隧道建设
隧道建設
수도건설
TUNNEL CONSTRUCTION
2014年
7期
608-613
,共6页
龚国芳%洪开荣%周天宇%侯典清%王林涛
龔國芳%洪開榮%週天宇%侯典清%王林濤
공국방%홍개영%주천우%후전청%왕림도
盾构%掘进姿态控制%模糊PID%推进液压系统
盾構%掘進姿態控製%模糊PID%推進液壓繫統
순구%굴진자태공제%모호PID%추진액압계통
shield%attitude control%fuzzy PID%thrust hydraulic system
针对盾构掘进过程中姿态主要依赖操作人员施工经验手工调整、掘进轨迹精度主要依赖人员熟练性的情况,提出基于双闭环反馈自动控制盾构掘进轨迹的方法,通过主反馈实现掘进斜度的实时更新,局部反馈实现液压缸的速度控制。分析表明,局部反馈精度决定了预调偏差大小,在掘进轨迹控制中至为关键,因此以球铰支撑推进系统为例分析单环掘进前后液压缸的几何关系,推导左右推进液压缸速度关于掘进斜度、掘进速度的数学解析式,采用AMESim和MATLAB联合仿真工具搭建了推进速度控制的模糊PID模型,仿真分析非均载荷下推进液压缸的速度控制,并以盾构模拟推进试验台为例进行推进速度控制试验。结果表明:基于模糊PID控制策略的推进液压缸速度控制可实现较准确的盾构掘进轨迹,为盾构失准问题的进一步解决提供了理论基础和现实依据。
針對盾構掘進過程中姿態主要依賴操作人員施工經驗手工調整、掘進軌跡精度主要依賴人員熟練性的情況,提齣基于雙閉環反饋自動控製盾構掘進軌跡的方法,通過主反饋實現掘進斜度的實時更新,跼部反饋實現液壓缸的速度控製。分析錶明,跼部反饋精度決定瞭預調偏差大小,在掘進軌跡控製中至為關鍵,因此以毬鉸支撐推進繫統為例分析單環掘進前後液壓缸的幾何關繫,推導左右推進液壓缸速度關于掘進斜度、掘進速度的數學解析式,採用AMESim和MATLAB聯閤倣真工具搭建瞭推進速度控製的模糊PID模型,倣真分析非均載荷下推進液壓缸的速度控製,併以盾構模擬推進試驗檯為例進行推進速度控製試驗。結果錶明:基于模糊PID控製策略的推進液壓缸速度控製可實現較準確的盾構掘進軌跡,為盾構失準問題的進一步解決提供瞭理論基礎和現實依據。
침대순구굴진과정중자태주요의뢰조작인원시공경험수공조정、굴진궤적정도주요의뢰인원숙련성적정황,제출기우쌍폐배반궤자동공제순구굴진궤적적방법,통과주반궤실현굴진사도적실시경신,국부반궤실현액압항적속도공제。분석표명,국부반궤정도결정료예조편차대소,재굴진궤적공제중지위관건,인차이구교지탱추진계통위례분석단배굴진전후액압항적궤하관계,추도좌우추진액압항속도관우굴진사도、굴진속도적수학해석식,채용AMESim화MATLAB연합방진공구탑건료추진속도공제적모호PID모형,방진분석비균재하하추진액압항적속도공제,병이순구모의추진시험태위례진행추진속도공제시험。결과표명:기우모호PID공제책략적추진액압항속도공제가실현교준학적순구굴진궤적,위순구실준문제적진일보해결제공료이론기출화현실의거。
Considering the fact that the attitude of shield during the boring process is mainly controlled by manual adjustment according to personal experience and that the precision of shield boring trajectory mainly depends on personal proficiency,the authors propose the automatic shield attitude control method based on dual closed-loop feedback.The automatic shield attitude control method proposed contains a main-loop feedback that updates the tunneling trajectory and a local feedback that controls the velocity of the thrust cylinders.Succedent analysis shows that the local-feedback control is crucial.Therefore,the authors analyze the geometric relation of hydraulic cylinders before and after one-ring boring based on a spherical-hinge support thrust system,and deduce the mathematical expression of shield attitude and velocity of thrust cylinders on the left and right sides.The authors achieve the simulation of the velocity control system based on fuzzy PID by using AMEsim and MATLAB software,and make the corresponding test based on a thrust simulation test rig.The result indicates that accurate shield attitude can be realized by fuzzy PID control strategy.The paper provides the theoretical foundation and practical basis for further solution of the shield misalignment problem.