An aerial vehicle comprising an airframe, an aircraft flight controller to provide an output control signal, and a planar printed circuit board positioned on the airframe. The printed circuit board may include coupled thereto a processor, a rate gyroscope, and at least three accelerometers. The processor is configured to generate an actuation signal based at least in part on a feedback signal received from at least one of said rate gyroscope and the at least three accelerometers. The processor communicates the actuation signal to said aircraft flight controller, which is configured to adjust the output control signal based on said actuation signal.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Distributed Acceleration Sensing for Robust Disturbance Rejection


    Beteiligte:
    GRIFFIN RILEY (Autor:in) / SCOTT EDWARD (Autor:in) / HUMBERT SEAN (Autor:in)

    Erscheinungsdatum :

    2018-05-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G01B MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS , Messen der Länge, der Dicke oder ähnlicher linearer Abmessungen / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



    Distributed acceleration sensing for robust disturbance rejection

    GRIFFIN RILEY / SCOTT EDWARD / HUMBERT SEAN | Europäisches Patentamt | 2021

    Freier Zugriff

    DISTRIBUTED ACCELERATION SENSING FOR ROBUST DISTURBANCE REJECTION

    GRIFFIN RILEY / SCOTT EDWARD / HUMBERT SEAN | Europäisches Patentamt | 2020

    Freier Zugriff

    DISTRIBUTED ACCELERATION SENSING FOR ROBUST DISTURBANCE REJECTION

    GRIFFIN RILEY / SCOTT EDWARD / HUMBERT SEAN | Europäisches Patentamt | 2018

    Freier Zugriff

    Disturbance Rejection with Distributed Acceleration and Strain Sensing

    Gremillion, Gregory M. / Castano, Lina / Humbert, James | AIAA | 2015