并以法向过载控制模态为例，将线性二次型运用到飞行控制系统的控制律设计中。
The LQ is adapted to the flight control law design such as the Normal Acceleration control system.
因在由控制模态方程推导时滞最优控制律的过程中无近似处理，所给控制方法易于保证控制系统的稳定性。
Since no approximation is made in the derivation of the time-delay optimal controller from the mode-controlled equation, the system stability is easy to guarantee.
用该综合方法对某型飞机的侧向直接力控制模态(航向指向)进行了分析与设计，并将其与动态逆方法进行了比较。
The design and simulation of the yaw pointing mode dynamic decoupling fuzzy control system for an aircraft are studied in this paper.
提出了非线性空间飞行器系统采用滑动模态控制方法，它对强非线性的空间飞行器系统通道间交叉影响进行解耦。
A control method with sliding mode of nonlinear spacecraft system is provided in this paper, in which the interactive influences among channels of strong nonlinear spacecraft system are decoupled.
验证了稳定平台控制系统对于变结构控制的不变性条件，构造了滑动模态。
The invariant conditions of the stabilized platform control system for variable structure control were verified and a sliding mode was constructed.
为什么一个简单的模态视图控制器滞后时，解雇了吗？
Why would a simple modal view controller lag when presented and dismissed?
采用编译控制的译码方法，具体分析了译码的数据处理流程，介绍了模态指令处理等相关问题。
The way of compiling control coding is adopted, and coding data process flow is analyzed detailed, while some relevant problems such as modal instrument procession are introduced.
另外，密集模态挠性结构模型容易受到环境和结构参数变化的影响，导致控制器的失效。
In addition, flexible structures with close modes can be easily influenced by the environment and changes of structures parameters, which may disable the controller.
讨论了亏损系统模态控制的设计方法，并将其应用在飞机机翼颤振的控制问题中。
A modal controller design of defective system was presented, and it was applied in the flutter control problem of an airfoil.
为了提高天地景投影伺服系统的性能指标，对伺服系统的多模态控制算法进行了改进。
In order to improve the performance of a servo system for background projection system, its multi mode control algorithm is modified.
本文讨论了非线性变结构控制系统的综合问题，提出了滑动模态补偿器的概念。
In this paper, nonlinear variable structure control systems are considered, and a dynamic sliding mode compensator is proposed.
本文提出将多模态仿人智能控制应用于陀螺罗经的启动过程。
This paper provided the application of simulating human intelligent control multi-mode IC control to the starting process of the electronic magnetic controlled gyrocompass.
考虑的具体方法是将PD反馈波控制与基于极点配置法设计的模态控制相结合。
The particular approach considered is that of collocated, PD feedback wave control combined with modal control designed using pole placement.
提出了基于极点配置的混沌滑动模态控制方法。
The sliding mode control method for chaotic systems based on pole-replacement is presented.
介绍了大型卧螺机自动控制及模态分析诊断系统，它包括了控制逻辑的实现、完备的数据监测和报警等功能。
This paper introduces the automatic control and modal analysis diagnostic system of a large horizontal snail machine. It includes the realization of control logic, data monitor and alarm functions.
变结构控制作为控制系统的一种综合方法，它的滑动模态具有不变性，这是变结构控制在导弹姿态控制中最突出的优点。
As a synthesis method in control system, the sliding mode of variable structure control is invariable, and which is its most excellent advantage in the missile attitude control system.
使用等价控制方法构成双线性变结构控制系统的滑动模态方程。
Equations of sliding mode for bilinear variable structure control system are structured by employing method of equivalent control.
该方法首先利用平衡降阶法对结构进行降阶，然后在模态空间中采用LQG控制策略对结构进行控制；
The model reduction is first carried out by balanced reduction method, then LQG control strategy is used in modal space for control design.
结果表明，按滚转角对飞机进行反馈控制时，不能使该不稳定模态变为稳定模态。
The result shows that the unstable mode could not be changed into a stable one by using the bank Angle feedback control.
小角度调转时用反向开方代替饱和控制的三模态控制。
When the Angle is small, the saturation control is replaced by the reverse square root control.
在对建筑物采用柔性技术的基础上，本文提出了一种与之相适应的模态控制分析方法。
On the basis of adopting the flexible control technology in buildings, in this paper, we brought forward a simplified model analysis method which could be easily used in active control technology.
采用模态分析及控制理论，确定了定量度量模态对贮存在结构中能量积分贡献的方法。
By using mode analysis theory and control theory, a method is proposed to measure the modes contribution to the integrated energy of the system.
该算法可普遍应用于多回路控制律选参问题的求解，对SR-61悬停模态控制律设计的算例显示了它的直观和有效。
The given algorithm can be used easily to choose coefficients for control law with multi-loop configuration, and a design example with SR-61 hover model shows its convenience and effectiveness.
模型用带扰动观测器补偿的滑模变结构控制，对控制函数切换并受滑动模态控制。
Owing to applying the model of sliding mode variable-structure control that has compensation of disturbance monitor, switching control function was controlled by sliding mode.
对一般非线性系统，推导了一种综合运用非线性动态逆、自适应模糊逻辑系统和滑动模态控制进行控制律设计的方法。
For general nonlinear system, a control law design method which integrated the nonlinear dynamic inverse theory, adaptive fuzzy system and slide model control is developed.
提出了机、电、声三相耦合的噪声智能控制系统的模态控制方法，给出了模态控制器的设计方案。
A modal control method and controller design scheme for intelligent mechanically electrically acoustically coupled noise control system is proposed.
用该方法对某主动控制飞机的垂直平移模态（直接力控制）进行了解耦设计，并将其应用于飞机的阵风减缓。
As a numerical example, we used our method to design the vertical transition mode(direct lift control) of a certain active-control aircraft for gust alleviation.
这种控制方式既保留了传统的滑动模态控制的优点，又解决了高频抖动的问题，同时也提高了控制的鲁棒性。
This control method retains the positive properties of conventional sliding modecontrol. and solves the problem of high frequency shiver. as well as increases the robustness of the controller.
与油阻尼器被动控制相比，MR半主动控制可以有效地提高模态阻尼比，尤其在阻尼器位置距索端很近时仍有较好的控制效果。
However, the control efficiency of the MR semi-active control compared with that of the oil-dampers control is better, especially when the damper position is close to the end of the cable.
与油阻尼器被动控制相比，MR半主动控制可以有效地提高模态阻尼比，尤其在阻尼器位置距索端很近时仍有较好的控制效果。
However, the control efficiency of the MR semi-active control compared with that of the oil-dampers control is better, especially when the damper position is close to the end of the cable.
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