单框架控制力矩陀螺,SGCMG英语短句,例句大全

单框架控制力矩陀螺,SGCMG
1)SGCMG单框架控制力矩陀螺
1.Research on Physics Simulation of Large Spacecraft Attitude Control System Using SGCMG;用单框架控制力矩陀螺的大型航天器姿态控制系统实物仿真研究
2.Single Gimble Control Moment Gyro (SGCMG) is a momentum exchange device of spacecraft, which is suitable for three-axis attitude control and quick movement of large spacecraft.单框架控制力矩陀螺(SGCMG)是一种重要的航天器动量交换装置。
3.Singularity of SGCMG system is analyzed in this paper.作为航天器制导、导航和控制系统的执行部件，单框架控制力矩陀螺是较为理想的大型航天器姿控系统的选择，但是单框架控制力矩陀螺系统（ＳＧＣＭＧ）存在严重的奇异现象，增加了操纵律的设计与开发的难度。
2)single-gimbal control moment gyros单框架控制力矩陀螺群
1.This research is focused on the singularity analysis for single-gimbal control moment gyros systems (SCMGs) which include two types, with constant speed (CSCMG) or variable speed (VSCMG) rotors.使用几何方法对单框架控制力矩陀螺群(包括转子恒速的CSCMG和转子变速的VSCMG)的奇异性进行了分析。
3)DGCMG双框架控制力矩陀螺
1.An exact mathematical description of spacecraft attitude motion driven by double-gimbal control moment gyroscopes(DGCMGs) is proposed.推导出了双框架控制力矩陀螺系统操纵空间飞行器姿态机动的精确数学模型,并在此基础上基于Lyapunov第二法设计了空间飞行器大角度姿态机动非线性控制律,在设计的同时证明了系统的稳定性。

英文短句/例句

1.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
2.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
3.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
4.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
5.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
6.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
7.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
8.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
9.Active Magnetic Suspended CMG System Simulation主动磁悬浮控制力矩陀螺的系统仿真
10.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
11.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
12.gravity-gyro attitude-control system重力陀螺高度控制仪
13.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
14.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
15.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
16.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
17.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
18.Robust Nonlinear Slewing Motion Control of Spacecraft Truss with Scissored Pair of CMGs基于同步双陀螺的空间构架非线性鲁棒回转运动控制

相关短句/例句

single-gimbal control moment gyros单框架控制力矩陀螺群
1.This research is focused on the singularity analysis for single-gimbal control moment gyros systems (SCMGs) which include two types, with constant speed (CSCMG) or variable speed (VSCMG) rotors.使用几何方法对单框架控制力矩陀螺群(包括转子恒速的CSCMG和转子变速的VSCMG)的奇异性进行了分析。
3)DGCMG双框架控制力矩陀螺
1.An exact mathematical description of spacecraft attitude motion driven by double-gimbal control moment gyroscopes(DGCMGs) is proposed.推导出了双框架控制力矩陀螺系统操纵空间飞行器姿态机动的精确数学模型,并在此基础上基于Lyapunov第二法设计了空间飞行器大角度姿态机动非线性控制律,在设计的同时证明了系统的稳定性。
4)Single Gimbal Control Moment Gyroscope(SGCMG)单框架力矩陀螺
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。