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舵机加载
相关语句
  rudder loading
     Research on Extraneous Torque Compensator Based on CMAC for Electro-Hydraulic Servo Rudder Loading System
     基于小脑模型关节控制器的电液伺服舵机加载系统多余力矩补偿器研究
短句来源
     A novel extraneous torque compensator based on cerebella model articulation controller(CMAC) is proposed to solve the problem of extraneous torque,which exists in electro-hydraulic servo rudder loading system.
     针对电液伺服舵机加载系统存在多余力矩的问题,提出一种基于小脑模型关节控制器的多余力矩补偿器设计方法。
短句来源
  “舵机加载”译为未确定词的双语例句
     Research of H_∞ control in steering gear load system
     舵机加载系统H_∞控制的研究
短句来源
     There must be interrelated coupled channels when moment control system is loading to the fin servo.
     当力矩控制系统对飞行器舵机加载时,不可避免地存在着相互关联的通道(耦合)。
短句来源
     The article analysis the characteristics and effect of redundant force in steering gear load system,builds exact mathematic model,and designs a H ∞ controller of the system by treating redundant force as exoteric disturbance,Analysis and simulation results show that H ∞ controller can be effective to compensate redundant force of load system,greatly improve the performance of robust and trace,and ideally depress redundant force of steering gear load system.
     该文从理论上分析了舵机加载系统存在多余力的特点及其对加载系统控制性能的影响 ,建立了准确的数学模型 ,并将多余力作为系统的外干扰设计了舵机加载系统的H∞ 控制器。 分析与仿真结果表明 ,H∞ 控制器对补偿加载系统多余力有很好的效果 ,可以大大地提高加载系统的鲁棒性和跟踪性能 ,较理想地实现了舵机加载系统的多余力抑制
短句来源
     A new actuator loading device is proposed on the basis of analyzing the force on the rudder under flying condition.
     在分析飞行器飞行过程中舵面受力情况的基础上,提出了一种新型舵机加载装置,在舵面持续运动的情况下能够模拟和舵面运动方向相反的空气阻力矩,弥补了弹簧扭杆加载模拟空气阻力矩仅向一个方向的不足;
短句来源
  相似匹配句对
     Dynamic Loading for Missile Actuators
     导弹舵机动态加载技术
短句来源
     Research on Aircraft Rudder Motor Servo Loading System
     飞行器舵机电动伺服加载系统研究
短句来源
     Introduce the load settings.
     介绍了加载装置。
短句来源
     Analyses of the faults and maintenance of the steering gear
     舵机的故障及维护保养
短句来源
     COMPUTER AIDED TEST OF ELECTRIC ACTUATOR
     电动舵机的计算机辅助测试
短句来源
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There must be interrelated coupled channels when moment control system is loading to the fin servo. To implement the control of multivariable interelated variables, on of the primary problems which is worth studying is to aralyse how the variables are coupled, and then decoupling design can be made The coupling characteristics and a new method of decoupling for multivariable moment control systems is studied Various coupling test results

当力矩控制系统对飞行器舵机加载时,不可避免地存在着相互关联的通道(耦合)。为了对多个相关变量实现统一控制,其中一个重要且值得研究的问题是分析变量耦合情况,然后进行解耦设计。本文论述多变量力矩控制系统的耦合特性和新的解耦方法,讨论多变量力矩系统中各种耦合实验结果,并且分析耦合的物理本质,建立耦合力矩的数学模型,最后拟定五种解耦方法。

Because of inertia, time lag etc, in general the control system's output signal always falls behind its input command, and the order of the numerator is always lower than that of the denominator in transfer functions for any control system. It is inconceivable in real system that their relations are reversed(the order of numerator is that of ). B,"sureffect" arosed in the output ment command during the original loading system test The physical nature of opling moment of servo loading system has been revealed...

Because of inertia, time lag etc, in general the control system's output signal always falls behind its input command, and the order of the numerator is always lower than that of the denominator in transfer functions for any control system. It is inconceivable in real system that their relations are reversed(the order of numerator is that of ). B,"sureffect" arosed in the output ment command during the original loading system test The physical nature of opling moment of servo loading system has been revealed in this paper, and the force balance relations and the motion laws of servomechanism have been analysed. The mathematical model of the loading system is described circumstantially. The Bode diagram calculated through the transfer function is compared with the experimental data. the usefulness of the mathematical model for servo loading system and the effectiveness of the design fundamentals have been evaluated.

通常控制系统由于惯性、滞后等原因,其输出信号必然落后于输入信号.控制系统传递函数分子阶次总是低于分母阶次,把它们颠倒过来(分子阶次高于分母阶次),现实系统认为是不可能的。但是,在原型加载系统实验中,输出力矩信号却出现了“超前效性”.为了研究这个异常情况,本文揭示了舵机加载系统耦合力矩的物理本质,分析伺服机构受力平衡关系与运动规律,对系统数学模型的细节进行描述.根据传递函数计算的伯德图与实验值比较,评估该系统数学模型的有用性和基本设计原理的有效性.

The article analysis the characteristics and effect of redundant force in steering gear load system,builds exact mathematic model,and designs a H ∞ controller of the system by treating redundant force as exoteric disturbance,Analysis and simulation results show that H ∞ controller can be effective to compensate redundant force of load system,greatly improve the performance of robust and trace,and ideally depress redundant force of steering gear...

The article analysis the characteristics and effect of redundant force in steering gear load system,builds exact mathematic model,and designs a H ∞ controller of the system by treating redundant force as exoteric disturbance,Analysis and simulation results show that H ∞ controller can be effective to compensate redundant force of load system,greatly improve the performance of robust and trace,and ideally depress redundant force of steering gear load system.

该文从理论上分析了舵机加载系统存在多余力的特点及其对加载系统控制性能的影响 ,建立了准确的数学模型 ,并将多余力作为系统的外干扰设计了舵机加载系统的H∞ 控制器。分析与仿真结果表明 ,H∞ 控制器对补偿加载系统多余力有很好的效果 ,可以大大地提高加载系统的鲁棒性和跟踪性能 ,较理想地实现了舵机加载系统的多余力抑制

 
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