A micromachined electrostatically suspended gyroscope(MESG)based on UV-LIGA microfabrication process was introduced.By close-loop control,the suspended rotor is kept in null position and through the torque rebalance l...A micromachined electrostatically suspended gyroscope(MESG)based on UV-LIGA microfabrication process was introduced.By close-loop control,the suspended rotor is kept in null position and through the torque rebalance loop,in which the output control voltages reflects the input angular velocity,a dual-axis input angular velocity can be measured simultaneously.First,the system model of MESG was established by dynamic analysis based on the torque analysis.Then,the rebalance loop under ideal condition is designed using modern control technique.The performance of the designed decoupling rebalance loop was compared with that of conventional proportional integral differential(PID)rebalance loop combined with the compensation loop.In order to realize the decoupling of the output voltages,a compensated decoupling matrix and its difference equation were presented and realized by a digital decoupling method employing digital signal processor(DSP).It was confirmed that the controller could realize the complete decoupling and improve the performance of the gyroscope,which includes merits of fast response speed,low overshoot and good dynamic performance,as the simulation results shown.At last,the circuit and digital realization scheme were given.展开更多
Non-spherical of rotor was described with solution method. Electrostatically suspended gyroscope＇s hollow spherical rotor＇s structure was presented. The simulative analysis of static deformation, dynamic deformation...Non-spherical of rotor was described with solution method. Electrostatically suspended gyroscope＇s hollow spherical rotor＇s structure was presented. The simulative analysis of static deformation, dynamic deformation and synthesize deformation of rotor under different working conditions using the finite element software were carried out. Its deformation law and volume were obtained. The structural parameters of the rotor were optimized. The value of pressure required when the rotor was machined was calculated. The analysis has important theoretical reference value to the design for hollow spherical rotor in electrostatically suspended gyroscope.展开更多
双框架磁悬浮控制力矩陀螺(Double gimbal magnetically suspended control moment gyroscope,DGMSCMG)是由磁悬浮高速转子系统与内框架、外框架速率伺服系统构成的航天器新型姿控执行机构。由于非线性及三个子系统间的强耦合,框架转动...双框架磁悬浮控制力矩陀螺(Double gimbal magnetically suspended control moment gyroscope,DGMSCMG)是由磁悬浮高速转子系统与内框架、外框架速率伺服系统构成的航天器新型姿控执行机构。由于非线性及三个子系统间的强耦合,框架转动时磁悬浮转子位移急剧增大影响稳定性,同时框架系统的响应速度显著下降,称之为动框架效应。该效应严重影响了DGMSCMG的功能,必须加以抑制。建立DGMSCMG的动力学模型,分析三个子系统间的动力学耦合机理,提出一种基于复合控制的补偿方法,引入针对陀螺项的反馈和针对框架角速率给定的前馈消除磁悬浮转子附加位移,提高框架系统响应速度,并对补偿后系统做全局稳定性分析。仿真和试验结果表明,该方法能在保证系统稳定性的前提下有效抑制动框架效应,满足DGMSCMG的功能要求。展开更多
基金Sponsored by the Pre-weapons Research Fund(Grant No.9140A09020706JW0314)New Teacher Research Fund for the Doctoral Program of HigherEducation of China(Grant No.200802481026)
文摘A micromachined electrostatically suspended gyroscope(MESG)based on UV-LIGA microfabrication process was introduced.By close-loop control,the suspended rotor is kept in null position and through the torque rebalance loop,in which the output control voltages reflects the input angular velocity,a dual-axis input angular velocity can be measured simultaneously.First,the system model of MESG was established by dynamic analysis based on the torque analysis.Then,the rebalance loop under ideal condition is designed using modern control technique.The performance of the designed decoupling rebalance loop was compared with that of conventional proportional integral differential(PID)rebalance loop combined with the compensation loop.In order to realize the decoupling of the output voltages,a compensated decoupling matrix and its difference equation were presented and realized by a digital decoupling method employing digital signal processor(DSP).It was confirmed that the controller could realize the complete decoupling and improve the performance of the gyroscope,which includes merits of fast response speed,low overshoot and good dynamic performance,as the simulation results shown.At last,the circuit and digital realization scheme were given.
基金supported by the Shandong Province Scientific Research Fund Project of Binzhou University under Grant No. BZXYLG200704
文摘Non-spherical of rotor was described with solution method. Electrostatically suspended gyroscope＇s hollow spherical rotor＇s structure was presented. The simulative analysis of static deformation, dynamic deformation and synthesize deformation of rotor under different working conditions using the finite element software were carried out. Its deformation law and volume were obtained. The structural parameters of the rotor were optimized. The value of pressure required when the rotor was machined was calculated. The analysis has important theoretical reference value to the design for hollow spherical rotor in electrostatically suspended gyroscope.
文摘双框架磁悬浮控制力矩陀螺(Double gimbal magnetically suspended control moment gyroscope,DGMSCMG)是由磁悬浮高速转子系统与内框架、外框架速率伺服系统构成的航天器新型姿控执行机构。由于非线性及三个子系统间的强耦合,框架转动时磁悬浮转子位移急剧增大影响稳定性,同时框架系统的响应速度显著下降,称之为动框架效应。该效应严重影响了DGMSCMG的功能,必须加以抑制。建立DGMSCMG的动力学模型,分析三个子系统间的动力学耦合机理,提出一种基于复合控制的补偿方法,引入针对陀螺项的反馈和针对框架角速率给定的前馈消除磁悬浮转子附加位移,提高框架系统响应速度,并对补偿后系统做全局稳定性分析。仿真和试验结果表明,该方法能在保证系统稳定性的前提下有效抑制动框架效应,满足DGMSCMG的功能要求。
