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控制器
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  controllers
    Based on them,tow controllers are designed: semi-states feedback controller and output feedback controller as well as angular velocity filters.
    在此基础上,设计了两种非全状态反馈控制器及相应的角速度滤波器:半状态反馈控制器和角速度滤波器,输出反馈控制器和滤波器,进行相对姿态控制。
短句来源
    An approach was proposed which addressed the design of output feedback H ∞controllers.
    通过利用极点配置的方法对多回路切换控制系统设计H∞输出反馈控制器
短句来源
    The PID controllers is tuned by Ziegler Nichols closed loop method and get a good simulation effect.
    采用Ziegler Nichols 方法整定PID控制器参数,得到了较好的效果。
    Sliding Mode Control Based Tracking Controllers Design for Multivariable Nonlinear Systems and Its Applications
    基于滑模控制的一类非线性多变量系统跟踪控制器设计及应用
短句来源
    A New Design and Verification Technique for Virtual Prototypes of UAV Flight Controllers
    一种UAV飞行控制器虚拟原型设计与验证新技术
短句来源
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  controller of a
    This paper applies the fuzzy control theory to solve the range control problem of point of descent in atmosphere reenty of manned spacecrafts, designs the fuzzy controller of a three input/one output system based on longitudinal error  Δ DR, transverse error  Δ CR and remaining flight time t\-\{cf\} as input variables, and the roll angle γ\-v as output variable, finally gives simulation results and the design method which is convenient for engineering application.
    将模糊控制理论应用于载人飞船再入大气层的落点航程控制问题 ,以纵程误差ΔDR、横程误差ΔCR、剩余时间tcf为输入变量 ,滚动角γv为输出变量 ,得到一个三输入单输出系统的模糊控制器并给出了便于工程应用的设计方法及仿真结果
短句来源
    This paper presents the instruction and illustration of the frequency-domain Zplan direct methodology (FZDD) for designing the digital controller of a flight vehicle digital attitude tontrol system.
    本文提出了频域Z平面直接设计方法的说明。 用于设计飞行器数字姿态控制系统数字控制器
短句来源
    This method was applied to designing the steady state controller of a two spool turbojet aeroengine with success.
    该方法被用于某型双转子涡喷航空发动机稳态控制器的设计,并取得了良好效果。
短句来源
    This method was applied to design the steady state controller of a certain double spool turbojet aero engine,and the expected results were obtained
    该方法应用于某型双转子涡喷发动机稳态控制器的设计,取得了预期的效果。
短句来源
    This method is applied to design the steady state two variable regulating controller of a non standard system——a certain double spool turbojet aero engine. And through the simulation results on aero thermodynamic model, it shows that a preferable effect is achieved.
    该方法应用于非“标准”系统——某型双转子涡喷发动机稳态双变量调节控制器的设计 ,通过在气动热力学模型上的仿真结果表明 ,取得了良好的结果
短句来源
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  s controller
    Optimized Design for Simulator's Controller Based on Hybrid Genetic Algorithm and Its Application
    基于遗传算法的仿真转台控制器优化设计与应用
短句来源
    Because H ∞ control theory is a successful and perfect theory in solving the robust problem at present,this paper studied the servo loop's controller using H ∞ control theory.
    H∞ 控制理论是目前解决鲁棒控制问题比较成功且比较完善的理论体系 ,本文利用 H∞ 控制理论 ,研究了平台稳定回路多输入多输出 ( MIMO)控制器的设计。
短句来源
    Both design and realization of the magnetic system's controller are studied in this paper based on MSBS.
    本文以磁悬挂天平为对象,重点研究磁悬挂天平悬浮控制器的设计与实现问题。
短句来源
    According to the requirement of data recording integrality, a high performance processor of ARM9 series was chosen as system’s controller and a widely used RTOS (Real-Time Operating System), VxWorks, was migrated.
    针对系统对数据记录的完整性的要求,选择了高性能的ARM9芯片作为系统的控制器,并移植了广泛应用的VxWorks实时操作系统。
短句来源
  “控制器”译为未确定词的双语例句
    Design of an Automatic Carrier Landing System Using H ∞ Synthesis
    着舰导引系统 H_∞ 控制器设计
短句来源
    The Drive System for the Plane's Wheel Based on Lingyang 061A MCU
    基于凌阳061A MCU的机轮驱动控制器
短句来源
    The Design of Rotor Speed Regulator in Helicopter
    直升机旋翼转速控制器设计
短句来源
    The system primarily proves it is feasible that we realize Link-Controller function on VxWorks.
    该系统主要验证了在VxWorks上实现链路控制器业务功能(包括包装业务、多路复用业务和位流业务等)的可行性。
短句来源
    First, a design project with the primary conroller of TMS320F2812 was determined after sufficient study.
    论文采用自顶向下的设计思想,首先研究了先进飞机电气系统,并参照已有的研究成果,确定了以TMS320F2812为主控制器的设计方案。
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  controllers
The single-input single-output (SISO) j-step-ahead predictor for generalized predictive control (GPC) controllers was traditionally derived using the polynomial approach through the Diophantine equations.
      
In the control process of nonlinear multivariable system, a decoupling controller was constructed, which took advantage of multi-nonlinear PID controllers in parallel.
      
The control strategies utilized real-time state variables obtained by PMU to linearize the state equations of the system, and then the linear optimal control strategy was used to design excitation controllers.
      
By using matrix inequalities, the existence conditions of robust H∞ static state feedback and dynamic output feedback controllers are derived.
      
Moreover, the design methods for such controllers are provided in terms of the solutions of matrix inequalities.
      
更多          
  controller of a
A Method of Successive Improvement in the Design of the Controller of a Linear Discrete Plant
      
Furthermore, it is possible to design an online controller of a SOFC stack based on this GA-RBF neural network identification model.
      
The design of the controller of a two-wheeled mobile robot is usually based on a kinematical model.
      
Although the system has static stability, manipulation on the moving base or mobile locomotion with a manipulator may cause the system to turn over due to dynamics, so the controller of a mobile manipulator is carefully designed.
      
Given a linear full state feedback controller (of a certain form) which stabilizes the system in the absence of control constraints, we then determine sufficient conditions under which the system with constrained control remains stable.
      
更多          
  s controller
In respect to the rate-based speciality, a periodical input is considered as the system's controller.
      
Yamakawa's controller featured two types of chips of his own design.
      
You can not use vendor A's software to program vendor B's controller.
      
According to Mott's controller Jack DeVito, the value of CRM begins with the processes.
      
A blank billet is routed to the machine while the program to create the mold is downloaded to the machine's controller.
      
更多          


In this paper,eight methods in terrein-following ( n method,template method,adaptive angle method,close-loop lift acceleration method,projected slope method,altimeter method,curve fitting method and optimal controller method ) are introduced.The basic ideas,the mathematical models,the principles of operation,the advantages and disadvantages of these methods are described.

本文介绍了地形跟随的八种方法(n方法,样板法,适应角法,闭环升力加速度法,投影坡度法,高度表法,曲线拟合法,最优控制器法),说明了这些方法的基本思想、数学模型,运行原理和优缺点。

In this paper, a design procedure for an attitude control systemconsisting of four skewed reaction wheels is investigated. The attitudedynamics of the satellite is described by a controllable and observablelinear, time-invariant system. State feedback is used in the control, withthe state reconstructed by a minimal dimension observer. Control law isgiven by minimizing a quadratic criterion function. The concepts of "normalcontrol" law and "failed control" law of skewed reaction wheels isintroduced. It is shown...

In this paper, a design procedure for an attitude control systemconsisting of four skewed reaction wheels is investigated. The attitudedynamics of the satellite is described by a controllable and observablelinear, time-invariant system. State feedback is used in the control, withthe state reconstructed by a minimal dimension observer. Control law isgiven by minimizing a quadratic criterion function. The concepts of "normalcontrol" law and "failed control" law of skewed reaction wheels isintroduced. It is shown that combination of correct distribution of torquecommands can be done using a simple network of distribution. The influenceof a flexible solar cell plate on the control law of skewed reaction wheelsis discussed. Analytical results are verified by computer simulation.

本文研究了采用斜装反作用飞轮阵的卫星姿态控制系统。文中引入了正常控制律和失效控制律的概念,并论证了斜装反作用飞轮阵的力矩指令的分配计算,可设计简单的分配网络实现。控制器的设计采用了多变量系统理论,并对设计结果进行了数字模拟。最后,讨论了卫星所带的太阳帆板动力学对斜装飞轮阵控制律的影响。

The development, communication standards, system structures, operating principles of airborne multiplex data bus and its sphere of application are discussed in this paper. A method using a microcomputer to design the intelligent terminal and bus controller of the system is described with emphasis on hardware and software design.The major problems about high speed, real-time and secure transmission of data between computer and its interface are reviewed. The intelligent terminal and bus controller have been developed...

The development, communication standards, system structures, operating principles of airborne multiplex data bus and its sphere of application are discussed in this paper. A method using a microcomputer to design the intelligent terminal and bus controller of the system is described with emphasis on hardware and software design.The major problems about high speed, real-time and secure transmission of data between computer and its interface are reviewed. The intelligent terminal and bus controller have been developed by means of 8086 computer. An experimental prototype has been made and its job programs debugged.The optical fiber data bus system consists of optical receivers, optical transmitters, an optical couple with eight ports, the bus controller and the intelligent terminal. Some of checkout tests have been completed at code rate of 1 Mbit/s with this system.The optic fiber transmission system are also considered and some experimental results are given.

本文讨论机载数据总线的发展、应用、通讯协议、系统结构。文中着重讨论总线控制器和远程终端的硬件设计、软件设计及光导纤维传输系统的设计,还列举了一些实验情况及结果。

 
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