A yaw control system for a rotorcraft featuring a floor mounted pair of pedals configured to measure an up and down motion of a pair of pedals and utilize that up and down motion as a yaw moment control input. The pair of pedals can rock laterally, fore and aft, or vertically. The pair of pedals can be mechanically interconnected to other pairs of pedals or electrically interconnected to duplicate motion across pairs of pedals.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ALTERNATIVE YAW CONTROL


    Beteiligte:

    Erscheinungsdatum :

    30.07.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    ALTERNATIVE CONTROL DEVICE, ALTERNATIVE CONTROL METHOD, ALTERNATIVE CONTROL PROGRAM, AND FAIL-OPERATIONAL SYSTEM

    YAMAMOTO HITOSHI / KONAKA HIROKI | Europäisches Patentamt | 2020

    Freier Zugriff

    Alternative yaw control

    LAVALLEE YANN / SINUSAS ERIC ALBERT / WARDLAW ROBERT PATRICK | Europäisches Patentamt | 2022

    Freier Zugriff

    Alternative control technologies

    Hudgins, Bernard | TIBKAT | 1998


    Alternative Model Reference Adaptive Control

    Lavretsky, E. / Levin, J. / Gadient, R. et al. | British Library Conference Proceedings | 2010


    Containerized alternative fuel control unit

    COLDREN DANA RAY / NELSON BRYAN E / KIM HOISAN | Europäisches Patentamt | 2025

    Freier Zugriff