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基于LabWindows/CVI的導彈舵機測控系統設計
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北京航空航天大學(xué) 機械工程及自動(dòng)化學(xué)院,北京航空航天大學(xué) 機械工程及自動(dòng)化學(xué)院

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TP274

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Design of the Measuring and Controlling system for Missile Actuator Based on LabWindows/CVI
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School of Mechanical Engineering and Automation, Beihang University,

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    摘要:

    舵機是導彈控制系統的重要執行機構,為實(shí)現對電動(dòng)及氣動(dòng)多種型號導彈舵機性能的測試,設計開(kāi)發(fā)了一種基于LabWindows/CVI虛擬儀器的測控系統。介紹了該測控系統硬件組成和軟件結構流程,軟件設計過(guò)程中充分利用多線(xiàn)程、數據庫等技術(shù),準確快速完成舵機自動(dòng)化性能測試。應用結果表明:該舵機測控系統工作穩定,測試精度和自動(dòng)化程度高,滿(mǎn)足舵機試驗測試精度和技術(shù)指標要求,為舵機的性能研究和維修維護提供了良好的測試環(huán)境。

    Abstract:

    It is about a measurement and control system based on virtual instrument development platform of LabWindows/CVI, thus establishing a universal missile steering gear performance test platform for performance test both in idle-loading and loading of various steering gears including electric actuator and pneumatic actuator, which are used in missile as vital actuator of control system. In this paper,the composition of hardware structure and the software flow of the testing and controlling system for missile actuator are introduced. The dynamic link library, database, multi thread technology and so on are used in the process of software designing. By application of these techniques, performance test for steering gears could be completed accurately and rapidly. The result of application showed that this measurement and control system has features of stable working, high testing precision, strong commonality, fully automation, easy extended, meeting the requirements of steering engine test accuracy and technical specifications, thus providing a good test environment for performance research and design improvement of steering engine.

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陳娟,張建.基于LabWindows/CVI的導彈舵機測控系統設計計算機測量與控制[J].,2017,25(6):18.

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  • 收稿日期:2016-11-15
  • 最后修改日期:2017-01-13
  • 錄用日期:2017-01-13
  • 在線(xiàn)發(fā)布日期: 2017-07-18
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