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控制器设计     
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  controller design
    MAV Flight Controller Design Approach Based on Multidisciplinary Synthesis and Optimization
    基于多学科综合与优化的MAV飞行控制器设计方法研究
短句来源
    Robust Controller Design for Airplane and Research on Stability Margins
    飞机鲁棒控制器设计及稳定裕度研究
短句来源
    AN AEROENGINE H ∞ CONTROLLER DESIGN METHOD
    航空发动机H_∞控制器设计方法
短句来源
    ROBUST CONTROLLER DESIGN FOR SELF-REPAIRING FLIGHT CONTROL SYSTEM
    自修复飞控系统的鲁棒控制器设计
短句来源
    A Controller Design Method for Carrier Rocket with Integrity to Sensor Failures
    对传感器失效具有完整性的运载火箭控制器设计
短句来源
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  design of controller
    Based on these analyses, quantitative comparison between constrained and unconstrained mode frequency with different flexible/rigid body inertia is made. The theoretical basis for modeling and design of controller of such flexible system is provided.
    在此基础上定量分析了约束模态和非约束模态的频率随不同挠性梁 /中心刚体惯量比的不同近似程度 ,为动力学建模和控制器设计提供了理论依据
短句来源
  control design
    ON THE INTEGRATED ANALYSIS OF OPTIMUM CONTROL DESIGN IN INTELLIGENT STRUCTURE SUBJECTED TO CONSTRAINT OF STRUCTURE OPTIMIZATION
    智能结构动力系统控制器设计和结构优化的综合分析
短句来源
    Output Tracking Control Design of Subminiature Rotorcraft
    超小型旋翼机系统的输出跟踪控制器设计
短句来源
    The flight control system is designed for one model of advanced aircraft by using nonlinear H ∞ control design algorithms without the DGKF simplifying conditions.
    应用无 DGKF简化条件的非线性 H∞ 控制器设计方法 ,为某型飞机设计了非线性 H∞ 飞行控制系统。
短句来源
    A new vibration control design method based on FEM(finite element method) was proposed for structures to avoid the model error due to simplification and model reduction,in order to solve the difficulty of complex structures modeling and to improve the accuracy of the control design.
    为了避免在建立结构数学模型过程中因简化和降阶引起的模型误差,解决复杂结构建模难的问题,提高控制器设计的准确性,提出了一种新的基于有限元法(FEM)的结构振动控制设计方法.
短句来源
    Employing the above design method, the decoupling flight control system of UH 60A helicopter is designed for attitude command attitude hold (ACAH) response type. The simulation results show that the validity of the decoupling control design method with too fast mode of controller being limited.
    通过对 UH-6 0直升机的“姿态命令 /姿态保持”响应模式的解耦飞行控制器设计 ,验证了 H∞ 控制理论对直升机解耦控制 ,以及所提解决控制器运动模态过快方案的有效性。
短句来源
  attitude controller
    A Method for Designing Helicopter Attitude Controller Based on Fuzzy Control
    一种基于模糊控制的直升机姿态控制器设计方法
短句来源
    Roll/Yaw Attitude Controller Design of Biased Momentum Satellite Based on Roll Information Feedback
    基于滚动信息反馈的偏置动量卫星滚动/偏航回路姿态控制器设计
短句来源
    Design and Simulation of Spacecraft Attitude Controller
    空间飞行器姿态控制器设计与仿真
短句来源

 

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      controller design
    Decentralized adaptive robust controller design for complex system based on partition of unity
          
    Delay-dependent robust H∞ controller design for a class of nonlinear uncertainty time-delay systems with input delay
          
    Based on a linearized TCP/AQMmodel, a new proportional integral (PI) controller design approach is proposed.
          
    The results show the advantages of the new PI controller design approach for AQM routers supporting TCP flows.
          
    The controller design does not need an accurate model of the robot manipulator.
          
    更多          
      design of controller
    Sequential design of controller for parallel dc/dc converters via Gauss-Jordan factorization: Nyquist approach
          
    In the design of controller all the inputs and outputs are presented in the form of voltage signals.
          
    In this paper we present the hardware design and design of controller for mobile manipulator and a design of transport mobile robot behaviour.
          
    On the other hand, the unknown sign of virtual control gain function leads to great trouble in the design of controller.
          
      control design
    Finally, the image-based control design of combined multivariable symmetric cascade system and its results were given.
          
    Control design for a class of linear 0-controllable discrete systems with constraints
          
    Control design for a class of linear 0-controllable discrete systems with constraints
          
    The joint control design strategy is the construction of minimizing sequences, which converge in intervals by stationarity to the optimal process of the initial problem.
          
    Considered is the control design problem for planar motion of a wheeled robot.
          
    更多          
      attitude controller
    A neural network based attitude controller of a satellite with deployable solar arrays was developed.
          
    To validate an ANN attitude controller, the dynamics and kinematics of a given satellite was simulated in computer.
          
    The longitudinal position and velocity controllers command a desired pitch angle s to the longitudinal attitude controller.
          


    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。

    Simplification of the mathematical model for a marine gas turbine propulsion system is studied by modal analysis,and selection of remained state variables in the order-reduced model

    木文结合航机改装的舰用燃气轮机系统,在较详细的高阶非线性模型的基础上进行了系统的模态分析和灵敏度分析,进而探讨了燃气轮机作为控制对象时反馈变量的选择和高阶模型的简化方法。这方法为这类系统的控制器设计时数学模型的处理提供了有价值的参考。

    A design method of"Linear Quadratic Output PI Feedback Control" is proposed in this paper. Amarine gas turbine propulsion system controller has been designed by use of this method. The controller not only has the advantages of the PI controller in classical control theory, but also those of the state-variable feedback in modern control theory. The simulation of this controller gives satisfactory results.

    本文利用舰用燃气轮机推进系统的简化模型及部分状态反馈进行最优控制器的设计。文中提出一种线性二次型PI控制,和一般二次型控制不同之处在于,它既能消除静态偏差,又能使系统整体最优。

     
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