Technologically improved flight guidance systems and methods that generate thrust guidance related to a potential flight path angle are provided. The thrust guidance is provided as acceleration commands that may be communicated to the pilot in an intuitive manner, such as with an acceleration cue on a primary flight display (PFD) system. The provided acceleration cues are uniform across the flight envelope and present consistently for two basic thrust guidance modes.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    SYSTEMS AND METHODS FOR PROVIDING THRUST GUIDANCE RELATED TO FLIGHT PATH ANGLE


    Beteiligte:
    MELENDEZ LUIS (Autor:in) / SIN PHILIP (Autor:in) / KOENIG JOHN (Autor:in) / MAST MICHAEL (Autor:in)

    Erscheinungsdatum :

    04.03.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS



    SYSTEMS AND METHODS FOR PROVIDING THRUST GUIDANCE RELATED TO FLIGHT PATH ANGLE

    MELENDEZ LUIS / SIN PHILIP / KOENIG JOHN et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Systems and methods for providing thrust guidance related to flight path angle

    MELENDEZ LUIS / SIN PHILIP / KOENIG JOHN et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Flight-Path Angle Control for Cutoff Insensitive Guidance

    Kim, Sang-Jae / Um, Tae-Yoon | AIAA | 2015


    SYSTEMS AND METHODS FOR ENERGY MANAGED AUTOFLIGHT GUIDANCE USING POTENTIAL FLIGHT PATH ANGLE

    MELENDEZ LUIS / SIN PHILIP / KOENIG JOHN | Europäisches Patentamt | 2021

    Freier Zugriff