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反作用飞轮    
相关语句
  reaction wheel
    The Combined Control Algorithm for Magnetorquer and Reaction Wheel of Small Satellite
    小卫星磁力矩器与反作用飞轮联合控制算法研究
短句来源
    The Design of Torque Mode Control for Reaction Wheel System
    反作用飞轮力矩模式控制系统设计
短句来源
    The Reaction Wheel Control Mode in the Azimuth Control of Nacelle System
    高空气球吊篮方位控制系统的反作用飞轮控制模式
短句来源
    Design and Application of Reaction Wheel Elec-Simulator Device
    反作用飞轮电模拟器设计与应用
短句来源
    Optimization Design of Magnetic Bearing Reaction Wheel Rotor
    50Nms磁悬浮反作用飞轮转子优化设计方法的研究
短句来源
更多       
  reaction wheel
    The Combined Control Algorithm for Magnetorquer and Reaction Wheel of Small Satellite
    小卫星磁力矩器与反作用飞轮联合控制算法研究
短句来源
    The Design of Torque Mode Control for Reaction Wheel System
    反作用飞轮力矩模式控制系统设计
短句来源
    The Reaction Wheel Control Mode in the Azimuth Control of Nacelle System
    高空气球吊篮方位控制系统的反作用飞轮控制模式
短句来源
    Design and Application of Reaction Wheel Elec-Simulator Device
    反作用飞轮电模拟器设计与应用
短句来源
    Optimization Design of Magnetic Bearing Reaction Wheel Rotor
    50Nms磁悬浮反作用飞轮转子优化设计方法的研究
短句来源
更多       
  reaction flywheel
    The nacelle azimuth control of DC torque motor under the reaction flywheel control mode is presented,and the nacelle azimuth control syst em is investigated in theory.
    提出了用直流力矩电动机在反作用飞轮控制方式下对气球吊篮的方位控制,从理论上研究了气球吊篮方位控制系统。
短句来源
    The controller using reaction flywheel on the SABGT is designed and then computer simulation is obtained.
    用反作用飞轮作为控制执行机构,设计了控制器,进行了相关的计算机仿真。
短句来源
    A dynamic nacelle azimuth control is realized. Its c ontrol performance and quality are enhanced under the reaction flywheel control. High precision and reliability was obtained.
    该系统实现了气球吊篮方位的动态控制,提升了反作用飞轮控制方式的控制特性和系统的控制品质,提高了系统的精度和可靠性。
短句来源
    A reliable nacelle decoupling mechanism control effect can be achieved while using the embedded computer PC/104 actualized closed loop control system. It also obtained a continuous control,high precision and reliability when combining with reaction flywheel control system.
    系统选用PC/104嵌入式计算机对整个系统进行闭环控制,可靠实现了对气球吊篮的解捻,并能和吊篮反作用飞轮控制系统有效结合,实现气球吊篮姿态控制的连续性,提高了吊篮姿态的控制精度和可靠性。
短句来源
    This paper introduced the structure of a permanent magnet bias magnetic bearing reaction flywheel for stabilization of spacecraft attitude. Its rotation speed is from-5000rpm to 5000rpm(rating angular momentum is 50Nms).
    介绍了一种额定工作转速为-5000rpm~5000rpm,额定角动量为50Nms的五自由度磁悬浮反作用飞轮
短句来源
  reaction wheels
    Deign of Skewed Reaction Wheels Controller for Three--Axis Stabilized Satellite
    三轴稳定卫星斜装反作用飞轮控制器设计
短句来源
    The simulation proved that the Instrument-in-Loop method can greatly improve the precision of attitude determination with low cost. The small astronomical satellite has demands on both pointing accuracy and attitude maneuverability, so this thesis modeled the attitude control subsystem based on reaction wheels.
    2)SVOM卫星同时对指向精度和姿态机动性有着很高的要求,因此本文建立了基于反作用飞轮的SVOM卫星姿态控制系统模型,在高精度惯性定向三轴稳定模式下分别设计了PD控制律和变结构控制律,通过仿真验证了变结构控制对于SVOM卫星的有效性,并基于变结构控制研究了SVOM卫星快速大角度机动的方法。
短句来源
    The quaternion feedback control laws was studied for the three-axis stabilization control using reaction wheels, a design method for the PID controller parameters was presented and the simulation results indicated that the control algorithm works efficiently.
    针对以反作用飞轮作为执行机构的三轴稳定控制情形,研究了四元数反馈控制算法,给出PID控制器参数的设计,仿真结果验证了控制器设计是合理的。
短句来源
    The time-optimal control law for motor torques of reaction wheels is designed, and, the calculated formulations of maneuver time and system state are given.
    进一步的设计了反作用飞轮电机力矩的快速控制规律。 给出了机动时间和系统状态的简单计算公式。
短句来源
    This paper designs an attitude decoupling control law for small satellite in large-angle biased flight mode about roll axis of zero-momentum system via reaction wheels.
    研究了采用反作用飞轮为执行机构的整星零动量卫星绕X轴大角度偏置飞行模式的姿态解耦控制问题。
短句来源
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  reaction wheel
A lumped mass dynamic model of the reaction wheel is given in Figure 3-1.
      
A tachometer signal is required for speed and direction of rotation feedback from the reaction wheel.
      
A two-dimensional schematic of the PREMAG magnetically suspended reaction wheel.
      
As external disturbances were compensated for using a shown in Figure 4, thrust values determined from reaction wheel.
      
Continuous magnetic unloading of reaction wheel momentum will be performed using a cross-product control law.
      
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