A device for revising a low-altitude flight phase of a flight path of an aircraft includes an input unit configured to allow an operator to input parameters to define an intermediate flight section (Si) which has to be inserted into a low-altitude flight phase, and a processing unit configured to calculate a profile relating to the intermediate flight section (Si) using input parameters, and to automatically insert this profile into the flight phase between a first upstream part (P1) and a second downstream part (P2) so as to establish a revised flight phase (PR).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Method and device for revising a low-altitude flight phase of a flight path of an aircraft


    Beteiligte:
    KOEBEL THOMAS (Autor:in) / ALBERT NICOLAS (Autor:in)

    Erscheinungsdatum :

    15.03.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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





    METHOD FOR UNMANNED AERIAL VEHICLE FLIGHT TO ALTITUDE FLIGHT PATH

    MISHCHENKO ANATOLIJ PETROVICH / PLOKHIKH DMITRIJ SERGEEVICH / CHERNOV LEONID ALEKSANDROVICH | Europäisches Patentamt | 2020

    Freier Zugriff

    Flight Path Optimization at Constant Altitude

    Ardema, M.D. / Asuncion, B.C. | British Library Conference Proceedings | 2009