and smoother routine developments have continued. These routines are being checked out.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Space Shuttle propulsion parameter estimation using optimal estimation techniques


    Publication date :

    1983-08-20


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English