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
2024-02-28
Patent
Electronic Resource
English
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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