A method named the PI decoupling control of a tandem cold mill based on a linearized model is presented. Results of simulation show that the method is available.
文中提出了一种基于线性化模型的冷连轧机pi解耦控制方案，仿真结果证明该方法的有效性。
A design for nonlinear excitation controller using an input-output feedback linearized model of the power system is presented. The controller design is independent of operating points.
介绍使用电力系统输入-输出反馈线性化模型的非线性励磁控制器的设计，该控制器的设计与运行点无关。
The engine mathematical model in the simulation system is obtained by approximation of testing data of an actual engine with a series of small deviation and linearized models.
仿真系统中的发动机数学模型是用一系列小偏差线化模型去逼进某一实际发动机的试车数据而得到的。
A new approach of compensating linearized model errors by the fictitious time-varying noise statistics is proposed.
作者提出了用虚拟时变噪声统计，补偿线性化模型误差的新思想。
The vertical propagating process and evolutive characteristics of planetary waves forced by topography are investigated by a global linearized primitive equation model.
本文用线性化全球原始方程谱模式来研究地形强迫行星波的垂直传播过程及演变特征。
Firstly, the original nonlinear model of the aircraft longitudinal motion is linearized to a three-order decoupling system via the input-output feedback technique.
首先，对飞机纵向运动的非线性模型进行输入输出反馈线性化，将其等效为一个三阶线性系统，并同时实现了解耦。
A linearized mathematical model for the developed triplex redundance servo control system is derived on the basis of its mechanism analysis.
对研究的三余度伺服控制系统的机理进行分析，建立了被控对象的线性化数学模型。
The equations of couple rotor fuselage are linearized . An example is given and this paper provides a new model for analysis of coupled rotor fuselage dynamics.
同时作线性处理，计算一个简单模型的固有频率，为旋翼与机身藕合系统的振动特性和响应分析提供一种新模型。
The technique was applied to a simulated model of a boom crane slewing at a constant luff Angle while reeling in the cable and linearized around the payload equilibrium position.
传送时间由叠代减到最小技术被申请了于旋转在一个恒定的逆风行驶角度的景气起重机的一个被模仿的模型，当卷在缆绳时并且在酬载平衡位置附近线性化了。
The linearized atmospheric equation system is solved analytically to obtain a theoretical model of the urban heat island circulation.
文中根据线性化的大气方程组求得了城市热岛环流的理论模式。
Thus, the perturbation model is updated in a batch-wise manner. After completion of each batch, a batch-wise perturbation model is identified linearized around the control trajectory for that batch.
每完成一个批次就利用新得到的数据对模型进行更新，该更新的模型也是在前一批次的控制轨迹基础上进行线性化得到的。
Thus by nonlinear state transformation and nonlinear state feedback, the original 6 order nonlinear attitude model of a spacecraft is partially precisely linearized into a 2 order linear system.
这样通过非线性状态变换和非线性状态反馈，将飞行器原来的6阶非线性姿态模型部分精确线性化为二阶线性系统。
Based on the feedback linearized model, a robust adaptive control method is presented.
针对反馈线性化后的不确定非线性对象，提出了一种鲁棒自适应控制方法。
Based on the feedback linearized model, a robust adaptive control method is presented.
针对反馈线性化后的不确定非线性对象，提出了一种鲁棒自适应控制方法。
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