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   系统动态性能 在 航空航天科学与工程 分类中 的翻译结果: 查询用时:0.178秒
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系统动态性能
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  system dynamic performance
    Based on the golden - section robust adaptive controller, a passively adapivefault - tolerant controller is designed. The controller can identify characteristic model of aplant and on - line extract system dynamic performance and fault properties. So it is able topassively tolerate some soft faults of actuators and sensors of a control system.
    在黄金分割鲁棒自适应控制器的基础上,设计了一种自适应被动容错控制器,能在线辨识对象特征模型,在线提取系统动态性能特征和故障特征,对控制系统执行机构和测量部件的某些软故障具有被动容错能力。
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    A mathematical model for the pod′s mechanical transmission system was established with MATLAB.The improvement on system dynamic performance made by the filtering network was analyzed.
    运用MATLAB软件建立了系统机械传动装置的数学模型,分析了该滤波网络对系统动态性能的改进效果。
短句来源
    Compared to the traditional filter,such filter takes care of both central resonance frequency′s impact on system dynamic performance and other resonances′ impact on system performance.
    相对于常规滤波器,该滤波网络既考虑了中心谐振频率对系统动态性能的影响,又兼顾了其他谐振点对系统性能的影响。
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  “系统动态性能”译为未确定词的双语例句
    Dymamic characteristics analysis of solid rocket motor magnetic suspension test fixture system
    固体火箭发动机磁悬浮试验架系统动态性能分析
短句来源
    In this paper, the mechanism of the liquid integrating gyro drift caused by temperature changes and the influence on the dynamic performance of a stabilized platform system are discussed detail,The numerical results of simulation are also given for reference so as to further improve the quality of the system.
    本文详细讨论了由于温度变化而引起液浮积分陀螺产生漂移的机理以及对所组成稳定平台系统动态性能的影响,并给出了仿真的数值结果,为进一步改进系统质量提供了参考。
短句来源
    Advance an automatic quantitative analysis method of failure modes and effects analysis with system transient simulation in the system design stage, take a airborne power system as a case in point. Be in use of the method, every possible failure mode of elements and devices in the system is accounted to the system transient model and system is simulated. Then simulate results of the failure states, and the cruel level of every failure mode effect is determined in numerical quantities.
    以飞机电源系统为例提出了一种在系统设计阶段,利用系统动态性能仿真模型自动进行定量故障模式影响分析的方法.该方法将系统中各个元器件可能的故障模式计入系统的动态模型中,并进行系统仿真,再将系统故障状态下的仿真结果与其正常状态下的仿真结果进行比较,以量化判定每种故障影响的严重程度,从而实现故障模式影响分析的自动化.
短句来源
    In spite of the controller simplicity, good performance including robusteness can be obtained.
    能同时考虑鲁棒性和系统动态性能要求 ,满足解耦与鲁棒性等高性能飞行控制系统的设计要求 ;
短句来源
    Calculation results indicate that control mode and controller parameters are the important factors except for the machine design parameters. The effects of controller parameters on dynamic characterisitcs of system were described by meams of computer simulation.
    表明除系统机械设计参数外,控制方式及控制器参数是影响系统动态特性的关键因素,并通过仿真说明了控制器参数对系统动态性能的影响。
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  system dynamic performance
Phasor data collected on PDC units are a primary and preferred means for obtaining a first overall view of system dynamic performance.
      


In this paper, the constituent, operation principle and regulation process of the bipropellant variable thrust rocket engine for a variable area injector that uses solenoid valve control are introduced.According to the constituent and practical operation process of usch an engine control system, the mathematical models for the main links are given, by transfer function method, the dynamic and steady-state performance is analysed, According to the calculation results, the effect on dynamic performance and steady...

In this paper, the constituent, operation principle and regulation process of the bipropellant variable thrust rocket engine for a variable area injector that uses solenoid valve control are introduced.According to the constituent and practical operation process of usch an engine control system, the mathematical models for the main links are given, by transfer function method, the dynamic and steady-state performance is analysed, According to the calculation results, the effect on dynamic performance and steady error for the engine control system is further described.

本文介绍一种用电磁阀控制的可变喷注器截面双组元变推力液体火箭发动机的组成部分、工作原理和调节过程。 根据发动机系统的组成部分和实际工作过程,建立各环节的数学模型,用传递函数法分析发动机控制系统的动态和稳态性能。通过具体的数值计算,进一步说明影响发动机控制系统动态性能和稳态误差的主要因素。

Cockpit temperature condition,is one of common and important factors which have influence on pilot's efficiency.A mathematical model of the cockpit temperature control system(CTCS)has been established on the basis of theoretical analysis and experimental data.According to the theory of automatic control the dynamic and static characteristics of CTCS have been calculated and simulated by means of an electronic computer.The effects of each parameter on the dynamic characteristics of CTCS have been studied systematically,and...

Cockpit temperature condition,is one of common and important factors which have influence on pilot's efficiency.A mathematical model of the cockpit temperature control system(CTCS)has been established on the basis of theoretical analysis and experimental data.According to the theory of automatic control the dynamic and static characteristics of CTCS have been calculated and simulated by means of an electronic computer.The effects of each parameter on the dynamic characteristics of CTCS have been studied systematically,and a quite good combination of parameters is provided.Finally,improvement of CTCS has been investigated and the results of calculation and analysis are presented.

座舱温度状态是影响飞行员工作效率的经常性和主要因素之一。我国目前研制和使用的大多数飞机,座舱温度动态性能差。本文在理论分析和试验的基础上建立了座舱温控系统的数学模型;借助电子计算机并运用自动控制理论计算和模拟了温控系统的动静态特性;系统地分析了各参数对系统动态性能的影响,并给出一组较好的参数组合;探讨了系统的改进方案并给出计算和分析结果。

In this paper, the mechanism of the liquid integrating gyro drift caused by temperature changes and the influence on the dynamic performance of a stabilized platform system are discussed detail,The numerical results of simulation are also given for reference so as to further improve the quality of the system.

本文详细讨论了由于温度变化而引起液浮积分陀螺产生漂移的机理以及对所组成稳定平台系统动态性能的影响,并给出了仿真的数值结果,为进一步改进系统质量提供了参考。

 
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