Present novel and non-trivial system, device, and method for generating an aircraft energy indicator(s) is disclosed. The energy indicator generating system is comprised of one or more sources of aircraft performance factors data, an image generator (IG), and a presentation system. The IG may be configured to receive the aircraft performance factors data representative of at least aircraft altitude and speed; determine descent path data as a function of at least the aircraft performance data; determine target aircraft energy data as a function of at least the descent path data; determine actual energy data as a function of at least the aircraft performance data; and generate presentation data as a function of the target energy data and the actual energy data, where the presentation data is representative of one or more images of an aircraft energy indicator presentable to a viewer.


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    Title :

    Aircraft energy indicator generating system, device, and method


    Contributors:

    Publication date :

    2017-11-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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