哈尔滨工程大学学报
哈爾濱工程大學學報
합이빈공정대학학보
JOURNAL OF HARBIN ENGINEERING UNIVERSITY
2014年
11期
1422-1426
,共5页
皮阳军%王骥%胡玉梅
皮暘軍%王驥%鬍玉梅
피양군%왕기%호옥매
并联六自由度机构%结构参数%标定方法%标定精度%关节空间%动力学标定%运动学标定
併聯六自由度機構%結構參數%標定方法%標定精度%關節空間%動力學標定%運動學標定
병련륙자유도궤구%결구삼수%표정방법%표정정도%관절공간%동역학표정%운동학표정
6-DOF parallel mechanism%structural parameter%calibration method%calibration accuracy%joint spac-ing%dynamic calibration%kinematic calibration
为了研究并联六自由度机构不同标定方法的适用性,依据运动学标定和动力学标定,分别建立了并联六自由度机构的标定模型,并通过数值仿真对标定效果进行对比分析。结果表明:运动学标定方法对提高机构运动正解精度更为有效,正解误差比动力学标定的结果小4.9%,有利于传统的基于关节空间的并联机构控制策略;动力学标定方法对提高机构动力学模型精度更为有效,关节驱动力误差比运动学标定的结果小5~25 N,更适合基于工作空间的并联机构控制策略。
為瞭研究併聯六自由度機構不同標定方法的適用性,依據運動學標定和動力學標定,分彆建立瞭併聯六自由度機構的標定模型,併通過數值倣真對標定效果進行對比分析。結果錶明:運動學標定方法對提高機構運動正解精度更為有效,正解誤差比動力學標定的結果小4.9%,有利于傳統的基于關節空間的併聯機構控製策略;動力學標定方法對提高機構動力學模型精度更為有效,關節驅動力誤差比運動學標定的結果小5~25 N,更適閤基于工作空間的併聯機構控製策略。
위료연구병련륙자유도궤구불동표정방법적괄용성,의거운동학표정화동역학표정,분별건립료병련륙자유도궤구적표정모형,병통과수치방진대표정효과진행대비분석。결과표명:운동학표정방법대제고궤구운동정해정도경위유효,정해오차비동역학표정적결과소4.9%,유리우전통적기우관절공간적병련궤구공제책략;동역학표정방법대제고궤구동역학모형정도경위유효,관절구동력오차비운동학표정적결과소5~25 N,경괄합기우공작공간적병련궤구공제책략。
In order to study the usability of different calibration methods for the 6-DOF ( six degrees of freedom) parallel mechanism, calibration models of the mechanism were established on the basis of kinematic and the dynam-ic calibrations.The comparative analyses of kinematic and the dynamic calibrations were done by the numerical sim-ulation .The results showed that the kinematic calibration is more effective in improving forward solution precision of the mechanism.It is also shown that the forward solution error is 4.9%less than that of the dynamic calibration, which is beneficial to the conventional joint-space control of parallel mechanism.The dynamic calibration is more effective in improving dynamic model precision of the mechanism and joint force error is 5~25 N less than that of the kinematic calibration, which is suitable for the task-space control strategy of parallel mechanism.