摘要
针对航天器在轨微振动环境测量,文章分析了微振动的来源及其对空间科学实验和对地成像载荷的影响,设计了典型微振动测量单元,提出了微振动测量单元标度因数和偏值的地面标定方法,利用精测设备进行了地面测试验证,结果表明微振动测量单元各轴测量误差小于5×10^(-3)g0,验证了微振动测量单元的设计和地面标定方法的正确性。
For the on-board micro-vibration of a spacecraft, the disturbance source and the micro-vibration effect on the space scientific experimental instruments and the earth-imaging payloads are analyzed. A typical configuration of the micro-vibration measurement unit is designed. A method of on-ground calibration for the scale factor and the offset value is proposed and verified by accurate alignment tests. The testing result shows that the measurement error in each axis is less than 5×10-3g0 and the design and the calibration method are feasible.
作者
杨金禄
孙永进
赵振昊
霍红庆
YANG Jinlu;SUN Yongjin;ZHAO Zhenhao;HUO Hongqing(Institute of Manned Space System Engineering, China Academy of Space Technology, Beijing 100094, China;Lanzhou Institute of Space Technology Physics, Lanzhou 730000, China)
出处
《航天器环境工程》
2016年第6期680-685,共6页
Spacecraft Environment Engineering
关键词
航天器
微振动
测量
标度因数
偏值
地面标定
spacecraft
micro-vibration measurement
scale factor
offset value
ground calibration
