John Bell, Laura Redmond, Kalind C. Carpenter, Jean-Pierre de la Croix
{"title":"Numerical Simulation and Influence of Non-Gaussian Vibrations on Flexible Robotic Systems","authors":"John Bell, Laura Redmond, Kalind C. Carpenter, Jean-Pierre de la Croix","doi":"10.2514/1.a35648","DOIUrl":null,"url":null,"abstract":"Random vibration excitation is a standard method for obtaining the dynamic properties of aerospace structures and simulating loading conditions. Shaker-based random excitation and traditional finite element analysis techniques use random vibrations, assuming a Gaussian distribution of excitation impulse magnitudes. While Gaussian signals may sufficiently describe some vibrational environments, many real-world excitations have non-Gaussian distributions. These signals may contain vibrational impulses larger than those observed in a Gaussian signal and could cause damage if not considered. This paper examines the influence of non-Gaussian signals on flexible vs. rigid robotic architectures using NASA JPL’s Pop-Up Flat Folding Explorer Robot (PUFFER) and Cooperative Autonomous Distributed Robotic Explorer (CADRE). The results indicate that flexible systems can be significantly impacted by a non-Gaussian excitation profile and that neither a typical enveloping of a Gaussian excitation nor a superposition of the responses to a worst-case impulse load with the response to a Gaussian signal was sufficient to bound the response due to non-Gaussian excitation. The driving mechanism for increased sensitivity of flexible robotic systems appears to be inertial, and designers may consider shifting the relative flexibility of the system or its constraints to force particular deformation modes or designing hinge mechanisms with increased damping to minimize the influence of non-Gaussian signals on the response of a flexible robotic structure.","PeriodicalId":508266,"journal":{"name":"Journal of Spacecraft and Rockets","volume":"76 6","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2024-03-31","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of Spacecraft and Rockets","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.2514/1.a35648","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
Random vibration excitation is a standard method for obtaining the dynamic properties of aerospace structures and simulating loading conditions. Shaker-based random excitation and traditional finite element analysis techniques use random vibrations, assuming a Gaussian distribution of excitation impulse magnitudes. While Gaussian signals may sufficiently describe some vibrational environments, many real-world excitations have non-Gaussian distributions. These signals may contain vibrational impulses larger than those observed in a Gaussian signal and could cause damage if not considered. This paper examines the influence of non-Gaussian signals on flexible vs. rigid robotic architectures using NASA JPL’s Pop-Up Flat Folding Explorer Robot (PUFFER) and Cooperative Autonomous Distributed Robotic Explorer (CADRE). The results indicate that flexible systems can be significantly impacted by a non-Gaussian excitation profile and that neither a typical enveloping of a Gaussian excitation nor a superposition of the responses to a worst-case impulse load with the response to a Gaussian signal was sufficient to bound the response due to non-Gaussian excitation. The driving mechanism for increased sensitivity of flexible robotic systems appears to be inertial, and designers may consider shifting the relative flexibility of the system or its constraints to force particular deformation modes or designing hinge mechanisms with increased damping to minimize the influence of non-Gaussian signals on the response of a flexible robotic structure.
随机振动激振是获取航空航天结构动态特性和模拟加载条件的标准方法。基于振动台的随机激振和传统的有限元分析技术使用随机振动,假设激振脉冲幅度呈高斯分布。虽然高斯信号可以充分描述某些振动环境,但现实世界中的许多激励都是非高斯分布。这些信号可能包含比高斯信号更大的振动脉冲,如果不加以考虑,可能会造成损坏。本文利用 NASA JPL 的弹出式扁平折叠探索机器人(PUFFER)和合作式自主分布机器人探索器(CADRE),研究了非高斯信号对柔性与刚性机器人架构的影响。结果表明,柔性系统会受到非高斯激励曲线的显著影响,无论是高斯激励的典型包络,还是最坏情况下脉冲负载响应与高斯信号响应的叠加,都不足以约束非高斯激励引起的响应。柔性机器人系统灵敏度增加的驱动机制似乎是惯性,设计人员可以考虑改变系统的相对柔性或其约束条件,以强制特定的变形模式或设计具有更大阻尼的铰链机构,从而最大限度地减少非高斯信号对柔性机器人结构响应的影响。