|Table of Contents|

Review and development prospect of space rendezvous and docking mechanism(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2022年03期
Page:
1-15
Research Field:
专论与综述
Publishing date:

Info

Title:
Review and development prospect of space rendezvous and docking mechanism
Author(s):
MA Shuai1; 2; FENG Xin1; KONG Ning2; ZHOU Lei1; ZHU Zihuan1
(1.Beijing Institute of Aerospace Testing Technology, Beijing 100074, China 2.University of Science and Technology Beijing,Beijing 100083, China)
Keywords:
space rendezvous docking mechanism spacecraft orbital replacement unit locking structure docking technology
PACS:
V526
DOI:
-
Abstract:
Space rendezvous and docking is a necessary technology for developing aerospace industry and exploring unknown space.Aiming at the technical requirements of spacecraft rendezvous and docking for manned delivery or on-orbit maintenance in aerospace engineering, the research progress and achievements of space rendezvous and docking mechanism at home and abroad over the years were emphatically reviewed.The mechanical space rendezvous and docking mechanism utilizing the rocket engine propulsion technology to complete the spacecraft integration was divided into three types:cone-rod, peripheral and three-claw, and their different working modes were compared.Along the development of space rendezvous and docking technology, the docking mechanism, locking structure and working principle of large and small spacecraft and orbital replacement unit were summarized.Through the comparison of the review content at home and abroad, the technological gaps in domestic space rendezvous and docking mechanism development are revealed, and the key directions and core technologies for the space rendezvous and docking mechanism development are proposed, which provides reference for the development of Chinas aerospace industry.

References:

[1] 周前祥,连顺国.空间交会对接技术及其发展趋势[J].中国航天,1998(1):25-28.
[2] 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):20-26.
[3] 林来兴.自主空间交会对接技术进展[J].载人航天,2005,11(4):13-17.
[4] 潘科炎,王旭东.空间站的在轨技术(一):空间的交会与对接[J].航天控制,1988,6(3):34-42.
[5] 郑永煌.空间交会对接技术[J].自然杂志,2011,33(6):311-314.
[6] 林来兴.空间交会对接的发展历程[J].国际太空,2018(10):39-42.
[7] 博引.美国的空间交会对接技术[J].太空探索,2011(10):37-39.
[8] 边广龙.苏联/俄罗斯的空间交会对接技术[J].太空探索,2011(10):34-36.
[9] 朱仁璋,王鸿芳,徐宇杰,等.美国航天器交会技术研究[J].航天器工程,2011,20(5):11-36.
[10] 周建平.载人航天交会对接技术[J].载人航天,2011,17(2):1-8.
[11] 林来兴.四十年空间交会对接技术的发展[J].航天器工程,2007,16(4):70-77.
[12] 石军,郭廷源.航天器在轨可更换技术研究[C]//中国空间科学学会空间机电与空间光学专业委员会学术年会.兰州:中国空间科学学会,2008.
[13] FRIEND R B.Orbital express program summary and mission overview[C]//SPIE Defense and Security Symposium.Orlando,Florida:SPIE,2008.
[14] MEGURO A,SHINTATE K,USUI M,et al.In-orbit deployment characteristics of large deployable antenna reflector onboard engineering test satellite VIII[J].Acta Astronautica,2009,65(9/10):1306-1316.
[15] VINALS J,URGOITI E,GUERRA G,et al.Multi-functional interface for flexibility and reconfigurability of future European space robotic systems[J].Advances in Astronautics Science and Technology,2018,1(1):119-133.
[16] 马婷婷,魏晨曦.空间交会对接概述[J].中国航天,2004(7):33-34.
[17] 博引.空间交会对接技术的发展[J].国际太空,2011(10):22-29.
[18] 张崇峰.空间对接机构综述[J].世界科学,2003(1):26-27.
[19] 李强.新型类锥杆式对接机构的碰撞过程分析[D].长沙:国防科学技术大学,2009.
[20] 韩伟,姜志杰,黄奕勇,等.面向小型自主航天器的锥-杆式对接机构锥面构型设计[J].空间科学学报,2019,39(2):228-232.
[21] 李磊,聂宏,陈金宝,等.自动卫星对接结构设计及关键参数研究[J].机械设计与制造,2012(11):143-145.
[22] HAYS A B,TCHORYK P,PAVLICH J C,et al.Dynamic simulation and validation of a satellite docking system[C]//AeroSense 2003.Orlando,Florida:SPIE,2003.
[23] HAYS A B,TCHORYK P,PAVLICH J C,et al.Advancements in KC-135 microgravity testing of an autonomous satellite docking system[J].Proceedings of SPIE - The International Society for Optical Engineering,2004,5419(3):119-129.
[24] PAVLICH J C,TCHORYK P,HAYS A B,et al.KC-135 zero G testing of a micro satellite docking mechanism[J].Proceedings of SPIE - The International Society for Optical Engineering,2003,5088(1):31-42.
[25] HAYS A B,TCHORYK P,PAVLICH J C,et al.Advancements in design of an autonomous satellite docking system[J].Proceedings of SPIE - The International Society for Optical Engineering,2004,5419(3):107-118.
[26] LI W J,CHENG D Y,LIU X G,et al.On-orbit service(OOS)of spacecraft:a review of engineering developments[J].Progress in Aerospace Sciences,2019,108:32-120.
[27] HU B S,CHEN F,HAN L L,et al.Design and ground verification of space station manipulator control method for orbital replacement unit changeout[J].International Journal of Aerospace Engineering,2018,2018:4271035.
[28] MEDINA A,TOMASSINI A,SUATONI M,et al.Towards a standardized grasping and refuelling on-orbit servicing for geo spacecraft[J].Acta Astronautica,2017,134:1-10.
[29] ADOMEIT A,REIMERDES H G,LAKSHMANAN M,et al.Structural concept and design for modular and serviceable spacecraft systems[C]//54th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference.Reston,Virginia:AIAA,2013.
[30] KORTMANN M,DAFNIS A,REIMERDES H G.Development and breadboard testing of a mechanical coupling interface for modular spacecraft systems[C]//13th European Conference on Spacecraft Structures,Materials and Environmental Testing.[S.l.:s.n.],2014.
[31] KORTMANN M,MEINERT T,DAFNIS A,et al.Multifunctional interface for modular satellite systems with robotic servicing capabilities[C]//68th International Astronautical Congress.Adelaide:IAC,2017.
[32] KORTMANN M,R?L S,WEISE J,et al.Building block-based “iBOSS” approach:fully modular systems with standard interface to enhance future satellites[C]//66rd International Astronautical Congress.Jerusalem:IAC,2015.
[33] KORTMANN M,ZEIS C,MEINERT T,et al.Design and qualification of a multifunctional interface for modular satellite systems[C]//69th International Astronautical Congress.Bremen:IAC,2018.
[34] YAN X T,BRINKMANN W,PALAZZETTI R,et al.Integrated mechanical,thermal,data,and power transfer interfaces for future space robotics[J].Frontiers in Robotics and AI,2018,5(64):1-16.
[35] JANKOVIC M,BRINKMANN W,BARTSCH S,et al.Concepts of active payload modules and end-effectors suitable for standard interface for robotic manipulation of payloads in future space missions(SIROM)interface[C]//2018 IEEE Aerospace Conference.New York:IEEE,2018.
[36] OGILVIE A,ALLPORT J,HANNAH M,et al.Autonomous robotic operations for on-orbit satellite servicing[J].Proceedings of SPIE - The International Society for Optical Engineering,2008,6958(9):1-12.
[37] 马聪.在轨更换模块组件设计及动力学分析[D].哈尔滨:哈尔滨工业大学,2014.
[38] 杨惠欣.航天器在轨可更换模块设计与分析[D].沈阳:东北大学,2011.
[39] 张艳丽,杨惠欣,李树军.航天器在轨可更换模块机构与结构设计[J].沈阳航空航天大学学报,2014,31(5):72-76.
[40] 籍勇翔.面向在轨服务的航天器可更换模块概念研究[D].南京:南京航空航天大学,2016.
[41] 杨铭波.空间站通用停靠机构方案设计与动力学分析[D].南京:南京航空航天大学,2013.
[42] POLITES M E.Technology of automated rendezvous and capture in space[J].Journal of Spacecraft and Rockets,1999,36(2):280-291.
[43] 朱仁璋,王鸿芳,邹玲,等.载人航天器加压连接机构研究[J].航天器工程,2012,21(5):8-24.
[44] 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.
[45] 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.
[46] SHOEMAKER J,WRIGHT M.Orbital express space operations architecture program[J].Proceedings of SPIE - The International Society for Optical Engineering,2004,5088(3):1-9.
[47] CHRISTIANSEN S,NILSON T.Docking system mechanism utilized on orbital express program[C]//39th Aerospace Mechanisms Symposium.Huntsville:Marshall Space Flight Center,2008.
[48] STAMM S,MOTAGHEDI P.Orbital express capture system:concept to reality[J].Proceedings of SPIE - The International Society for Optical Engineering,2004,5419(3):78-91.
[49] DIPPREY N,ROTENBERGER S.Orbital express propellant resupply servicing[C]//39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.Reston,Virginia:AIAA,2003.
[50] ROTENBERGER S,SOOHOO D,ABRAHAM G.Orbital express fluid transfer demonstration system[J].Proceedings of SPIE-The International Society for Optical Engineering,2008,6958(8):1-9.
[51] YAMAGISHI A,KAWAGUCHI Y,YOKOBORI S I,et al.Environmental data and survival data of Deinococcus aetherius from the exposure facility of the Japan experimental module of the international space station obtained by the tanpopo mission[J].Astrobiology,2018,18(11):1369-1374.
[52] KAWAGUCHI Y,YOKOBORI S I,HASHIMOTO H,et al.Investigation of the interplanetary transfer of microbes in the tanpopo mission at the exposed facility of the international space station[J].Astrobiology,2016,16(5):363-376.
[53] COOK J,AKSAMENTOV V,HOFFMAN T,et al.ISS interface mechanisms and their heritage[C]//AIAA SPACE 2011 Conference & Exposition.Reston,Virigina:AIAA,2011.
[54] 庄原,孔宁,任杰,等.在轨可更换模块对接接口技术综述[J].中国机械工程,2020,31(16):1917-1930.
[55] MASAHARU T.JEM exposed facility system and operation[J].IHI Engineering Review,2010,43(1):1-5.
[56] OLIVIERI L,ANTONELLO A,SAVIOLI L,et al.Dynamic behavior of a semi-androgynous small satellite docking interface[C]//65th International Astronautical Congress.Toronto:IAC,2014.
[57] 宫兆飞.空间一体化对接接口设计与分析[D].哈尔滨:哈尔滨工业大学,2016.
[58] 韩亮亮,赫向阳,杨健,等.一种自移动空间机械臂末端执行器的研制[J].机器人,2016,38(6):720-726.
[59] 丰飞,唐丽娜,韩锋.空间多功能在轨维护机器人系统及其末端执行器设计[J].航空制造技术,2019,62(10):14-22.
[60] 田立成,王小永,张天平.空间电推进应用及技术发展趋势[J].火箭推进,2015,41(3):7-14.
TIAN L C,WANG X Y,ZHANG T P.Application and development trend of space electric propulsion technology[J].Journal of Rocket Propulsion,2015,41(3):7-14.
[61] FREDRICKSON S E,DURAN S,HOWARD N,et al.Application of the mini AERCam free flyer for orbital inspection[J].Proceedings of SPIE - The International Society for Optical Engineering,2004,5419(8):26-35.
[62] RODGERS L,HOFF N,JORDAN E,et al.A universal interface for modular spacecraft[C]//19th Annual AIAA/USU Conference on Small Satellites.Reston,Virginia:AIAA,2005.
[63] WOKES D,SMAIL S,PALMER P,et al.Pose estimation for in-orbit self-assembly of intelligent self-powered modules[C]//AIAA Guidance,Navigation,and Control Conference.Reston,Virginia:AIAA,2009.
[64] UNDERWOOD C,PELLEGRINO S,LAPPAS V J,et al.Using CubeSat/micro-satellite technology to demonstrate the Autonomous Assembly of a Reconfigurable Space Telescope(AAReST)[J].Acta Astronautica,2015,114:112-122.
[65] BOESSO A,FRANCESCONI A.ARCADE small-scale docking mechanism for micro-satellites[J].Acta Astronautica,2013,86:77-87.
[66] 许军校.面向空间对接的电磁机构设计与实验研究[D].长沙:国防科学技术大学,2008.
[67] 张强.柔性自稳定空间电磁对接系统设计与实验研究[D].长沙:国防科学技术大学,2013.
[68] 谢逸轩.微纳卫星电磁连接及分离机构的研究[D].哈尔滨:哈尔滨工业大学,2018.
[69] 王波,庄原,刘芃,等.航天器电磁对接技术发展综述[J].航天器工程,2018,27(6):92-101.

Memo

Memo:
-
Last Update: 1900-01-01