To quickly restore a rapid change in an attitude caused by a disturbance of a flying object.SOLUTION: An attitude control device is installed on a flying object 30 that generates thrust according to a controlled amount. The attitude control device comprises: a movable unit 330 that can move against an airframe of the flying object 300; drive means 130 for moving the movable unit; and control means 110, 150, 160 that output a control amount so as to return the airframe to the original attitude thereof when the attitude of the airframe changes, and controls the drive means to move the movable unit in a direction of returning the attitude to the original position.SELECTED DRAWING: Figure 1

    【課題】飛行体の外乱による急な姿勢変化を速やかに元に戻す。【解決手段】姿勢制御装置は、制御量に応じた推力を発生する飛行体30に設けられる。姿勢制御装置は、飛行体の機体300に対して移動可能な可動部330と、可動部を移動させる駆動手段130と、機体の姿勢が変化した際に、該姿勢を元に戻すための制御量を出力するとともに、姿勢を元に戻す方向に可動部を移動させるように駆動手段を制御する制御手段110、150、160とを有する。【選択図】図1


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    Title :

    ATTITUDE CONTROL DEVICE, FLYING OBJECT AND ATTITUDE CONTROL METHOD


    Additional title:

    姿勢制御装置、飛行体および姿勢制御方法


    Contributors:

    Publication date :

    2024-01-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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