To provide an automatic control technique capable of reducing oscillations of an aircraft body when an aircraft encounters turbulence, even in the presence of a minor measurement error in forecast information.SOLUTION: An aircraft automatic control system comprises: a measurement section which measures a difference between a wind speed that an aircraft currently experiences and a wind speed that the same will experience in the future as forecast information and outputs measurement information with an estimated error in a measurement value or information to determine validity of the measurement information added to the measurement information; a ladder to control lift force, drag force or posture of the aircraft or a device to control propulsion force of the aircraft; and a control calculation section which calculates an angle of the ladder or the propulsion force to mitigate an influence of the wind speed on the aircraft body based on a wind speed value in a planned flight direction of the aircraft measured with the measurement section.SELECTED DRAWING: Figure 1

    【課題】予見情報に若干の計測誤差があったとしても、航空機が乱気流に突入した際の機体の動揺を低減させことができる自動制御技術を提供する。【解決手段】本発明の一形態に係る航空機の自動制御システムは、航空機が現に受けている風速に対して、将来遭遇する風速との差を予見情報として計測し、その計測値の推定誤差または有効・無効を判別する情報を計測情報に付加して出力する計測部と、航空機の揚力、抗力または姿勢を制御する舵、もしくは推力を制御する装置と、前記計測部で計測した航空機の飛行予定方向の風速値に基づき、前記風速が機体に及ぼす作用を減少させるような前記舵の角度または推力を算出する制御演算部とを具備する。【選択図】図1


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    Titel :

    AIRCRAFT AUTOMATIC CONTROL SYSTEM, EFFECTIVENESS EVALUATION METHOD AND MEASURING DEVICE FOR THE SAME


    Weitere Titelangaben:

    航空機の自動制御システム、その有効性評価方法およびその自動制御システム用の計測装置


    Beteiligte:
    INOKUCHI HAMAKI (Autor:in) / HAMADA YOSHIRO (Autor:in)

    Erscheinungsdatum :

    2024-03-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge




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