共查询到19条相似文献,搜索用时 46 毫秒
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条件Lyapunov指数是混沌系统同步的重要指标,文中以已知方程的Lyapunov指数谱计算方法为基础,通过数值计算考察了参考,同时,用其计算了混沌同步系统的条件Lyapunov指数,并研究了混沌同步系统的稳定性。 相似文献
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二阶随机系统的Lyapunov指数与稳定性 总被引:2,自引:0,他引:2
利用线性变换方法研究了二阶系统在随机扰动下系统的运动稳定性及分叉问题。给出了线性化系统最大Lyapunov指数的计算公式,从而由其最大Lyapunov指数为零可求出线性化系统几乎必然稳定区域的边界。 相似文献
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利用Duffing振子的运动状态来判断微弱信号的存在是一种常用的方法,通常此方法没有明确的门限。由于最大Lyapunov特性指数是指示动力学系统是否处于混沌状态的重要参数,所以将最大Lyapunov特性指数作为混沌判据引入基于Duffing振子的微弱信号检测中。利用最大Lyapunov特性指数指示Duffing振子所处的状态,如果最大Lyapunov特性指数大于1,测说明系统处于混沌状态,反之则处于周期状态,从而为此方法提供了更为直观的判断依据。仿真结果表明,采用最大Lyapunov指数作为判断依据可以更准确的判断微弱信号的存在,进而说明此方法的可行性。 相似文献
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Lyapunov指数是定量描述系统运动状态的重要参数之一.讨论了Lyapunov指数谱的数值计算方法以及它和总时间的关系,利用混沌状态下系统的最大Lyapunov指数大于零的性质预测了非线性隔振系统处于混沌运动状态时两个可变参数的参数区域。 相似文献
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Sandra Rugonyi Klaus‐Jürgen Bathe 《International journal for numerical methods in engineering》2003,56(1):145-163
A procedure to calculate the Lyapunov characteristic exponent of the response of structural continuous systems, discretized using finite element methods, is proposed. The Lyapunov characteristic exponent can be used to characterize the asymptotic stability of the system dynamic response, and it is frequently employed to identify a chaotic behaviour. The proposed procedure can also be used in the stability characterization of fluid–structure interaction systems in which the focus of the analysis is on the behaviour of the structural part. Copyright © 2002 John Wiley & Sons, Ltd. 相似文献
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故障电弧是引起电气火灾的主要原因之一,故障电弧断电保护作为一项较新的电路保护技术,能较好地防止因故障电弧而引发的火灾.通过分析故障电弧特征信号,提出了一种故障电弧检测方法,设计了故障电弧断路器的硬件和软件.利用电流互感器采集电流信号,经滤波处理后送入MCU,利用Daubechies 4阶小波变换对检测到的电流信号进行处理分析,判断有无故障电弧产生并做出相应处理.经试验分析,表明该设计是有效的,该故障电弧断路器同时具有漏电保护功能,具有识别率高、误动作率低等特点,可最大限度地保护供电系统、用电设备和人员的安全. 相似文献
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最大Lyapunov指数是判断时间序列是否为混沌的一个重要判据,目前应用比较广泛的是小数据量法。将信息熵和HQ准则应用在最大Lyapunov指数的算法中,改进了小数据量法。信息熵优化了相空间重构参数,克服了独立求解重构参数的不足;利用HQ准则确定邻近点个数增加了计算时的精度。仿真实验表明该改进的小数据量法在计算最大Lyapunov时具有良好的准确性,对噪声具有良好的鲁棒性。 相似文献
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In the transition mode of quad tilt wing-unmanned aerial vehicle (QTW-UAV), the system stability of UAV will change with the tilt angle changes, which will cause serious head drop down. Meanwhile, with the complex air flow and other disturbances, the system is prone to side bias, frying, stall and other kinetic stability problems, hence the system stability analysis has become an urgent problem to be solved. To solve the stability problem, we need the quantitative criteria of system stability and effective tool of stability analysis, and can improve the stability of the motion control by optimizing the structural parameters of the aircraft. Therefore, based on the design of the mechanical structure, the quantitative relationship between the structure parameters of the aerial vehicle and kinetic stability of the system transition mode is established by the Lyapunov exponent method. In this paper, the dynamic modeling of the position and attitude angle is carried out and the stability of the system is analyzed by Lyapunov exponent, the results show that changing the mechanical structure of the system can improve the flight stability for the system transition mode and lay a theoretical foundation for the system stability analysis. Compared with the Lyapunov direct method, this method can be construct easily, has a simple calculation process and so on. We improve the flight stability by optimizing the structure and the experiment confirms that expanding area can enhance flight stability within limits. 相似文献
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