A real-time compensation system of a projectile includes at least one flight controller, at least one imager device, at least one gyroscope, and at least one processor. The at least one flight controller is configured to rotate the projectile about an axis between a first orientation and a second orientation. The at least one imager device is configured to capture a first image at the first orientation and a second image at the second orientation. The at least one gyroscope is configured to sense a first angular rate of the projectile as the projectile rotates from the first orientation to the second orientation. The at least one processor is configured to determine a first rotation angle based upon the first and second images and a second rotation angle based upon the angular rate sensed by the at least one gyroscope, and determine a gyroscope compensation parameter.


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    Titel :

    REAL-TIME COMPENSATION OF INERTIAL GYROSCOPES


    Weitere Titelangaben:

    ECHTZEITKOMPENSIERUNG VON TRÄGHEITSGYROSKOPEN
    COMPENSATION EN TEMPS RÉEL DE GYROSCOPES INERTIELS


    Beteiligte:
    ELLIS DAVID (Autor:in) / ELL TODD (Autor:in)

    Erscheinungsdatum :

    28.04.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen



    Real-time compensation of inertial gyroscopes

    ELLIS DAVID / ELL TODD ANTHONY | Europäisches Patentamt | 2020

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