空间精密跟瞄Hexapod平台作动器研制与实验  

Development and experiment of active member for space-base precise pointing Hexapod

作　　者：李伟鹏[1] 黄海[1] 边边[1] 

机构地区：[1]北京航空航天大学宇航学院,北京100083

出　　处：《北京航空航天大学学报》2007年第9期1017-1020,1040,共5页Journal of Beijing University of Aeronautics and Astronautics

基　　金：国家863基金资助项目

摘　　要：针对基于并联机构的空间精密跟瞄Hexapod平台的大行程、高性能要求,通过对现有主动元件的分析,从作动器角度研制了以滚珠丝杠作动器为宏动部分、压电作动器为微动部分的大行程高频响精密复合作动器,测试了复合作动器的行程、开环定位精度及动态特性,以dSPACE半物理仿真系统为核心建立了实验系统,进行了复合作动器单自由度精确定位实验和振动主动控制实验.由结果可知,复合作动器作动行程超过50 mm、经微动部分补偿后的整体定位误差小于1μm、正弦持续扰动下采用自适应滤波ADC(Active Disturbance Canceller)方法使振幅下降90%以上.结果表明,将此复合作动器应用于空间高稳定精密跟瞄Hexa-pod平台是完全可行的.A platform scheme that provides precision pointing and active vibration isolation for space-base payloads based on parallel mechanism-Hexapod was proposed. With the analysis of the current Hexapod＇s actuators, a high precision dual-driving hybrid actuator was developed. It integrated ball-screw actuator as macro-moving stage and piezoelectric stack actuator as micro - moving stage. Key characteristics of the hybrid actuator were measured at first, such as stroke, macro-moving stage open-loop positioning accuracy and micromoving stage dynamic property. An experiment system based on MATLAB/dSPACE environment was established and the actuator single degree-of-freedom positioning experiment and active vibration isolation experiment were carried on then. Experiment results show that the hybrid actuator stroke exceeds 50 mm and its whole positioning error being less than 1 μm with the close-loop compensation of the micro-moving stage. The results also show that when continuously excited at 30Hz on one end of the hybrid actuator, vibration on the other end is decreased more than 90% with the adaptive filtering active disturbance canceller （ADC） algorithm. The study indicates that the hybrid actuator is expected to apply to precise pointing Hexapod.

关 键 词：并联机构 复合作动器 精密定位 主动振动控制 

分 类 号：V41[航空宇航科学与技术—航空宇航推进理论与工程]