航天结构空间组装动力学与控制研究进展  

Review on dynamics and control of space structure in the process of on-orbit assembly

作　　者：吴志刚 蒋建平 邬树楠 李庆军 王兴 谭述君 邓子辰 WU Zhigang;JIANG Jianping;WU Shunan;LI Qingjun;WANG Xing;TAN Shujun;DENG Zichen(School of Aeronautics and Astronautics,Sun Yat-sen University,Shenzhen 518107,China;State Key Laboratory of Structural Analysis,Optimization and CAE Software for Industrial Equipment,Dalian University of Technology,Dalian 116023,China;School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China)

机构地区：[1]中山大学航空航天学院,广东深圳518107 [2]工业装备结构分析优化与CAE软件全国重点实验室,大连116023 [3]西北工业大学航空学院,西安710072

出　　处：《力学进展》2024年第2期344-390,共47页Advances in Mechanics

基　　金：国家自然科学基金(12372053,12232015,52005522,11872381,91748203)的支持。

摘　　要：空间组装是建造空间站、大型卫星天线、大口径空间望远镜、空间太阳能电站等大型和超大型航天结构的重要手段.然而,航天结构组装过程将面临构型增长、参数变化、轨道-姿态-结构耦合、接触碰撞等复杂的动力学与控制问题,给精准、高效、稳定完成组装任务带来挑战.本文介绍了大型航天结构的动力学建模方法、超大型航天结构特殊的动力学现象、航天结构空间组装过程的动力学建模研究现状;综述了航天结构在轨运行阶段的控制方法、空间组装过程的组装序列规划方法、姿态控制与振动抑制方法研究进展;总结了航天结构组装过程动力学与控制地面模拟试验中的重力卸载、缩比模型设计与试验、非线性与不确定性试验等关键技术.最后,面向未来千米量级超大型航天结构空间组装需求,针对组装过程中结构尺寸、质量和力学参数跃变等特性提出了当前研究工作中亟须解决的几类动力学与控制问题.On-orbit assembly is a crucial means to construct large and ultra-large space structures such as space stations,large satellite antennas,large-aperture space telescopes,and space solar power stations.However,complicated dynamics and control problems,such as the configuration increasement,parameter variations,orbit-attitude-structure coupled effects,and contact problems,will be encountered during the process of on-orbit assembly and bring challenges to accomplishing the assembly task accurately,efficiently,and safely.The development status of dynamic modelling methods of large space structures,special dynamic phenomena of ultra-large space structures,and dynamic modelling studies of space structures during on-orbit assembly process were reviewed.Then,the control methods of the on-orbit operation stage,the assembly sequence planning methods,and the control methods for the on-orbit assembly process were introduced.In addition,the key techniques of gravity unloading,scale model design and testing,nonlinearity and uncertainty quantification techniques with ground tests in the assembly process were summarized.Finally,to address the increasing configuration and discontinuously varying parameters of the ultra-large space structures during on-orbit assembly process,a few suggestions were put forward to deal with the dynamic and control problems.

关 键 词：大型航天结构 超大型航天结构 航天器动力学 航天器控制 空间组装 地面模拟试验 

分 类 号：V423.9[航空宇航科学与技术—飞行器设计]