同济大学学报(自然科学版)
同濟大學學報(自然科學版)
동제대학학보(자연과학판)
JOURNAL OF TONGJI UNIVERSITY(NATURAL SCIENCE)
2009年
11期
1423-1427
,共5页
结构振动控制%密频结构%可控性%摄动法
結構振動控製%密頻結構%可控性%攝動法
결구진동공제%밀빈결구%가공성%섭동법
structure vibration control%structure with closelyspaced natural frequencies%controllability%perturbation method
为研究密频结构频率密集度对结构可控性的影响,针对3自由度的密频结构,从结构基本振动方程入手,采用摄动分析方法推导了闭环系统频率、阻尼比和摄动量的相关方程.在速度反馈和状态反馈情况下,讨论了结构频率密集度对结构可控性的影响,并对不确定参数对结构模态阻尼比的影响进行了分析.分析结果表明,对于采用速度反馈、位移反馈的闭环系统,随着结构频率密集度参数的减小,结构的部分模态阻尼比逐渐趋向于零,相应的结构模态趋于不可控.考虑了结构刚度和质量参数不确定性对密频结构可控性的影响,结果表明参数不确定性会影响密频结构不同模态之间的耦合程度,进而改变结构的可控度.
為研究密頻結構頻率密集度對結構可控性的影響,針對3自由度的密頻結構,從結構基本振動方程入手,採用攝動分析方法推導瞭閉環繫統頻率、阻尼比和攝動量的相關方程.在速度反饋和狀態反饋情況下,討論瞭結構頻率密集度對結構可控性的影響,併對不確定參數對結構模態阻尼比的影響進行瞭分析.分析結果錶明,對于採用速度反饋、位移反饋的閉環繫統,隨著結構頻率密集度參數的減小,結構的部分模態阻尼比逐漸趨嚮于零,相應的結構模態趨于不可控.攷慮瞭結構剛度和質量參數不確定性對密頻結構可控性的影響,結果錶明參數不確定性會影響密頻結構不同模態之間的耦閤程度,進而改變結構的可控度.
위연구밀빈결구빈솔밀집도대결구가공성적영향,침대3자유도적밀빈결구,종결구기본진동방정입수,채용섭동분석방법추도료폐배계통빈솔、조니비화섭동량적상관방정.재속도반궤화상태반궤정황하,토론료결구빈솔밀집도대결구가공성적영향,병대불학정삼수대결구모태조니비적영향진행료분석.분석결과표명,대우채용속도반궤、위이반궤적폐배계통,수착결구빈솔밀집도삼수적감소,결구적부분모태조니비축점추향우령,상응적결구모태추우불가공.고필료결구강도화질량삼수불학정성대밀빈결구가공성적영향,결과표명삼수불학정성회영향밀빈결구불동모태지간적우합정도,진이개변결구적가공도.
An investigation was made into the influence of frequency intensity on the controllability of structures with closely-spaced natural frequencies. The perturbation equations were established for a closed-loop system to study the relationship of frequencies,modal damping ratios and perturbation parameters.The analysis focused on a three-degree-freedom structure with closely spaced natural frequencies. The velocity and displacement feedbacks were considered in the calculation. Several cases with velocity feedback and state feedback were considered. And the preciseness of perturbation methods was checked. The calculation results show that the damping ratios of two modes are decreasing with the decreasing of intensity parameter values of the structure with closely spaced natural frequencies, indicating that the controllability of corresponding modes is diminishing. The uncertainties in mass and stiffness matrices were also discussed in this paper. The calculation results show that the degrees of mode coupling will change due to the structural uncertainties and the controllability will be influenced subsequently.