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.
AIRCRAFT CONTROL SYSTEM, AIRCRAFT, AIRCRAFT CONTROL METHOD, AND PROGRAM
FLUGZEUGSTEUERUNGSSYSTEM, FLUGZEUG, FLUGZEUGSTEUERUNGSVERFAHREN UND PROGRAMM
SYSTÈME DE COMMANDE D'AÉRONEF, AÉRONEF, PROCÉDÉ DE COMMANDE D'AÉRONEF, ET PROGRAMME
28.02.2024
Patent
Elektronische Ressource
Englisch
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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