张崇峰;姚建;刘志;丁立超;程芳华;邱华勇;

• 1:上海航天技术研究院
• 2:上海宇航系统工程研究所

摘要(Abstract)：

空间对接技术是载人航天的一项基本技术，是实现空间站建造和长期运营的先决条件。我国2011年实现了神舟八号飞船和天宫一号目标飞行器的空间对接，经改进及多次飞行应用，支持我国空间站的建设和运行，我国载人周边式对接机构产品技术成熟度和可靠性得到充分验证。文章论述了我国载人航天器对接机构在总体技术、对接动力学设计和对接试验等方面发展及应用情况，并对后续载人月球探测任务对接需求与对接方案情况进行了阐述。

关键词(KeyWords)： 载人航天器;对接机构;对接动力学;对接试验

Abstract:

Keywords:

基金项目(Foundation): 中国载人航天工程

作者(Authors): 张崇峰;姚建;刘志;丁立超;程芳华;邱华勇;

参考文献(References)：

• [1] 张柏楠.中国载人航天开启新征程[J].中国航天.2021(8):8-13 Zhang Bainan.China Manned Space Launch a New Journey[J].Aerospace China,2021(8):8-13 (in Chinese)
• [2] 周建平.空间交会对接技术[M].北京：国防工业出版社，2013 Zhou Jianping.Spacecraft rendezvous and docking technology[M].Beijing:National Defense Industry Press,2013 (in Chinese)
• [3] 陈宝东，郑云青，邵济明，等.对接机构分系统研制[J].上海航天，2011,28(6):1-6 Chen Baodong,Zheng Yunqing,Shao Jiming,et al.Development of docking subsystem[J].Aerospace Shanghai,2011,28(6):1-6 (in Chinese)
• [4] 张崇峰，柏合民.飞船空间对接机构技术[J].中国科学：技术科学，2014,44(1):22-26.Zhang Chongfeng,Bai Hemin.Space docking mechanism technology of spacecraft[J].Scientia Sinica Technologica,2014,44:20-26 (in Chinese)
• [5] 陈宝东，唐平.空间对接机构技术及其研制 [J].上海航天，2005 (5):6-8,61 Chen Baodong,Tang Ping.The technology development of docking mechanism system[J].Aerospace Shanghai,2005 (5):6-8,61 (in Chinese)
• [6] 张崇峰，陈宝东，郑云青，等航天器对接机构[M].北京：科学出版社，2016 Zhang Chongfeng,Chen Baodong,Zheng Yunqing,et al.Spacecraft docking mechanism[M].Beijing:Science Press,2016 (in Chinese)
• [7] 上海宇航系统工程研究所.邱华勇，张崇峰，苑会领，等.一种阻尼可控的对接机构传动缓冲系统[P].中国：ZL201811057025.X,2018 Aerospace System Engineering Shanghai.Qiu Huayong,Zhang Chongfeng,Yuan Huiling,et al.A damping controllable transimission buffer system for docking mechanism[P].China:ZL201811057025.X,2018 (in Chinese)
• [8] ISS MCB.International Docking System Standard (IDSS),Interface Definition Document(IDD) (Revision E).[EB/OL].[2017-04-01].http://International Docking Standard.com/.
• [9] 刘志，张崇峰，靳宗向，等.GB/T 34512-2017,载人航天周边式交会对接机构接口要求[S].北京：中国标准出版社，2017 Liu Zhi,Zhang Chongfeng,Jin Zongxiang,et al.GB/T 34512-2017,Requirement for interface of manned spacecraft peripheral docking mechanism[S].Beijing:Standards Press of China,2017 (in Chinese)
• [10] 张崇峰，刘志.空间对接机构技术综述[J].上海航天，2016,33(5):1-11 Zhang Chongfeng,Liu Zhi.Review of space docking mechanism and its technology[J].Aerospace Shanghai,2016,33(5):1-11 (in Chinese)
• [11] 娄汉文，曲广吉，刘济生.空间对接机构[M].北京：航空工业出版社，1992 Lou Hanwen,Qu Guangji,Liu Jisheng.Space docking mechanism[M].Aviation Industry Press,1992 (in Chinese)
• [12] TobieLabauve.Low Impact Docking System (LIDS) [R/OL].[2021-12-20].http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20090007783_2009006897.pdf.
• [13] Pejmun Motaghedi,Siamak Ghofranian.Feasibility of the soft impact mating attenuation concept for the NASA docking system[C].AIAA Space 2014 Conference and Exposition.Washington D.C.:AIAA,2014
• [14] 刘志，张崇峰，邵济明，等.异体同构、刚度阻尼闭环反馈控制的对接系统及方法[P].中国：ZL201210489374.5,2013 Liu Zhi,Zhang Chongfeng,Shao Jiming,et al.Docking system and method of androgynous,stiffness and damping closed-loop feedback control[P].China:ZL201210489374.5,2013 (in Chinese)