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再入飛行器低誤碼率數字化遙測系統設計
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北京航天長(cháng)征飛行器研究所

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Design of Low Error Rate Digital Telemetry System for Reentry Vehicle
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    摘要:

    針對再入飛行器遙測領(lǐng)域要求存儲系統容量大、誤碼率低、惡劣環(huán)境下可靠回收等特點(diǎn),以及傳統供配電方式存在的地面設備組成多、操作復雜、可靠性低等不足,提出了一種適用于再入飛行器的低誤碼率數字化遙測系統設計方法。系統采用大容量冗余備份存儲設計、基于ECC糾錯編碼算法的低誤碼率設計、抗高沖擊回收防護設計等關(guān)鍵技術(shù),存儲容量提高到32GB,可連續存儲9h數據,存儲器誤碼率降低至10-10,實(shí)現了高沖擊條件下的可靠回收;采用基于1553B總線(xiàn)的數字化供配電技術(shù)、在線(xiàn)故障診斷技術(shù)等關(guān)鍵技術(shù),簡(jiǎn)化了地面測試設備及操作,節約研制成本,提高了飛行器智能化和測試性水平。該系統已成功應用于某再入飛行器,通過(guò)了地面炮擊試驗和飛行試驗考核,獲取到了完整的全程飛行試驗數據。

    Abstract:

    In order to meet the requirements of large storage capacity, low bit error rate and reliable recovery in harsh environment in the field of reentry vehicle telemetry, and the shortcomings of traditional power supply and distribution mode, such as many ground equipment components, complex operation and low reliability, a low bit error rate digital telemetry system design method for reentry vehicle is proposed.The system adopts key technologies such as large capacity redundant backup storage design, low bit error rate design based on ECC error correction coding algorithm, high impact recovery protection design, etc., which improves storage capacity to 32GB,can continuously store 9h data, reduces bit error rate to 10-10, and realizes reliable recovery under high impact conditions; digital power supply and distribution technology based on 1553B bus, online fault diagnosis technology and other key technologies are adopted to simplify the ground test equipment and operation, save the development cost and improve the intelligence and testability of the aircraft. The system has been successfully applied to a certain reentry vehicle. It has passed the ground artillery test and flight test, and obtained complete flight test data.

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閆新峰,鄺浩欣,金文,蘇偉,王偉偉.再入飛行器低誤碼率數字化遙測系統設計計算機測量與控制[J].,2020,28(7):139-142.

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歷史
  • 收稿日期:2019-12-13
  • 最后修改日期:2020-05-19
  • 錄用日期:2020-01-13
  • 在線(xiàn)發(fā)布日期: 2020-07-14
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