Aircraft indication systems and processes for calculating an engine-out return altitude for an aircraft are described. In implementations, an aircraft indication system comprises a memory operable to store one or more modules and a processor coupled to the memory. The processor is operable to execute the one or more modules to cause the processor to: identify a takeoff event associated with the aircraft; access dynamic aircraft performance data including at least a current altitude of the aircraft; calculate an engine-out return altitude for the aircraft; and provide a return altitude indication to a pilot of the aircraft using the calculated engine-out return altitude.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    IMPOSSIBLE TURN INDICATION SYSTEM


    Beteiligte:

    Erscheinungsdatum :

    29.10.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS



    Possible "Impossible" Turn

    Rogers, D.F. | Online Contents | 1995


    Possible 'impossible' turn

    Rogers, David F. | AIAA | 1995


    Analyzing the Impossible Turn

    Melnyk, Richard / Osmon, Michael / Robinson, Dylan et al. | AIAA | 2024


    The Possible `Impossible' Turn

    Rogers, D. F. / AIAA | British Library Conference Proceedings | 1994


    The possible 'impossible' turn

    Rogers, David | AIAA | 1994