Volume 16 Issue 6
Nov.  2023
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REN Li-min, CHEN Li-heng, MENG Xu, WANG Zhi. Thermal design of ground weak force measurement system for inertial sensors[J]. Chinese Optics, 2023, 16(6): 1404-1413. doi: 10.37188/CO.2023-0022
Citation: REN Li-min, CHEN Li-heng, MENG Xu, WANG Zhi. Thermal design of ground weak force measurement system for inertial sensors[J]. Chinese Optics, 2023, 16(6): 1404-1413. doi: 10.37188/CO.2023-0022

Thermal design of ground weak force measurement system for inertial sensors

doi: 10.37188/CO.2023-0022
Funds:  Supported by National Key R & D Program of China (No. 2020YFC2200600)
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  • Corresponding author: chenliheng3@163.com
  • Received Date: 04 Feb 2023
  • Rev Recd Date: 20 Feb 2023
  • Accepted Date: 26 Jul 2023
  • Available Online: 26 Jul 2023
  • In order to meet the ultra-high temperature stability requirements of the ground weak force measurement system for inertial sensor, the thermal design of the whole system is carried out. Firstly, the structure of ground weak force measurement system of inertial sensor, heat transfer path of sensitive structure and internal heat source are introduced. Secondly, according to the index requirements of the thermal control of the system, a high-precision thermal control method combining the three-stage thermal control structure and Proportional Integral Differential (PID) control algorithm is proposed to reduce the influence of temperature noise on the detection sensitivity of the inertial sensor. Then, UG/NX software is used to establish the finite element model and carry out the thermal analysis calculation under different working conditions, and the temperature change value of the measurement system in the time domain after equilibrium is (1.2−1.6) ×10−5 K. Finally, the temperature distribution of the measurement system in the time domain is described in the frequency domain, and the temperature stability results of sensitive structure of the inertial sensor are obtained. The analysis results show that under the current thermal control measures, the temperature stability of the sensitive structure of the inertial sensor is better than 10−4 K/Hz1/2, meeting the requirements of thermal control indicators, and the thermal design scheme is reasonable and feasible.

     

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  • [1]
    CYRANOSKI D. Chinese gravitational-wave hunt hits crunch time[J]. Nature, 2016, 531(7593): 150-151. doi: 10.1038/531150a
    [2]
    HU W R, WU Y L. The Taiji program in space for gravitational wave physics and the nature of gravity[J]. National Science Review, 2017, 4(5): 685-686. doi: 10.1093/nsr/nwx116
    [3]
    GONG Y G, LUO J, WANG B. Concepts and status of Chinese space gravitational wave detection projects[J]. Nature Astronomy, 2021, 5(9): 881-889. doi: 10.1038/s41550-021-01480-3
    [4]
    LUO J, CHEN L SH, DUAN H Z, et al. TianQin: a space-borne gravitational wave detector[J]. Classical and Quantum Gravity, 2016, 33(3): 035010. doi: 10.1088/0264-9381/33/3/035010
    [5]
    LOBO A, NOFRARIAS M, RAMOS-CASTRO J, et al. On-ground tests of the LISA PathFinder thermal diagnostics system[J]. Classical and Quantum Gravity, 2006, 23(17): 5177-5193. doi: 10.1088/0264-9381/23/17/005
    [6]
    HIGUCHI S, SUN K X, DEBRA D B, et al. Design of a highly stable and uniform thermal test facility for MGRS development[J]. Journal of Physics: Conference Series, 2009, 154: 012037. doi: 10.1088/1742-6596/154/1/012037
    [7]
    LUO J, BAI Y ZH, CAI L, et al. The first round result from the TianQin-1 satellite[J]. Classical and Quantum Gravity, 2020, 37(18): 185013. doi: 10.1088/1361-6382/aba66a
    [8]
    CHEN K, ZHANG X F, GUO T, et al. Key technologies analysis and design of ultra-clean & ultra-stable spacecraft for gravitational wave detection[J]. International Journal of Modern Physics A, 2021, 36(11-12): 2140021.
    [9]
    刘红, 张晓峰, 冯建朝, 等. 精密热控技术在太极一号卫星上的应用[J]. 空间科学学报, 2021, 41(2): 337-341.

    LIU H, ZHANG X F, FENG J CH, et al. Application of precision thermal control techniques in Taiji-1 satellite[J]. Chinese Journal of Space Science, 2021, 41(2): 337-341. (in Chinese)
    [10]
    王少鑫. 空间惯性传感器敏感结构构建及地面评价方法研究[D]. 长春: 中国科学院大学(中国科学院长春光学精密机械与物理研究所), 2020.

    WANG SH X. Research on the construction of the sensitive structure and ground evaluation method of space inertial sensor[D]. Changchun: Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, 2020. (in Chinese)
    [11]
    ARMANO M, AUDLEY H, AUGER G, et al. In-flight thermal experiments for LISA pathfinder: simulating temperature noise at the inertial sensors[J]. Journal of Physics: Conference Series, 2015, 610: 012023. doi: 10.1088/1742-6596/610/1/012023
    [12]
    BENDER P L. LISA sensitivity below 0.1 mHz[J]. Classical and Quantum Gravity, 2003, 20(10): S301-S310. doi: 10.1088/0264-9381/20/10/333
    [13]
    LIU J Y, SERGATSKOV D A, DUNCAN R V. Adaptive optimal PI controller for high-precision low-temperature experiments[C]. Proceedings of the 2005, American Control Conference, IEEE, 2005: 4220-4224.
    [14]
    ZHANG J, ZHANG K Y. A particle swarm optimization approach for optimal design of PID controller for temperature control in HVAC[C]. Proceedings of 2011 Third International Conference on Measuring Technology and Mechatronics Automation, IEEE, 2011: 230-233.
    [15]
    GUO T T, WANG Q T, SHEN Q. A high accurate adaptive temperature control algorithm based on fuzzy reasoning and PID control[J]. Applied Mechanics and Materials, 2013, 331: 352-355. doi: 10.4028/www.scientific.net/AMM.331.352
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