• By using the method of quasi-sliding mode, the variable structure control law for lane keeping was designed.

    采用准滑模控制方法,设计车道保持变结构控制规律;

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  • The sufficient conditions of sliding mode mean stability are given, and the variable structure control law can guarantee the sliding mode to have reachability.

    文中给出了滑动模均方稳定的充分条件,所设计的变结构控制律能够保证滑动模具有可达性。

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  • Under certain conditions, the designed variable structure control law makes the sliding mode along a specified sliding manifold invariable to the system perturbation and external disturbances.

    在一定条件下,设计的滑动模控制律使得系统沿预先设计的滑动流形的滑动运动对系统的参数摄动和外干扰具有不变性。

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  • Parameter of optimized trajectory and variable structure with sliding modes control theorem are used to construct sliding surface, obtain a new tracking trajectory guidance law.

    利用基准优化弹道参数和滑模控制思想,构造滑动面,提出了一种新的弹道跟踪制导规律。

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  • A new approach in the design of discrete-time variable structure control is presented based on the reaching law approach.

    研究基于离散趋近律方法的变结构控制设计问题,提出一种新型的离散趋近律。

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  • A turbo generator coordinated controller is designed by control law with self adjusting factor based on the theory of variable structure control and the fuzzy control.

    以变结构控制理论为基础,利用模糊控制理论设计了带自调整因子的控制规律,用于设计汽轮发电机组的综合控制器。

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  • Fuzzy logic rules are introduced to adjust approaching law adaptively, and the guidance is designed by applying variable structure control theory.

    应用变结构控制理论,引入模糊规则自适应地调整趋近律,设计了制导律。

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  • For the sake of the tyre works under optimal slip ratio, a braking variable structure control (VSC) law based on slip ratio control was introduced so as to obtain the maximum friction coefficient.

    飞机防滑刹车控制的关键是控制机轮的滑移率,为了使机轮工作在最佳滑移率,得到最大结合系数,提出了一种基于滑移率控制的防滑刹车变结构控制律。

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  • Discrete time variable structure control system designed by a discrete reaching law is the definite function of the system states.

    以趋近律设计的离散滑模变结构控制与系统参数及扰动有关。

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  • The design of variable structure control based on the discrete variable rate reaching law is discussed.

    研究基于离散变速趋近律的变结构控制设计问题。

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  • Based on the law that the sliding mode of variable structure control is constant to external interference, the thesis designed the output decoupling law of BTT missile.

    本文在变结构控制理论对外界扰动的不变性原理的基础上,采用变结构控制方法设计了BTT导弹的输出解耦控制律。

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  • The sliding surface is designed by the "pole-placement" method and the variable structure control is determined by the "reaching law approach".

    采用极点配置方法设计滑模面,基于趋近律方法求取变结构控制律。

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  • Based on the variable structure control theory, a guidance law that can perpendicularly impact on the target was proposed in this paper.

    基于变结构控制理论,提出了一种垂直命中目标的导引律。

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  • The design of variable structure control using the reaching law approach for uncertain discrete time systems was discussed.

    研究有界不确定离散时间系统的变结构控制设计问题。

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  • A new control approach is proposed for multimachine power systems during transient crises. The variable structure control theory is applied to design the valve control law.

    将变结构控制理论引入电力系统的暂稳汽门控制,使汽门控制器的设计大为简化,控制规律易于实现。

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  • This paper presents a new approach to the discrete-time variable structure control design based on the reaching law.

    研究基于趋近律方法的离散变结构控制设计问题。

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  • As to the attitude stablization of reentry vehicle with parameter uncertainties, its variable structure decoupling control law is designed and simulation results are given.

    讨论了其滑模面的构造方法和解耦控制条件,在姿态控制中保证了姿态跟踪期望值。

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  • Applying the discrete reaching law approach to flight simulator control system, a discrete variable structure controller is designed.

    将此离散趋近率方法应用于转台控制系统中,设计了离散变结构控制器。

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  • Fuzzy control theories combined together with the theory of variable structure control, put forward a approach law based on fuzzy logic.

    组合控制将模糊控制理论与滑模变结构理论相结合,提出模糊趋近律的控制方法。

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  • This paper presents a variable rate reaching law for discrete variable structure system based on the attenuating control.

    提出离散变结构控制系统基于衰减控制的变速趋近律。

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  • The missile guidance law utilizing nonlinear variable structure control is proposed. The acceleration command input is determined considering the target acceleration as an uncertainty.

    针对导弹拦截问题,在非线性系统滑模变结构控制理论的基础上,提计出一种新型滑模变结构导引律;

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  • The missile guidance law utilizing nonlinear variable structure control is proposed. The acceleration command input is determined considering the target acceleration as an uncertainty.

    针对导弹拦截问题,在非线性系统滑模变结构控制理论的基础上,提计出一种新型滑模变结构导引律;

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