宇航计测技术 ›› 2020, Vol. 40 ›› Issue (2): 81-84.doi: 10.12060/j.issn.1000-7202.2020.02.15

• 计量综合管理 • 上一篇    下一篇

某拖缆长度测量结构改进方法研究

李红泉   

  1. 中国人民解放军92419部队,辽宁 125106
  • 出版日期:2020-04-25 发布日期:2022-03-05
  • 作者简介:李红泉(1969-),男,硕士,高级工程师,主要研究方向:飞行器设计和使用。

Research on Structure Improvement Method for a Towing Length Measurement

LI Hong-quan   

  1. 92419 Unit of PLA,Liaoning 125106,China
  • Online:2020-04-25 Published:2022-03-05

摘要: 拖缆放出长度是拖靶飞行的重要参数,测长过程一旦发生故障势必造成严重后果。针对长度计数间断现象,从长度测量装置的结构原理、空中受力和飞行过程分析了计数错误原因,提出了结构改进方法和飞行机动航路要求,以实际应用验证了解决措施的有效性。

关键词: 拖靶系统, 长度测量, 结构改进, 飞行试验

Abstract: Towing released length is an important parameter for a certain towing flight, if a failure occurs in measuring procedure, it will cause serious consequences. Aiming at the length counting loss phenomenon, the reasons of counting error are analyzed, from the structure principle, air force and flight process of the length measuring device. The structural improvement method and flight maneuvering route requirements are proposed. The effectiveness of the resolutions is verified by the actual flight.

Key words: Tow target system, Length measurement, Structure improvement, Flight test

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