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SERVO CONTROL SYSTEM FOR RUDDER OF AIR PLANE

机译:飞机舵机伺服控制系统

摘要

PROBLEM TO BE SOLVED: To provide a controller, which can always obtain the stabilized control characteristic even in the case where the natural frequency of an object to be controlled is fluctuated in a certain range and of which installation is facilitated. ;SOLUTION: In this system, operation of a rudder of an air plane to be operated by an actuator is controlled by a controller 10 provided with a compensating unit 14 for outputting the operated variable so that a target value and a controlled variable of the rudder coincide with each other. The actuator and the rudder are regulated as an object to be controlled, which generate the fluctuation of' the natural frequency, and this system is also provided with a means a for treating the fluctuation of the object to be controlled in a predetermined range, which includes the natural frequency thereof, as the fluctuation of parameter of the equivalent mass and the rigidity of the rudder, and provided with a linear compensating unit 14 designed by the robust control method so as to obtain the robust stability even in the case where the object to be controlled is fluctuated within the predetermined range.;COPYRIGHT: (C)1997,JPO
机译:解决的问题:提供一种即使在被控制物的固有频率在一定范围内变动且易于安装的情况下,也能够始终获得稳定的控制特性的控制器。 ;解决方案:在该系统中,由致动器操作的飞机舵的操作由控制器10控制,该控制器设有补偿单元14,用于输出操作变量,从而使舵的目标值和受控变量彼此重合。致动器和舵被调节为要被控制的对象,其产生固有频率的波动,并且该系统还设有用于在预定范围内处理被控制的对象的波动的装置。包括其固有频率,作为等效质量的参数波动和舵的刚度,并且设有通过鲁棒控制方法设计的线性补偿单元14,从而即使在目标物体的情况下也可以获得鲁棒稳定性。 COPYRIGHT:(C)1997,JPO

著录项

  • 公开/公告号JPH09136698A

    专利类型

  • 公开/公告日1997-05-27

    原文格式PDF

  • 申请/专利权人 KAYABA IND CO LTD;

    申请/专利号JP19950298458

  • 发明设计人 SATO KOSUKE;MIKAMI TAKESHI;

    申请日1995-11-16

  • 分类号B64C13/00;G05B13/02;

  • 国家 JP

  • 入库时间 2022-08-22 03:35:02

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