Spacecraft Recovery & Remote Sensing, Volume. 45, Issue 4, 29(2024)

Design and Implementation of a Light Weight, Compact, and Highly Reliable Recovery Controller

Jinglei LIU1,2, Yunlong YAN1,2, Xiaoyan PEI1,2, Xiyun SUN1,2, Haiye LIU1,2, and Maoyong QIAO1,2
Author Affiliations
  • 1Beijing Institute of Space Mechanics & Electricity, Beijing 100094, China
  • 2Laboratory of Aerospace Entry, Descent and Landing Technology, CASC, Beijing 100094, China
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    Figures & Tables(11)
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    • Table 1. Main technical indicators of overload sensor

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      Table 1. Main technical indicators of overload sensor

      指标项指标数据
      测量范围±10 g
      灵敏度(200±10)mV/g
      零位输出2 400~2 600 mV
      外形尺寸16.5 mm×14 mm×13.8 mm
      质量≤10 g
    • Table 2. Centrifuge simulated overload test resules

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      Table 2. Centrifuge simulated overload test resules

      工况触发时间传感器1触发点过载/g传感器2触发点过载/g传感器3触发点过载/g
      下降沿触发工况A机触发过载5.775.775.71
      B机触发过载5.625.635.52
      上升沿触发工况A机触发过载4.965.285.12
      B机触发过载4.965.195.07
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    Jinglei LIU, Yunlong YAN, Xiaoyan PEI, Xiyun SUN, Haiye LIU, Maoyong QIAO. Design and Implementation of a Light Weight, Compact, and Highly Reliable Recovery Controller[J]. Spacecraft Recovery & Remote Sensing, 2024, 45(4): 29

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    Paper Information

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    Received: Oct. 9, 2023

    Accepted: --

    Published Online: Nov. 1, 2024

    The Author Email:

    DOI:10.3969/j.issn.1009-8518.2024.04.004

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