多体结构的英文

• multiple hull construction

• "多"英文翻译    many; much; more
• "体"英文翻译    body; part of the body
• "结构"英文翻译    structure; composition; cons ...
• "八面体结构" 英文翻译 :    octahedral structure
• "半胶体结构" 英文翻译 :    hemicolloid structure
• "包裹体结构" 英文翻译 :    inclusion texture
• "包体结构" 英文翻译 :    inclusion texture; inclusiontexture
• "船体结构" 英文翻译 :    hull construction; hull structure; hullconstruction; hullstructure; ship structure
• "船体结构钢" 英文翻译 :    hull-structural steel
• "船体结构图" 英文翻译 :    framing plan; shistructure graphing
• "磁晶体结构" 英文翻译 :    magnetic crystal structure
• "单体结构船" 英文翻译 :    monolithic ship
• "导体结构" 英文翻译 :    conductorconstruction
• "地体结构" 英文翻译 :    geotexture
• "多面体结构" 英文翻译 :    polyhedral structure
• "格体结构" 英文翻译 :    cellular construction
• "固溶体结构" 英文翻译 :    structure of solid solution
• "核糖体结构" 英文翻译 :    ribosome structure
• "简体结构" 英文翻译 :    frame with sidesway; tube structure
• "胶体结构" 英文翻译 :    colloform texture; gel texture
• "晶体结构" 英文翻译 :    crystal configuration; crystal morphology; crystal pattern; crystal place structure; crystal structure; crystal strucure; crystal sturcture; crystalline structure; crystallographic structure; crystallographic texture; crystalstructure; structure, crystalline
• "晶体结构学" 英文翻译 :    crystallology; structural crystallography; structural morphology
• "具体结构" 英文翻译 :    concrete structure
• "抗体结构" 英文翻译 :    antibody structure
• "壳体结构" 英文翻译 :    shell structure, shell construction

• Then similar human intelligent control method is selected to control movement of rolling base . in order to overcome modeling and control difficulty of flexible multibody structure , decentralized modeling method based on structural identification and decentralized predictive control is studied
  根据这个控制策略，分别系统地研究了中心刚体机动的仿人智能控制方法和柔性多体结构的分散预测控制方法，设计了具有组织级、协调级和执行级的组合结构振动主动控制器。
• Based on the requirements of high precision pointing / targeting of advanced spacecraft , dynamic modeling of spacecraft with flexible appendages bonded with piezoelectric sensors / actuators , attitude control and active vibration suppression theory are studied deeply in this dissertation , which is funded by the research fund for the doctoral program of higher education of china item ? “ large flexible multi - bodies structure spacecraft active vibration control technology ” ( 20050213010 ) . the main contents of this dissertation are as the follows : an approximate analytical dynamic model of a flexible spacecraft with surface bonded piezoelectric sensors and actuators is derived using hamilton ’ s principle with discretization by the assumed mode method . the model is then converted to state - space form for the purpose of control design
  本学位论文结合高等学校博士学科点专项科研基金“挠性多体结构卫星主动振动控制技术研究” ( 20050213010 )课题,从理论上对粘贴有压电智能元件的挠性航天器的建模、姿态控制和主动振动控制理论等展开了深入的研究,其研究内容主要包括以下几个方面:利用hamilton原理推导了挠性航天器的动力学模型、压电元件的作动方程及检测方程,并采用模态分析方法,进一步将挠性航天器的耦合方程规范化,使之适应于姿态控制系统的分析和设计。