A system and related methods for providing stall recovery guidance symbology via a head-up display (HUD) or similar avionics display element detects stall or near-stall conditions and provides symbology to guide the pilot through recovering from the stall by prioritizing pitch correction and disengagement of the autopilot system. Pitch correction symbology guides the pilot toward reducing the aircraft angle of attack and establishing level flight, while thrust recovery symbology helps the pilot control the application of thrust to avoid prolonging or reinstituting the stall. The system modifies the stall recovery symbology in response to detected changes in pitch, angle of attack, or airspeed. Once level flight has been established and stall conditions are no longer present, the system may transition out of stall recovery mode to regular inflight symbology.


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    Titel :

    Head-Up Display (HUD) Stall Recovery Symbology


    Beteiligte:
    NOICE LENARD E (Autor:in)

    Erscheinungsdatum :

    2018-01-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / G09G Anordnungen oder Schaltungen zur Steuerung oder Regelung von Anzeigevorrichtungen mit statischen Mitteln zur Darstellung veränderlicher Informationen , ARRANGEMENTS OR CIRCUITS FOR CONTROL OF INDICATING DEVICES USING STATIC MEANS TO PRESENT VARIABLE INFORMATION



    Head-up display (HUD) stall recovery symbology

    NOICE LENARD E | Europäisches Patentamt | 2018

    Freier Zugriff

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    Reising, J. / Zenyuh, J. / Barthelemy, K. | Tema Archiv | 1988


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    Chandra, D. / Weintraub, D. J. | British Library Conference Proceedings | 1994


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    REID ALEXANDER D / KIRCHNER WILLIAM T / BOGGS CHRISTOPHER M et al. | Europäisches Patentamt | 2023

    Freier Zugriff