An aircraft control system includes a target instruction value calculation unit that acquires a target instruction value to set an aircraft in a target state, a reference velocity calculation unit that inputs, to a reference model in which reference velocity corresponding to a reference value of aircraft velocity is set uniquely as an output value in accordance with an input value, a value based on the target instruction value as the input value, thereby calculating the reference velocity, a relative velocity calculation unit that calculates relative velocity of the aircraft to a target position, the relative velocity being used in control of the aircraft, an estimated disturbance quantity calculation unit that calculates an estimated disturbance quantity acting on the aircraft, based on a difference between the relative velocity and the reference velocity, and a correction target instruction value calculation unit that corrects the target instruction value, based on the estimated disturbance quantity calculated at a previous timing.


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    Title :

    AIRCRAFT CONTROL SYSTEM, AIRCRAFT, AIRCRAFT CONTROL METHOD, AND PROGRAM


    Additional title:

    FLUGZEUGSTEUERUNGSSYSTEM, FLUGZEUG, FLUGZEUGSTEUERUNGSVERFAHREN UND PROGRAMM
    SYSTÈME DE COMMANDE D'AÉRONEF, AÉRONEF, PROCÉDÉ DE COMMANDE D'AÉRONEF, ET PROGRAMME


    Contributors:
    KOJIMA TORU (author) / MORI SATOSHI (author)

    Publication date :

    2024-02-28


    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 / B64C AEROPLANES , Flugzeuge / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS



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