1) VSCMG
变速控制力矩陀螺
1.
This paper deals with the attitude tracking of spacecraft with single-gimbal variable-speed control moment gyroscopes(VSCMGs) as actuator.
研究以变速控制力矩陀螺群(VSCMGs)为执行机构的航天器姿态跟踪问题。
2.
The steering law of variable speed control moment gyros(VSCMGs) used in integrated power/attitude control system(IPACS) is studied.
研究以变速控制力矩陀螺群(VSCMGs)为执行机构的能量/姿态一体化控制系统(IPACS)中的操纵律设计问题。
3.
This paper deals with the Integrated Power and Attitude Control System(IPACS) for spacecraft with single-gimbal Variable-Speed Control Moment Gyroscopes(VSCMGs) as main actuator.
研究以变速控制力矩陀螺群(VSCMGs)为主执行机构的卫星功率/姿态一体化控制(IPACS)问题。
2) variable speed control moment gyros
变速控制力矩陀螺
1.
The dynamical equations of a flexible spacecraft with VSCMGs(variable speed control moment gyros) were established,and the attitude kinematics was described by the error-quaternion so that the large angle maneuver of the satellite could be converted into the problem of regulation of the error-quaternion.
建立了带变速控制力矩陀螺群的挠性航天器的动力学模型,应用误差四元数来描述姿态运动,将星体大角度姿态机动问题转化为误差四元数的调节问题。
3) Variable Speed Control Moment Gyro(VSCMG)
变速控制力矩陀螺
1.
The multi-target rapid maneuver control problem is studied for agile satellites with Variable Speed Control Moment Gyro(VSCMG) as actuator.
研究了以变速控制力矩陀螺(VSCMG)作为执行机构的卫星多目标快速机动的控制问题。
4) variable speed control moment gyro
变速控制力矩陀螺
1.
This paper studies the integrated power and attitude control of a spacecraft using variable speed control moment gyros (VSCMG).
利用变速控制力矩陀螺(VSCMG)的航天器姿态与能量一体化控制问题。
2.
The fast-maneuver and high-attitude-stability control problem of agile satellites is addressed by employing the variable speed control moment gyros(VSCMGs) as the actuator.
研究采用变速控制力矩陀螺群(VSCMGs)作为姿态控制执行机构的高姿态稳定度敏捷卫星的操纵律设计问题。
5) control moment gyroscope
控制力矩陀螺
1.
Identification of magnetic parameters for magnetic bearings in control moment gyroscope(CMG);
控制力矩陀螺用磁轴承磁力参数的辨识
2.
The finite element model of the structure of the control moment gyroscope(CMG) is established and modal analysis about the rotor component and CMG combined structure is described in the application of the large-scale general software ANSYS7.
0,建立了控制力矩陀螺结构的有限元模型,对磁悬浮飞轮转子组件以及陀螺整体组合结构进行了模态分析。
6) CMG
控制力矩陀螺
1.
Fuzzy Control Method of Gimbal Servo System in Magnetically Suspended Rotor System of CMG
磁悬浮控制力矩陀螺框架伺服系统前馈补偿模糊控制方法
2.
This paper is focused on a new control method to lower the power loss of the active magnetic bearing(AMB) in magnetically suspended control moment gyro(MSCMG).
磁悬浮控制力矩陀螺(MSCMG)在输出力矩且不计重力引入的功耗时,磁轴承的铜耗与输出力矩的平方成正比。
3.
In order to eliminate the friction made by the MSCMG framework servo system,the gyro architecture was analyzed through dynamics methods first.
为消除磁悬浮控制力矩陀螺(MSCMG)框架伺服系统摩擦的影响,对陀螺框架系统进行动力学分析,分析了摩擦力矩随陀螺输出力矩和框架角位置及角速度的关系,建立了框架系统的非线性摩擦力矩模型。
补充资料：陀螺力矩
分子式：
CAS号：
性质：高速旋转的转子具有保持自转的轴线方向不变的特性。当它进动旋转即又绕另一相交轴公转时就产生一个使之恢复原自转轴线方向的力矩。将转子上这些力矩全部叠加(积分)起来就称为陀螺力矩，也称回转力矩。转子直径越大陀螺力矩越大。意味着轴的刚性越大，其临界转数越增加。因此设计刚性轴时应设法增加陀螺力矩，设计挠性轴时则应力求减小陀螺力矩。
CAS号：
性质：高速旋转的转子具有保持自转的轴线方向不变的特性。当它进动旋转即又绕另一相交轴公转时就产生一个使之恢复原自转轴线方向的力矩。将转子上这些力矩全部叠加(积分)起来就称为陀螺力矩，也称回转力矩。转子直径越大陀螺力矩越大。意味着轴的刚性越大，其临界转数越增加。因此设计刚性轴时应设法增加陀螺力矩，设计挠性轴时则应力求减小陀螺力矩。
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参考词条