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力限振動(dòng)試驗(yàn)力譜確定方法

Determination of force limits in spacecraft force limited vibration tests

  • 摘要: 文章從簡單模型出發(fā),介紹了力限控制技術(shù)中的表觀質(zhì)量、有效模態(tài)質(zhì)量和殘余質(zhì)量的基本概念以及常用的力譜確定方法。結(jié)合承力筒和某型號(hào)整星力限振動(dòng)試驗(yàn)研究的成果,指出現(xiàn)在使用的傳統(tǒng)的加速度控制方法可能存在過試驗(yàn)的問題,并提出在力限控制技術(shù)振動(dòng)試驗(yàn)中利用二自由度耦合分析方法確定力譜的思路,以期為今后國內(nèi)力限試驗(yàn)驗(yàn)證技術(shù)的深入開展提供參考。

     

    Abstract: Based on a simple model, this paper discusses some concepts of force limited control technology, including apparent mass, modal effective mass and residual mass, and the basic method of determining force limits. With the new research results concerning a center-tube and a satellite in the force limited vibration test, this paper pinpoints the problems of the traditional acceleration controlled method and presents new methods of determining force limits, which may serve as a reference for development of force limited methods in our country.

     

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