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A new dimension design method for the cantilever-type legged lander based on truss-mechanism transformation

机译:基于桁架机制变换的悬臂式宽载机的新尺寸设计方法

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The cantilever-type legged lander (CTLL) is widely used in many extraterrestrial exploration activities, owing to the good buffering stability, large support stiffness, and excellent payload capacity. The paper will focus on the following two important and challenging aspects for its optimum dimension design: (1) One is to build a reliable and comprehensive optimization design model for the CTLL, including the optimization parameters of the topological structure, the performance indices of the landing behavior, and the constraint conditions of both landing stability and workspace; (2) The other aspect is to develop a systematic strategy to optimize both landing leg and overall lander respectively based on the optimization design model above. The paper proposes the trussmechanism transformation method (TMTM) to optimize the truss structure of the CTLL in the view of mechanisms and robotics with kinematics and dynamics characteristics. Furthermore, the design space dimensionality reduction method (DSDRM) is proposed for the multi-parameter optimization problem and develops the performance-chart based design methodology (PCbDM) as well. The paper can help one understand the relationship between different dimensions and the corresponding performances, and obtain the global optimum dimensions for both landing leg and overall lander. (C) 2019 Elsevier Ltd. All rights reserved.
机译:由于良好的缓冲稳定性,大的支撑刚度和优异的有效载荷能力,悬臂式腿部着陆器(CTLL)广泛应用于许多外星勘探活动。本文将重点关注其最优尺寸设计的两个重要和具有挑战性的方面:(1)一个是为CTLL构建可靠和全面的优化设计模型,包括拓扑结构的优化参数,性能指标着陆行为,以及着陆稳定性和工作空间的约束条件; (2)另一方面是开发系统的策略,以优化基于上述优化设计模型的着陆腿和整体着陆器。本文提出了特鲁斯主义转换方法(TMTM),以优化CTLL的机制和机器人与动力学和动力学特征的看法优化CTLL的桁架结构。此外,为多参数优化问题提出了设计空间维度减少方法(DSDRM),并也开发了基于表现图表的设计方法(PCBDM)。本文可以帮助人们了解不同尺寸与相应性能之间的关系,并获得着陆腿和整体着陆器的全球最佳尺寸。 (c)2019年elestvier有限公司保留所有权利。

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