An aircraft and a roll method thereof. The aircraft comprises a remote control, a motor, a power supply, a controller, a six-axis inertial sensor and an H-bridge chip. The remote control is configured for a user to input a desired inclination angle of the aircraft, and transmit the desired inclination angle to the controller, the desired inclination angle being 180° or 360°. The six-axis inertial sensor is configured to detect a current real-time inclination angle of the aircraft relative to a horizontal plane, and transmit the real-time inclination angle to the controller. The controller is configured to compute a difference value between the desired inclination angle and the real-time inclination angle, and compute a roll voltage according to the difference value. The controller is further configured to control the H-bridge chip so that the roll voltage is input to the motor.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT AND ROLL METHOD THEREOF


    Beteiligte:
    TIAN YU (Autor:in) / JIANG WENYAN (Autor:in)

    Erscheinungsdatum :

    2018-02-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge



    Aircraft and roll method thereof

    TIAN YU / JIANG WENYAN | Europäisches Patentamt | 2020

    Freier Zugriff

    AIRCRAFT AND ROLL METHOD THEREOF

    TIAN YU / JIANG WENYAN | Europäisches Patentamt | 2019

    Freier Zugriff

    Alert Aircraft Roll Over Chocks

    J. M. Connolly | NTIS | 1981


    Aircraft roll steering command system

    Lambregts, Antonius A. | NTRS | 1985


    METHOD FOR ADAPTIVE ROLL CONTROL OF AIRCRAFT

    VERESHSHIKOV DMITRIJ VIKTOROVICH / KOSTIN PAVEL SERGEEVICH / VERESHSHAGIN YURIJ OLEGOVICH et al. | Europäisches Patentamt | 2016

    Freier Zugriff