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首页> 外文期刊>PHYSICAL REVIEW E >Instability-based mechanism for body undulations in centipede locomotion
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Instability-based mechanism for body undulations in centipede locomotion

机译:cent运动中基于波动的身体波动机制

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摘要

Centipedes have many body segments and legs and they generate body undulations during terrestrialnlocomotion. Centipede locomotion has the characteristic that body undulations are absent at low speeds butnappear at faster speeds; furthermore, their amplitude and wavelength increase with increasing speed. There arenconflicting reports regarding whether the muscles along the body axis resist or support these body undulationsnand the underlying mechanisms responsible for the body undulations remain largely unclear. In the presentnstudy, we investigated centipede locomotion dynamics using computer simulation with a body-mechanicalnmodel and experiment with a centipede-like robot and then conducted dynamic analysis with a simple modelnto clarify the mechanism. The results reveal that body undulations in these models occur due to an instabilityncaused by a supercritical Hopf bifurcation. We subsequently compared these results with data obtained usingnactual centipedes. The model and actual centipedes exhibit similar dynamic properties, despite centipedes beingncomplex, nonlinear dynamic systems. Based on our findings, we propose a possible passive mechanism for bodynundulations in centipedes, similar to a follower force or jackknife instability. We also discuss the roles of thenmuscles along the body axis in generating body undulations in terms of our physical model.
机译:ped具有许多身体节段和腿部,它们在陆地运动中会产生身体起伏。 lo的运动具有以下特征:低速时不出现身体起伏,而较快时则不出现。此外,它们的幅度和波长随着速度的增加而增加。关于沿着身体轴的肌肉是否抵抗或支持这些身体起伏的报道尚无矛盾,而导致身体起伏的根本机制仍不清楚。在本研究中,我们使用带有人体力学模型的计算机模拟研究了lo的运动动力学,并以类似cent的机器人进行了实验,然后使用简单的模型进行了动力学分析以阐明其机理。结果表明,这些模型中的人体起伏是由于超临界霍夫夫分叉所引起的不稳定性所致。我们随后将这些结果与使用实际cent获得的数据进行了比较。尽管cent是复杂的非线性动力学系统,但模型和实际的exhibit表现出相似的动力学特性。根据我们的发现,我们提出了一种可能的被动机制,用于cent的人体成虫,类似于从动力或折刀不稳定。我们还将根据我们的物理模型讨论沿肌肉在身体轴上产生肌肉的角色。

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  • 来源
    《PHYSICAL REVIEW E》 |2013年第1期|1-11|共11页
  • 作者单位

    Department of Aeronautics and Astronautics Graduate School of Engineering Kyoto UniversityYoshida-honmachi Sakyo-ku Kyoto 606-8501 JapanJST CREST 5 Sanbancho Chiyoda-ku Tokyo 102-0075 Japan;

    1Department of Aeronautics and Astronautics Graduate School of Engineering Kyoto UniversityYoshida-honmachi Sakyo-ku Kyoto 606-8501 Japan;

    Department of Energy and Mechanical Engineering Faculty of Science and EngineeringDoshisha University 1-3 Tatara Miyakodani Kyotanabe Kyoto 610-0394 JapanJST CREST 5 Sanbancho Chiyoda-ku Tokyo 102-0075 Japan;

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