the INS systems, from the first realizations on, have enjoyed a strong push to miniaturization. On the one hand, this has made them less prone to various mechanical-electrical problems and therefore reduced many of the errors due to technology. On the other hand, the intrinsic errors due to the inseparable error of the instrument remains. This paper examines a simple methodology for filtering and deleting the propagation errors of the INS systems. Most of the errors that can be mathematically compensated through an appropriate series of Kalman’s filters


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Inertial Navigation Systems for UAV: Uncertainty and Error Measurements


    Contributors:


    Publication date :

    2019-06-01


    Size :

    1130165 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Inertial navigation system error models

    Widnall, William S. / Grundy, Peter A. | TIBKAT | 1973


    Error equations of inertial navigation

    ARSHAL, GEORGE | AIAA | 1987



    Error Analysis of Space-Stable Inertial Navigation Systems

    Nash, Raymond A. / Levine, Stephen A. / Roy, Kenneth J. | IEEE | 1971