A Flight Safety System requires high reliability in its operation because of the crucial duty to decide to destroy a flying vehicle or not, etc., in a state of emergency. A new Flight Safety System, one totally independent of the old one, which depends on radar information, is based on the principle of inertial navigation in calculating a real-time trajectory and impact points on earth by online PCM-telemetry data. This backup system has been applied to practical missions such as Halley and Ginga, with good success. An efficient, redundant system was created by connecting an ordinary personal computer to the line for speedy calculation in order to construct a transfer matrix for a single pole representation of altitude.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Development of New Redundant Flight Safety System Using Inertial Sensors


    Beteiligte:
    S. Tsukamoto (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Nonorthogonal redundant configurations of inertial sensors

    Sushchenko, O. A. / Bezkorovainyi, Y. N. / Novytska, N. D. | IEEE | 2017


    FDI using Multiple Parity Vectors for Redundant Inertial Sensors

    Yang, C.-K. / Shim, D.-S. | British Library Online Contents | 2006