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弹性梁式构件的运动稳定性分析
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作者 员超 宗光华 +2 位作者 周正干 张启先 刘又午 《机械工程学报》 EI CAS CSCD 北大核心 2000年第8期10-14,共5页
结构—控制耦合系统是一种机械负载与驱动控制器相互作用的动态反馈系统。将机械系统和控制系统统一考虑,将驱动机械负载的驱动力也看成是结构—控制耦合系统的内力,则可采用处理力学上保守系统的方法使建模和分析大大简化。采用能量... 结构—控制耦合系统是一种机械负载与驱动控制器相互作用的动态反馈系统。将机械系统和控制系统统一考虑,将驱动机械负载的驱动力也看成是结构—控制耦合系统的内力,则可采用处理力学上保守系统的方法使建模和分析大大简化。采用能量方法对无重力状态下弹性梁运动的相对平衡状态进行分析,得出了系统相对平衡的稳定条件。以此稳定条件作为系统运动的控制参数,有利于使弹性梁的动能转化为驱动—控制系统的电磁势能,这样一方面会加速驱动系统的制动,另一方面会迅速衰减弹性梁的振动。研究工作的结果是为弹性梁提供了一种非常简单有效的实时控制方法,该方法已在多种弹性梁试验系统上得到证实。 展开更多
关键词 弹性梁 结构-控制耦合系统 运动稳定性分析
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系留式四旋翼无人机起降时的运动稳定性分析 被引量:3
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作者 丁力 刘晨 +2 位作者 刘小峰 郑欣 吴洪涛 《仪器仪表学报》 EI CAS CSCD 北大核心 2020年第9期70-78,共9页
在起飞与降落过程中因地面效应、阵风干扰、系缆绳长等因素的影响,极易导致系留式四旋翼无人机(系留机)出现失稳现象。针对上述问题,提出一种基于李雅普诺夫指数法的系留机运动稳定性分析策略。通过Euler-Lagrange方程获得四旋翼的动力... 在起飞与降落过程中因地面效应、阵风干扰、系缆绳长等因素的影响,极易导致系留式四旋翼无人机(系留机)出现失稳现象。针对上述问题,提出一种基于李雅普诺夫指数法的系留机运动稳定性分析策略。通过Euler-Lagrange方程获得四旋翼的动力学模型,借助悬链线理论推导出系留缆绳的拉力公式,最终形成完整的系统动力学模型。给出基于李雅普诺夫指数的稳定性判定方法,构建系统结构参数与运动稳定性间的量化关系。搭建物理样机,采用直接法和间接法获得系统的物理参数。通过仿真与试验分析了系留机在起降阶段的动力学特性,结果表明:该无人机降落阶段的稳定性在仿真中比起飞阶段提高了329.5%、在试验中比后者提高了213.21%,所搭建系留机的结构参数是合理的。 展开更多
关键词 系留式四旋翼无人机 运动稳定性分析 起降阶段 李雅普诺夫指数 动力学模型
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基于图像分析的体操落地稳定性分析 被引量:1
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作者 高保华 《现代电子技术》 北大核心 2017年第5期66-69,共4页
针对体操落地稳定性控制和定量分析难度较大的问题,提出基于图像区域特征同态分割的体操落地图像视觉评估和稳定性分析方法。首先构建Pairwise MRF模型提取体操落地视觉特征,并划分图像区域;然后对采集的体操落地视觉图像在MRF框架下构... 针对体操落地稳定性控制和定量分析难度较大的问题,提出基于图像区域特征同态分割的体操落地图像视觉评估和稳定性分析方法。首先构建Pairwise MRF模型提取体操落地视觉特征,并划分图像区域;然后对采集的体操落地视觉图像在MRF框架下构建视觉观察分布模型,采用图像区域特征同态分割方法设计体操落地稳定性的视觉判别模型,实现体操落地稳定性视觉定量分析;最后仿真结果表明,该方法的体操落地稳定性控制和评价置信度较高,可靠性好,具有一定的实际应用价值。 展开更多
关键词 体操运动员落地稳定性分析 图像分析 图像分割 稳定性控制
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Chaotic Roll Motions of Ships in Regular Longitudinal Waves 被引量:4
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作者 胡开业 丁勇 王宏伟 《Journal of Marine Science and Application》 2010年第2期208-212,共5页
Parametric resonance can lead to dangerously large rolling motions, endangering the ship, cargo and crew. The QR-faetorization method for calculating (LCEs) Lyapunov Characteristic Exponents was introduced; parametr... Parametric resonance can lead to dangerously large rolling motions, endangering the ship, cargo and crew. The QR-faetorization method for calculating (LCEs) Lyapunov Characteristic Exponents was introduced; parametric resonance stability of ships in longitudinal waves was then analyzed using LCEs. Then the safe and unsafe regions of target ships were then identified. The results showed that this method can be used to analyze ship stability and to accurately identify safe and unsafe operating conditions for a ship in longitudinal waves. 展开更多
关键词 parametric resonance Lyapunov characteristic exponents longitudinal waves.
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Stability analysis via the concept of Lyapunov exponents―a case study
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作者 Chen Cheng Xu Jinfa +2 位作者 Liu Yunping Li Xianying Zhang Yonghong 《High Technology Letters》 EI CAS 2018年第2期156-162,共7页
The dynamics characteristics of the robotic arm system are usually highly nonlinear and strongly coupling,which will make it difficult to analyze the stability by the methods of solving kinetic equations or constructi... The dynamics characteristics of the robotic arm system are usually highly nonlinear and strongly coupling,which will make it difficult to analyze the stability by the methods of solving kinetic equations or constructing Lyapunov function,especially,these methods cannot calculate the quantitative relationship between mechanical structures or control input and dynamics parameters and stability.The theoretical analysis process from symbol dynamics modeling of the robotic arm system to the movement stability is studied by using the concept of Lyapunov exponents method. To verify the algorithm effectiveness,the inner relation between its joint input torque and stability or chaotic and stable motion of the 2-DOF robotic arm system is analyzed quantitatively. As compared with its counterpart of Lyapunov's direct method,the main advantage of the concept of Lyapunov exponents is that the methods for calculating the exponents are constructive to provide an effective analysis tool for analyzing robotic arm system movement stability of nonlinear systems. 展开更多
关键词 stability analysis nonlinear systems Lyapunov exponents LEs) 2-DOF roboticarm system
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The stability analysis of rolling motion of hypersonic vehicles and its validations 被引量:8
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作者 YE YouDa ZHAO ZhongLiang +1 位作者 TIAN Hao ZHANG XianFeng 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2014年第12期2194-2204,共11页
The stability of the rolling motion of near space hypersonic vehicles with rudder control is studied using method of qualitative analysis of nonlinear differential equations, and the stability criteria of the deflecte... The stability of the rolling motion of near space hypersonic vehicles with rudder control is studied using method of qualitative analysis of nonlinear differential equations, and the stability criteria of the deflected rolling motions are improved. The out- comes can serve as the basis for further study regarding the influence of pitching and lateral motion on the stability of rolling motion. To validate the theoretical results, numerical simulations were do^e for the rolling motion of two hypersonic vehicles with typical configurations. Also, wind tunnel experiments for four aircraft models with typical configurations have been done. The results show that: 1) there exist two dynamic patterns of the rolling motion under statically stable condition. The first one is point attractor, for which the motion of aircraft returns to the original state. The second is periodic attractor, for which the aircraft rolls periodically. 2) Under statically unstable condition, there exist three dynamic patterns of rolling motion, namely, the point attractor, periodic attractor around deflected state of rolling motion, and double periodic attractors or chaotic attrac- tors. 展开更多
关键词 rolling motion stability criterion numerical simulation wind tunnel experiment
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