The invention relates to an aircraft, a control system for the aircraft, and a method of controlling the aircraft. An aircraft, a method of controlling the aircraft, and a control system for the aircraft have a fuselage and a tilt wing movable relative to the fuselage. A plurality of main thrusters are coupled to the main propeller, the main propeller is coupled to the tilt wing, and the plurality of main thrusters are configured to provide a first maximum thrust force. A plurality of auxiliary thrusters are coupled to an auxiliary propeller spaced apart from the tilt wing, the plurality of auxiliary thrusters configured to provide a variable thrust force. When the tilt wing moves from the cruise position to the transition position, the controller signals the main thruster to operate at a first maximum thrust force; the controller signals the auxiliary thruster to operate at a variable thrust force when the tilted wing is in a transition position in which the first maximum thrust force and the variable thrust force together provide a total thrust to descend and land the aircraft.

    本公开涉及飞行器、用于飞行器的控制系统以及控制飞行器的方法。飞行器、控制飞行器的方法以及用于飞行器的控制系统具有机身和能够相对于机身移动的倾斜机翼。多个主推进器被耦连到主螺旋桨,该主螺旋桨被耦连到倾斜机翼,所述多个主推进器被配置为提供第一最大推力量。多个辅助推进器被耦连到与倾斜机翼间隔开的辅助螺旋桨,所述多个辅助推进器被配置为提供可变推力量。当倾斜机翼从巡航位置移动到过渡位置时,控制器向主推进器发出信号以在第一最大推力量下操作;当倾斜机翼处于过渡位置时,控制器向辅助推进器发出信号以在可变推力量下操作,在所述过渡位置中第一最大推力量和可变推力量一起提供使飞行器下降和着陆的总推力。


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    Titel :

    Aircraft, control system for aircraft and method of controlling aircraft


    Weitere Titelangaben:

    飞行器、用于飞行器的控制系统以及控制飞行器的方法


    Beteiligte:

    Erscheinungsdatum :

    2024-04-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge





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