The invention provides a method for controlling the horizontal translation of the rocket in a mode of not increasing the manufacturing cost and the operation cost and not changing the attitude of the rocket body, so that the landing operation of the rocket is accurately carried out. A rocket control system includes: a gimbal actuator that controls a rudder angle of a gimbal mechanism located below a gravity center of a rocket body of the rocket; the wing panel actuator is used for controlling a rudder angle of an attitude control wing positioned above the gravity center of the rocket body of the rocket; a measurement means for measuring a physical quantity related to the movement of the rocket body of the rocket; and the control unit is used for controlling the universal joint mechanism and the attitude control wings according to a measurement result of the measurement unit so as to control translation of the rocket in the horizontal direction.

    提供一种以不增大制造成本及运行成本且不改变箭体姿态的方式控制火箭在水平方向上平移的方法,从而准确地进行火箭的着陆操作。一种火箭控制系统包括:对位于所述火箭的箭体重心下方的万向节机构的舵角进行控制的万向节致动器;对位于所述火箭的箭体重心上方的姿态控制翼的舵角进行控制的翼片致动器;对与所述火箭的箭体的运动相关的物理量进行测量的测量单元;以及控制单元,该控制单元根据所述测量单元的测量结果,对所述万向节机构和所述姿态控制翼进行控制,以对所述火箭在水平方向上的平移进行控制。


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    Titel :

    Rocket control system and rocket landing action control method


    Weitere Titelangaben:

    火箭控制系统以及火箭着陆动作的控制方法


    Beteiligte:

    Erscheinungsdatum :

    2023-02-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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