变速控制力矩陀螺,VSCMG英语短句,例句大全

变速控制力矩陀螺,VSCMG
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。

英文短句/例句

1.Active Magnetic Suspended CMG System Simulation主动磁悬浮控制力矩陀螺的系统仿真
2.The Study of the Control Moment Gyroscope with Application to the Satellite Attitude Control System;控制力矩陀螺在卫星控制系统中的应用
3.Research and Design of Servo Circuit for Magnetically Suspended Control Moment Gyroscope Gimbal磁悬浮控制力矩陀螺框架伺服电路研究与设计
4.Steering Law for Parallel Mounted Double Gimbaled Control Moment Gyros平行构型双框架控制力矩陀螺操纵律研究
5.Digital Servo System for Gimbal of Control Moment Gyro Based on DSP基于DSP的控制力矩陀螺框架数字伺服系统
6.Whirling Characteristics of High Speed Rotors in Flywheel and CMG飞轮和控制力矩陀螺高速转子的涡动特性研究
7.Singularity Analysis and Visualization of Double-Gimbaled Control Moment Gyro Systems双框架控制力矩陀螺奇异分析及可视化
8.High Precision Speed Digital Control System of BLDCM for CMG磁悬浮控制力矩陀螺用高速高精度无刷直流电机全数字控制系统
9.Moving-gimbal Effects and Angular Rate Feedforward Control in Magnetically Suspended Rotor System of CMG磁悬浮控制力矩陀螺的动框架效应及其角速率前馈控制方法研究
10.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
11.Nonlinear Attitude Control of Spacecraft Based on Double-Gimbaled Control Moment Gyroscopes基于双框架控制力矩陀螺的空间飞行器非线性姿态控制
12.Dynamics and Simulation of Spacecraft with Magnetically Suspended Control Moment Gyroscope基于磁悬浮控制力矩陀螺的航天器动力学与仿真
13.Study on the System Disturbance Rejection Method Used in the Gimbal Servo System of Double Gimbal Magnetically Suspended Control Moment Gyro一种双框架磁悬浮控制力矩陀螺框架伺服系统扰动抑制方法研究
14.Modal Analysis and Experimental Study of Magnetic Suspended CMG’s Structure磁悬浮控制力矩陀螺的高速转子模态分析及实验研究
15.Analysis of Structural Reliablity of Minitype Control Moment Gyroscope Using Finite Element Method应用有限元法的小型控制力矩陀螺结构可靠性分析
16.Axial Disturbance Characteristics for High Speed Rotor of Flywheel and CMG飞轮和控制力矩陀螺高速转子轴向干扰特性的研究
17.gravity-gyro attitude-control system重力陀螺高度控制仪
18.Analysis of Disturbing Torque in Electrostatic Field Caused by Rotor Radial Disbalance in ESG静电陀螺转子径向偏心干扰力矩分析

相关短句/例句

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。