Microgravity disturbance analysis on Chinese space laboratory

被引:19
作者
Dong, Wenbo [1 ,2 ]
Duan, Wenxiang [1 ,2 ,3 ]
Liu, Wei [1 ,2 ]
Zhang, Yongkang [1 ,2 ]
机构
[1] Chinese Acad Sci, Key Lab 3 Space Utilizat, Beijing 100094, Peoples R China
[2] Chinese Acad Sci, Technol & Engn Ctr Space Utilizat, Beijing 100094, Peoples R China
[3] Univ Chinese Acad Sci, Beijing 100094, Peoples R China
关键词
VIBRATION ISOLATION SYSTEM;
D O I
10.1038/s41526-019-0078-z
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
Many scientific experiments are conducted in space; therefore, it is critical to understand the microgravity environment of a space laboratory. The first Chinese cargo ship, Tianzhou-1 (TZ-1), entered space on 20 April, 2017 and later joined with the Tiangong-2 (TG-2) Chinese space laboratory. TZ-1 carried a high-precision electrostatic suspension accelerometer system (ES-ACC) for measuring the microgravity acceleration on the spacecraft and a microgravity-active vibration system (MAIS), which contained flexible quartz accelerometers (Q-ACC). The ES-ACC was able to provide a reduced-disturbance environment for the MAIS. The purpose of these two instruments was to validate novel technologies and as an opportunity to record the microgravity acceleration of TZ-1 and TG-2 in detail during spacecraft operation in different flight modes, with or without vibration isolation. The acceleration data were analyzed comprehensively in a time-frequency-amplitude spectrogram. Some periodical disturbances with orbital period and irregular signals related to certain in-orbit events were observed. After reducing those disturbances, the microgravity levels on TZ-1 and TG-2 could be resolved to better than 10(-6) m/s(2) in the root mean square in the frequency of 0.01-10 Hz. These accurate measurements aboard the Chinese space laboratory will provide valuable information to optimize working conditions for scientific experiments.
引用
收藏
页数:6
相关论文
共 34 条
  • [31] [薛大同 Xue Datong], 2004, [物理, Physics], V33, P351
  • [32] Design of a Vibration Isolation System for the Space Telescope
    Yang, Jianfeng
    Xu, Zhenbang
    Wu, Qingwen
    Wang, Zhongsu
    Li, Hang
    He, Shuai
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2015, 38 (12) : 2441 - 2447
  • [33] Verification of the Microgravity Active Vibration Isolation System based on Parabolic Flight
    Zhang, Yong-kang
    Dong, Wen-bo
    Liu, Wei
    Li, Zong-feng
    Lv, Shi-meng
    Sang, Xiao-ru
    Yang, Yang
    [J]. MICROGRAVITY SCIENCE AND TECHNOLOGY, 2017, 29 (06) : 415 - 426
  • [34] Zhou Z., 2010, CLASSICAL QUANT GRAV, V2787