有必要研究简单而有效的控制律控制其混沌现象。
The chaotic behavior of PMSM are controlled by partial linearization control.
趋近律控制是滑模控制的一种设计方法，目前被广泛应用于模型不确定、参数波动范围大或外界干扰强的控制系统中。
Reaching Law Control(RLC) is an approach to Sliding Mode Control (SMC) design which is widely applied in the presence of model uncertainties, parameter fluctuations and external disturbances now.
模型将东亚大陆限定在一梯形边界框架之中，大陆岩石层被视为由幂指数律控制的薄层，它上伏在粘滞性较低的软流层之上蠕变流动。
In this model the EastAsia continent is limited in a trapezoid geological frame and the continental lithosphere is regard as a continuum thin plate with a power law rheology.
律所也往往认为节流较之开源无足重轻，到事后才考虑成本控制问题。
Cost control is often an afterthought, trailing far behind revenue generation.
大臣们打算在下月发布英国第一份碳预算时拉开架势引入严格的联合王国控制碳污染的条律。
Ministers are poised to introduce strict limits on UK carbon pollution when they announce Britain's first carbon budget next month.
对一类同时具有状态时滞和输入时滞的不确定离散时滞系统，提出保性能状态时滞反馈控制律的设计问题。
For uncertain discrete-Time-delay systems with both state and input delays, this paper addresses the problem of designing an guaranteed cost state feedback time-delay controller.
对于攻击地面固定目标的飞行器，提出一种非线性制导律和控制方法。
A nonlinear guidance law and control strategy is proposed for aircraft applying to attack the ground fixed targets.
在单框架控制力矩陀螺（SGCMG）系统操纵律的设计中，如果考虑框架伺服特性，往往假设系统的物理参数是确切已知的。
Physical parameters of single gimbal control moment gyroscopes(SGCMGs) are often assumed to be known exactly when steering law is designed by taking gimbal servo characteristics into account.
然后将方法1和方法2分别应用于该模型，得出两种多机系统励磁的非线性L_2增益干扰抑制控制律。
Method 1 and method 2 are applied to the constructed nonlinear model, and then two nonlinear L2 gain disturbance attenuation control laws for multi-machine excitation are deduced.
为研究具有大离轴角及越肩发射能力的先进空空导弹初始段敏捷转弯方法，研究了装有反作用喷气控制系统的空空导弹的大角度姿态过失速机动控制律。
This paper investigates the large Angle attitude post stall maneuver control for the agile turn phase of an air-to-air missile that has high off-boresight capability and head reverse maneuverability.
在单框架控制力矩陀螺(SGCMG)系统操纵律的设计中，如果考虑框架伺服特性，往往假设系统的物理参数是确切已知的。
Physical parameters of Single gimbal Control Moment Gyroscopes (SGCMGs) are often assumed to be known exactly when steering law is designed taking gimbal servo characteristics into account.
可以在实验室完成对模型系统的控制实验，进行控制律的研究。
We can complete its control experiments in the laboratory, and do research on control rules.
在单框架控制力矩陀螺(SGCMG)系统操纵律的设计中，通常假定框架伺服系统具有理想的伺服跟踪性能。
Gimbal servo systems of single gimbal control moment gyroscopes (SGCMGs) are often assumed to have ideal tracking performance during the steering law design.
文中对带有自动驾驶仪飞机投弹的稳定性进行了分析，对其过程进行了仿真研究和控制律优化设计。
The paper analyses the launching missiles stability of aircraft with auto-flight system, and simulates the process of launching and optimizes the control law of the auto-flight system.
两种控制律不需要知道系统参数，对模型误差具有鲁棒性。
Both control laws do not require the knowledge of the system parameters and are robust to modeling errors.
从而将两点边值问题解序列的有限次迭代结果作为系统的次优控制律。
Some finite iterative result of the two-point boundary value problem sequence is taken as a suboptimal control law of the system.
取补偿项序列的有限次迭代值，获得次优控制律。
By taking a finite - time iteration of the compensation sequence, a suboptimal control law is obtained.
并证明了该最优输出反馈控制律可使网络控制系统均方指数稳定。
The paper proves that optimal controllers can stabilize the exponentially mean square of networked control systems.
使用符号运算方法设计了系统闭环控制律和大攻角下的过失速控制律。
The control laws of the inner closed loop system and post stall maneuver are obtained through using symbol operations design.
通过控制方程的相似律分析，可预言混合对流传热由阿基米德数和几何因子控制。
With similarity considerations on governing equations, the heat transfer of mixed convection can be predicted to be controlled by Archimedes number and geometric factors.
综述了单框架控制力矩陀螺(SGCMG)系统操纵律研究概况，并对现存操纵律的性能进行了评价。
A survey of steering laws for Single Gimbal Control Moment Gyroscope (SGCMG) systems is made. Meanwhile, steering performance of the art is appreciated.
然后利用灵敏度法推导出了该系统的最优跟踪控制律。
Then, the optimal tracking control law of this system was deduced through the sensitivity approach.
并用对偶方法刻画了最优控制律的特征。
By duality approach, we characterize the optimal control law.
利用动态逆方法设计了快子系统控制律。
The slow subsystem control law is designed by Lyapunov method.
推导了自适应控制律与相应的约束条件。
The adaptive control laws and constrain conditions are derived out.
给出了最优控制律的存在唯一性条件，并提出了最优控制律的设计算法。
The conditions of existence and uniqueness of the optimal control law is given and an algorithm of solving the optimal control law is proposed.
对两种不同控制律下变刚度半主动控制结构的地震影响系数进行了比较和分析。
Seismic influence coefficients of structures with active variable stiffness (AVS) systems, corresponding to two different control laws, are compared and analyzed.
对两种不同控制律下变刚度半主动控制结构的地震影响系数进行了比较和分析。
Seismic influence coefficients of structures with active variable stiffness (AVS) systems, corresponding to two different control laws, are compared and analyzed.
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