Optimum linear filter and control theory is applied to practical problem of supplementing inertial navigation system with discrete reference information; information takes form of position obtained from Loran C or Decca, for example, and occasional azimuth fixes obtained from star sightings; optimum use of this information is discussed for Ship's Inertial Navigation System (SINS) installations intended for missile carrying submarines and warships; interpretation of optimum control dictated in part by augmented SINS model is discussed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Optimum reset of ships inertial navigation system


    Weitere Titelangaben:

    IEEE -- Trans Aerospace Electronic Systems


    Beteiligte:
    Bona, B.E. (Autor:in) / Smay, R.J. (Autor:in)


    Erscheinungsdatum :

    1966


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Optimum Reset of Ship's Inertial Navigation System

    B. E. Bona / R. J. Smay | NTIS | 1965


    Optimum Reset of Ship's Inertial Navigation System

    Bona, B. E. / Smay, Robert J. | IEEE | 1966



    Inertial navigation system

    HENDERSON GEOFFREY THOMAS | Europäisches Patentamt | 2023

    Freier Zugriff

    INERTIAL NAVIGATION SYSTEM

    JOHN KEITH SHEARD / NICHOLAS MARK FAULKNER | Europäisches Patentamt | 2017

    Freier Zugriff