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Home > english-chinese > "analytical dynamics" in Chinese

Chinese translation for "analytical dynamics"

分析力学

Related Translations:
analytical language:  分析性语言
analytical cataloging:  分析编目
analytical journal:  多栏日记帐多栏式分录簿多栏式日记帐多栏式日记账
analytical quantity:  分解量
analytical radiochemistry:  分析放射化学
analytical statements:  分析表
analytical realism:  分析实在论
analytical system:  分析系统解的系统
analytical marxism:  分析型马克思主义
analytical toxicology:  毒理化验
Example Sentences:
1.Analytical dynamics of a kirchhoff elastic rod expressed in quasi - coordinates
弹性杆分析动力学的准坐标表达
2.Dimension - reduced semi - analytical dynamic programming approach for solving unit commitment problem
一种求解机组组合优化问题的降维半解析动态规划方法
3.Analytical dynamic model for planar adjustable five - bar linkages of alterable length and inertia of linkages
杆长和惯性参数可变的平面可调五杆机构的动力学解析模型
4.Analytical dynamic model for planar adjustable five - bar linkages , in which link lengths and the inertia parameters of links can be changed , was established based on kinematic analysis , kane dynamic equation and numeric - symbolic approach
基于运动分析、凯恩动力学方程和数字符号方法,首次建立了杆长和惯性参数可变的平面可调五杆机构的动力学解析模型。
5.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。
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