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基于機器視覺(jué)的航天器密封艙內結構裝配精度檢測系統設計
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天津航天機電設備研究所

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Design of the precision detection system for the assembly accuracy of the spacecraft sealed cabin structure based on machine vision
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    摘要:

    目前航天器機械加工裝配作業(yè)依賴(lài)人工操作,影響航天器密封艙內結構裝配精度。為此,設計了航天器密封艙內結構裝配精度檢測系統,為高精度裝配航天器密封艙內結構提供基礎。由于航天器密封艙艙內結構較為復雜,為了保證使用電池供電時(shí),檢測系統能夠保持穩定可靠工作模式,應保證電池電量充足前提下,系統發(fā)出預警信息,以便工作人員及時(shí)采取相應解決措施。在電池供電電路中,設計欠電壓電路監測形式,該電路主要是由電壓比較器LM393和555和諧振電路構成。當電池供電量不足時(shí),諧振電路中的微電流高效率650nm諧振腔發(fā)光二極管會(huì )出現閃爍報警信號。以STC89C52RC-40I-PDIP40單片機中央控制單元為核心芯片,檢測航天器密封艙密封性能。依據機器視覺(jué)檢測原理,使用非線(xiàn)性濾波算法增強圖像,避免外界噪聲對圖像采集結果造成影響,濾除圖像上若干白點(diǎn)。設計檢測流程可得到儀器板安裝精度和設備安裝支架裝調檢測結果。由實(shí)驗結果可知,該系統檢測精度最高與實(shí)測值一致,為航天器密封艙內結構優(yōu)化提供設備支持。

    Abstract:

    At present, the machining and assembly operations of spacecraft rely on manual operation, which affects the assembly accuracy of the structure inside the sealed cabin of the spacecraft. To this end, an assembly precision detection system for the spacecraft sealed cabin structure was designed to provide a basis for high-precision assembly of the spacecraft sealed cabin structure. Due to the complicated structure of the spacecraft's sealed cabin, in order to ensure that the detection system can maintain a stable and reliable working mode when using battery power, the system should issue an early warning message on the premise of sufficient battery power, so that the staff can take corresponding solutions in time. In the battery-powered circuit, the monitoring form of the undervoltage circuit is designed. The circuit is mainly composed of voltage comparators LM393 and 555 and a resonant circuit. When the battery power supply is insufficient, the micro-current high-efficiency 650nm resonant cavity LED in the resonant circuit will flash a warning signal. The STC89C52RC-40I-PDIP40 single-chip microcomputer central control unit is used as the core chip to test the sealing performance of the spacecraft sealed cabin. According to the principle of machine vision detection, a nonlinear filtering algorithm is used to enhance the image, to avoid the influence of external noise on the image acquisition result, and to filter out some white spots on the image. The testing process can be designed to obtain the test results of the installation accuracy of the instrument board and the installation and adjustment of the equipment mounting bracket. It can be seen from the experimental results that the highest detection accuracy of the system is consistent with the measured values, which provides equipment support for the optimization of the structure of the spacecraft sealed cabin.

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龐學(xué)豐,王瑞文,張玉美,趙超澤.基于機器視覺(jué)的航天器密封艙內結構裝配精度檢測系統設計計算機測量與控制[J].,2020,28(8):53-57.

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  • 收稿日期:2020-05-07
  • 最后修改日期:2020-06-01
  • 錄用日期:2020-06-01
  • 在線(xiàn)發(fā)布日期: 2020-08-13
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