Kalman filtering and smoothing and maximum likelihood estimation techniques were applied to the problem of estimating the aircraft state in nonsteady flight from onboard noisy inertial and barometric measurements. Applied to actual flight test data, the estimation schemes yielded similar results. (Author)


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    Title :

    Estimation of the Aircraft State in Non-Steady Flight


    Contributors:

    Publication date :

    1974


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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