The automatic piloting system includes an element for automatically supplying a computation unit, when the aircraft is guided according to a descending corrected speed and a new corrected speed which is greater than the corrected speed used for guidance of the aircraft is input by the pilot, with a predetermined maximum Mach number which replaces the current Mach number and which is intended to form, together with the new input corrected speed, a pair of speeds which is taken into account by the computation unit for determining the guidance instructions for the aircraft.


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    Title :

    Automatic piloting method and system for an aircraft


    Contributors:

    Publication date :

    2015-06-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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