• The first one is about how to build the connection between describing function method and phase plane method through limit cycle analysis.

    第一个是关于如何通过极限环分析建立描述函数法与相平面法之间联系;

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  • To compensate for this effect, a method is proposed in which velocity feedback signal is added to the original controller to reduce the limit cycle amplitude.

    为补偿间隙的影响,本文提出了在不改变原有的控制器基础上,通过引入速度反馈而减小间隙极限环的方法。

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  • The method of weakening integral when meeting limit is used in the common rail pressure PID control. The sampling cycle is obtained from the stepping curve, and many factors are considered.

    在系统共轨管油压的控制中引入遇限制削弱积分法,采样周期是从试验测出的阶跃响应曲线获取的,并考虑诸多的影响因素。

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  • This paper presented an analytical method with more accuracy than before considering the fundamental arid the third harmonic in limit cycle.

    提出了比较精确的计及极限环基阶谐波与三阶谐波的分析计算方法。

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  • The phenomena "limit cycle" occurred in wind tunnel test for active flutter suppression of a wing model are numerically explained using Harmonic Balance Method.

    本文采用谐波平衡法,定量地解释了机翼颤振主动抑制风洞试验中出现的极限环现象。

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  • The calculation method of finding the limit cycle suppression time is proposed also and the calculation results are consiste…

    本文还提出了一种求极限环平均抑制时间的计算方法,计算结果与实验数据相符。

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  • The calculation method of finding the limit cycle suppression time is proposed also and the calculation results are co...

    本文还提出了一种求极限环平均抑制时间的计算方法,计算结果与实验数据相符。

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  • This paper presents an approximate analytic method which determines the characteristics of aircraft lateral-directional limit cycle oscillation induced by aerodynamic hysteresis.

    本文给出近似解析公式,确定空气动力迟滞引起的飞机横航向极限环振荡特性。

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  • This paper presents an approximate analytic method which determines the characteristics of aircraft lateral-directional limit cycle oscillation induced by aerodynamic hysteresis.

    本文给出近似解析公式,确定空气动力迟滞引起的飞机横航向极限环振荡特性。

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