您要查找的是不是：
- Single gimbal control moment gyroscope (SGCMG) is one kind of inertial actuators applied to the spacecrafts.Three or more SGCMGs are used in order to meet the need of the 3-axis attitude control. 摘要為滿(mǎn)足航天器姿態(tài)三軸控制的要求，通常在姿態(tài)控制系統中采用3個(gè)或以上的單框架控制力矩陀螺(SGCMG)。
- And from the comprehensive survey of satellite development in foreign countries, the Control Moment Gyroscope (CMG) is a commonly used controller in the control system of large satellites. 縱觀(guān)國外衛星的發(fā)展,大型衛星控制系統通常采用的執行機構是控制力矩陀螺(CMG)。
- Single Gimbal Control Moment Gyroscope (SGCMG) 單框架力矩陀螺
- double-gimbal control moment gyroscope 雙框架控制力矩陀螺
- Stability of active magnetic bearing for control moment gyroscope 高速磁懸浮轉子穩定性研究及其在控制力矩陀螺中應用
- Failures of the five pyramid configuration(FPC) of single-gimbal control moment gyroscopes(SGCMGs) were studied using the singularity analysis method. 從奇異性分析角度對單框架控制力矩陀螺(SGCMG)的五棱錐構型(FPC)及其失效情況進(jìn)行了研究。
- Configuration Analysis of Single Gimbal Control Moment Gyroscope Systems 單框架控制力矩陀螺系統的構形分析
- In other spacewalk activities, astronauts installed an external platform onto the Station's Quest Airlock and replaced one of the orbital outpost's Control Moment Gyroscopes. 在太空漫步活動(dòng)中，宇航員在檢修氣壓過(guò)渡艙之上安裝了一個(gè)外部的平臺而且代替了軌道的控制回旋裝置。
- Control Moment Gyroscopes (CMGs) are often assumed to have ideal steering performance when they are used as actuators in the attitude control system of space station. 摘要在空間站姿態(tài)控制系統設計中，一般采用控制力矩陀螺(CMG)作為執行機構，并假定控制力矩陀螺具有理想的操縱性能。
- Physical parameters of single gimbal control moment gyroscopes (SGCMGs) are often assumed to be known exactly when steering la is designed by taking gimbal servo characteristics into account. 摘要在單框架控制力矩陀螺(SGCMG)系統操縱律的設計中，如果考慮框架伺服特性，往往假設系統的物理參數是確切已知的。
- Design of A Non-Contact Displacement Measurement Sensor for Control Moment Gyroscope Based on Active Magnetic Bearings 一種基于電磁軸承的控制力矩陀螺用非接觸位移傳感器設計
- Design and Realization of a Digital Control System for Active Magnetic Bearing of Control Moment Gyroscope 控制力矩陀螺用主動(dòng)電磁軸承數字控制系統設計與實(shí)現
- Singularity avoidance in redundant single gimbal control moment gyroscope systems 單框架控制力矩陀螺系統的運動(dòng)奇異及回避
- Self-Excited Vibration Depression of High-Speed Rotor in Magnetically Suspended Control Moment Gyroscope 磁懸浮控制力矩陀螺高速轉子高頻自激振動(dòng)的抑制
- Control Moment Gyroscope(CMG) 控制力矩陀螺
- Control moment gyroscope 控制力矩陀螺
- Dynamics and Control of Gimbal Servo Systems for Control Moment Gyroscopes 控制力矩陀螺框架伺服系統動(dòng)力學(xué)建模與控制
- Dynamic Steering Law Design for Redundant Single Gimbal Control Moment Gyroscopes 單框架控制力矩陀螺動(dòng)態(tài)操縱律設計
- Spacecraft Adaptive Attitude Tracking and Stable Control with Variable Speed Control Moment Gyroscopes 采用變速控制力矩陀螺的航天器自適應姿態(tài)跟蹤和穩定控制研究
- This paper, aimed at several crucial problems in the application of CMG to large satellites, is studied to afford basis for the application of moment gyroscope in aerospace engineering. 本文正是針對控制力矩陀螺在大型衛星應用的幾個(gè)關(guān)鍵問(wèn)題而開(kāi)展研究,為控制力矩陀螺工程應用提供依據。
