A system and method for controlling a deceleration profile of an aircraft, includes a processor and memory that receives a signal indicative of a deceleration command; receives signals indicative of a sensed velocity and a commanded heading rate; determines a commanded velocity in response to the receiving of the deceleration command and the commanded heading rate; determines an estimated deceleration command as a function of the commanded velocity; and determines an actual deceleration command in response to the determining of the estimated deceleration command.


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    Titel :

    DECELERATION TO HOVER MODULATION


    Beteiligte:
    KUBIK STEPHEN (Autor:in) / FAYNBERG ALEX (Autor:in) / MCCULLEY STEPHEN C (Autor:in) / RUCCI JOHN P (Autor:in) / CORRY CHRISTIAAN P (Autor:in) / PAVELKA EDWARD (Autor:in)

    Erscheinungsdatum :

    15.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    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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