线性状态的英文

• linear conditions

• "线性"英文翻译    linear; linearity
• "状态"英文翻译    status; state; condition; st ...
• "非线性状态" 英文翻译 :    nonlinear behaviour
• "非线性弹性状态" 英文翻译 :    nonlinear elastic behavior
• "性状态" 英文翻译 :    sexual state
• "半塑性状态" 英文翻译 :    semi plastic stage; semi-plastic state
• "变性状态" 英文翻译 :    denatured state
• "变应性状态" 英文翻译 :    allergic state
• "超弹性状态" 英文翻译 :    extraspring temper
• "磁性状态" 英文翻译 :    magneticalness
• "磁中性状态" 英文翻译 :    magnetic neutral state
• "脆性状态" 英文翻译 :    brittle state
• "弹塑性状态" 英文翻译 :    elastic plastic behavior; elasticoplastc be-havior; elastoplastic state
• "弹性状态" 英文翻译 :    elastic condition; elastic stage; elastic state; elaxtic state
• "弹粘性状态" 英文翻译 :    elasticoviscous behavior
• "动弹性状态" 英文翻译 :    dynamic elastic behaviour
• "非弹性状态" 英文翻译 :    inelastic behavior; inelastic state
• "非负性状态" 英文翻译 :    nonnegativity conditions
• "刚性状态" 英文翻译 :    hard mode
• "活性状态" 英文翻译 :    active condition; active state
• "静性状态" 英文翻译 :    aplanetism
• "可塑性状态" 英文翻译 :    plastic state
• "两性状态" 英文翻译 :    bisexual state
• "塑性状态" 英文翻译 :    condition of plasticity; plastic stage; plastic state; plasticstate
• "特应性状态" 英文翻译 :    atopic state; atopic status

• On the basis of that , linear state feedback control law is designed to ensure the stability and security of power system
  在此基础上，设计线性状态反馈控制规律，使得电力系统的运动状态保持稳定。
• From the simulation , we can get some parameter curves of landing gear . by analyzing these curves and the methods with two - masses model , the linear state equation of landing gear during landing process was established
  基于参数曲线分析和二质量模型建立了起落架着陆的线性状态方程,应用现代控制理论对方程进行分析并结合matlab软件对其进行着陆动态仿真。
• On the basis of the mathematic model , the controllability and observeability are analyzed , several kinds of controller including linear states feedback controller , pid controller , p - fuzzy - pi controller , balance method controller are designed for the system
  在此基础上，分析了系统的能控性和能观性，对磁悬浮系统设计了线性状态反馈控制器、 pid控制器、 p - fuzzy - pi控制器和平衡法控制器。
• Based on lyapunov stability theorem and lmis approach , a control profile , including both static state feedback control and dynamic output feedback control , is presented for norm - bounded uncertain discrete - time linear systems with actuator sector nonlinearity ; 2
  以线性矩阵不等式方法为带有扇形饱和非线性执行器的范数有界时变不确定离散线性系统设计线性状态反馈控制器和线性动态输出反馈控制器； 2
• 3 . investigated the direct model construction method of unsteady aerodynamics state space equation from volterra kernels , including linear state space model and bilinear state space model . the general model construction method for ase was brought forward
  研究了基于volterra核直接建立非定常气动力状态空间模型的方法，包括线性状态空间模型和双线性状态空间模型，并提出了将其用于ase系统建模的一般方法。
• On the basis of the mathematic model , the controllability and observeability are analyzed , several kinds of controller including linear states feedback controller , pid controller , linear quadratic optimal controller , neural network pid controller are designed for the system
  在此基础上，分析了系统的能控性和能观性，对磁悬浮系统设计了线性状态反馈控制器、 pid控制器、线性二次型最优控制器和神经网络pid控制器。
• In view of chaotic systems composed of a sum of a linear and nonlinear part , a compensative control method using radial basis function networks is proposed , the rbf networks trained can eliminate the nonlinear part of the chaotic system , the resulting system is dominated by the linear part
  然后针对大多数混沌非线性系统由线性函数和非线性函数两部分构成的特点，用rbf网络补偿系统非线性部分，使原系统变成近似线性系统，再结合线性状态反馈控制技术，对lorenz方程和duffing振子进行了非线性补偿控制。
• The second part of the thesis includes a derivation of reduced order models for the activated sludge process . firstly , the paper introduces the derivation of time - varying linear state - space models for the anoxic part and the aerobic part . secondly , by integrating the anoxic part model with the aerobic part model , we can get the resulting models - a time - varying bilinear state - space model for the activated sludge prenitrification system
  为了控制应用的需要，本文首先分别建立了缺氧池和好氧池的时变线性状态空间模型，然后把好氧池和缺氧池的时变线性状态空间模型结合起来得到由缺氧和好氧两部份构成的前硝化活性污泥系统的时变双线性模型，最后简单描述了理想状态下沉淀池的模型。
• Based on the state equations , the optimal control law is obtained . then the predictive controller based on nonlinear state equations is discussed . in chapter 6 , fast algorithm of predictive control and the analyse of the simulation system , and the parameters of the gpc controller is discussed in the matlab
  在分析了pmsm系统单变量carima模型后，进行了pmsm线性状态方程的多变量预测控制的研究，分析pmsm的微分方程组，在此基础上，推导出给定性能指标下，基于线性状态方程的多变量预测控制律。
• The paper mainly discussed and analyzed aircraft landing gear using model reference adaptive control and mcs ( minimal control synthesis algorithm ) , built up the mathematics model and linear state equations of aircraft landing gear during the landing and taxiing and analyzed the virtues of model reference adaptive and minimal control synthesis algorithm
  本论文主要是采用模型参考自适应和最小控制综合算法( minimalcontrolsynthesisalgorithm )来描述飞机起落架系统,建立了完整的起落架着陆滑跑的数学模型和线性状态控制方程,分析了模型参考自适应和最小控制综合算法的优点。