航天器环境工程2026，Vol.43Issue(1)：17-24,8.DOI:10.12126/see.2025054
航天器在轨操作过程柔性体碰撞动力学建模
Dynamic modeling of contact and impact between flexible bodies during spacecraft in-orbit operations
摘要
Abstract
To meet the requirements of dynamic modeling and system simulation of contact and impact in flexible multibody systems during spacecraft in-orbit operations,a flexible multibody contact and impact dynamic modeling method is proposed.The method is intended to characterize the dynamic behaviors associated with the generation,transmission and dissipation of impact energy during structural vibration and contact interactions.The established dynamic equations are applicable to any linear structures undergoing small deformations as well as to convex geometric shapes,exhibiting high generality in both structural dynamic models and geometric models.In addition,multi-face and multi-point contact/impact detection can be achieved,which is more consistent with actual physical processes.By coupling the flexible body contact and impact dynamic equations with the flexible multibody dynamic equations,a unified simulation model is constructed.This model can be applied to the overall scheme design and system-level simulation validation of typical spacecraft in-orbit operation tasks,such as in-orbit capture of space targets and in-orbit assembly of space structures.关键词
航天器/在轨操作/柔性多体系统/接触碰撞/动力学建模Key words
spacecraft/in-orbit operation/flexible multibody systems/contact and impact/dynamic modeling分类
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葛东明,鄂薇,邹元杰,邓润然,关晓东,柳翠翠,张志娟,宫伟伟..航天器在轨操作过程柔性体碰撞动力学建模[J].航天器环境工程,2026,43(1):17-24,8.基金项目
国家自然科学基金项目(编号:U24B2048) （编号:U24B2048）
