航天服软式上躯干主动适体方法

doi:10.7527/S1000-6893.2015.0149

Abstract

Abstract:

The upper torso is the foundation of the spacesuit, which makes it of significant influence on the spacesuit fit. There are two types of fit design of the upper torso:the passive fit design and the active fit design. The active fit design method realizes the reconfiguration of the soft upper torso, which achieves the best spacesuit fit. The Stewart platform is applied in the fit design of upper torso to research the active fit design method for soft spacesuit upper torso. First of all, the characteristic and kinematics of the Stewart platform are analyzed. Secondly, the active fit design method of upper torso is proposed by applying the Stewart platform to upper torso. Thirdly, the mathematical model of the active fit design method is built based on kinematics analysis of the active fit design method. What is more, the performance of the active fit design method is calculated by the model. Finally, after the manufacture of the experimental model, the active fit design method experiment is conducted. The consequence of study elucidates that the active fit design method for the soft upper torso is effective in the scye bearing adjusting, meeting the fit requirement of the upper torso, which testifies the validity of the active fit design method based on Stewart platform. The research of the active fit design method for the upper torso provides some reference for the fit design of spacesuit in the future.

Key words: spacesuit, soft upper torso, fit design, active fit method, Stewart platform

CLC Number:

V445.3

LI Yuanfeng, ZHANG Wanxin, LI Meng. Active fit method for spacesuit soft upper torso[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(4): 1363-1373.

References

[1] 李潭秋. 国外中长期载人航天医学工程关键技术信息研究专题资料:第一集, 出舱航天服及其系统[M]. 北京:航天医学工程研究所, 2001:1-60. LI T Q. Foreign information of manned space flight medico-engineering key technology monographic study:First episode, EVA spacesuit system[M]. Beijing:Institute of Space Medico-Engineering, 2001:1-60(in Chinese).
[2] 陈景山. 航天服工程[M]. 北京:国防工业出版社, 2004:1-7. CHEN J S. Spacesuit engineering[M]. Beijing:National Defense Industry Press, 2004:1-7(in Chinese).
[3] FERL J, HEWES L, CADOGAN D, et al. System considerations for an exploration spacesuit upper torso architecture:SAE-2006-01-2141[R]. Friedrichshafen:SAE, 2006.
[4] BENSON E A. Investigation of a cable-driven parallel mechanism for pressure suit arm resizing and motion assistance[D]. Maryland:University of Maryland, 2007:41-70.
[5] BRADSHAW H. Analysis of scye bearing motion as applicable to the design of a morphing spacesuit[D]. Maryland:University of Maryland, 2011:24-40.
[6] HARRIS G L. The origins and technology of the advanced extravehicular space suit[M]. San Diego:American Astronautical Society Publications Office, 2001:340-460.
[7] THOMSA K S, MCMANN H J. US spacesuits[M]. 2nd ed. Chichester:Springer-Praxis, 2012:340-410.
[8] LI Y F, ZHANG W X. Advances in fit design research of spacesuit upper torso[C]//The 6th International Conference on Intelligent Human-Machine System and Cybernetics. Hangzhou:Zhejiang University, 2014:70-82.
[9] GRAZIOSI D, FERL J, SPLAWN K, et al. Development of a space suit soft upper torso mobility/sizing actuation system:SAE-2004-01-2342[R]. Friedrichshafen:SAE, 2004.
[10] JONES R, GRAZIOSI D, SPLAWN W, et al. Development of a space suit soft upper torso mobility/sizing actuation system with focus on prototype development and manned testing:SAE-2007-01-3169[R]. Friedrichshafen:SAE, 2007.
[11] THOMAS, KENNETH S. Adjustable shoulder device for hard upper torso suit:US8621662B2[P]. 2014-01-07.
[12] JACOBS S E. Morphing upper torso:A novel concept in EVA suit design:SAE-2006-01-2142[R]. Friedrichshafen:SAE, 2006.
[13] JACOBS S E. Pressure-constrained, reduced-DOF, interconnected parallel manipulators with applications to space suit design[D]. Maryland:University of Maryland, 2009:16-24.
[14] GOUGH V E, WHITEHALL S G. Universal tyre test machine[C]//FISITA Ninth International Technical Congress. London:FISITA, 1962:117-137.
[15] STEWART D. A platform with six degrees of freedom[J]. Proceedings of the Institution of Mechanical Engineers, 1965, 180:371-386.
[16] MARTINEZ E E H. Towards a robust solution of the non-linear kinematics for the general Stewart platform with estimation of distribution algorithms[J]. International Journal of Advanced Robotic Systems, 2013, 10(38):1-11.
[17] JACOBS S E, BENSON E A, AKIN D L, et al. Kinematic analysis of a robotically augmented pressure suit for planetary exploration:SAE-2007-01-3171[R]. Friedrichshafen:SAE, 2007.
[18] 陈海龙, 汪伟, 王小兵. Stewart平台六自由度位姿方程的改进数值解法研究[J]. 机床与液压, 2014, 42(3):47-49. CHEN H L, WANG W, WANG X B. Study on improved numerical solution for the posture equation of six DOF Stewart platform[J]. Machine Tool & Hydraulics, 2014, 42(3):47-49(in Chinese).
[19] 刘延柱, 洪嘉振, 杨海兴. 多刚体系统动力学[M]. 北京:高等教育出版社, 1986:20-29. LIU Y Z, HONG J Z, YANG H X. Multi-body dynamics[M]. Beijing:Higher Education Press, 1986:20-29(in Chinese).
[20] 李元丰, 张万欣, 陈景山. 航天服肩法兰布局与上肢活动相关性试验[J]. 航空学报, 2016, 37(3):906-915. LI Y F, ZHANG W X, CHEN J S. Correlation test between spacesuit scye bearing configuration and mobility of upper limbs[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(3):906-915(in Chinese).

Active fit method for spacesuit soft upper torso

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 12

Recommended Articles

Metrics

Comments

[1]	WANG Min, WU Junwei, PU Huayan, SUN Yi, PENG Yan, XIE Shaorong, LUO Jun, DING Jiheng. Integrated active and passive Stewart vibration damping system based on polygonal diaphragm spring and piezoelectric actuator [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(9): 224532-224532.
[2]	GULJAINA Kazezkhan, XIANG Binbin, WANG Na, AILI Yusup, CHEN Maozheng, LI Ning, XUE Fei. Errors analysis of a subreflector adjustment mechanism for NSRT [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(4): 423271-423271.
[3]	LI Yuanfeng, ZHANG Wanxin, CHEN Jingshan. Correlation experiment between spacesuit scye bearing configuration and mobility of upper limbs [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(3): 906-915.
[4]	ZHANG Xinjun, LI Tanqiu, ZHANG Wanxin, LI Yuanfeng. Mathematical model for spacesuit joint torque [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(3): 865-871.
[5]	SHANG Kun, LIU Xiangyang, LI Meng. Modeling of spacesuit flat pattern mobility joint based on finite element method [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(3): 1002-1010.
[6]	LIU Qilin, LIU Xiangyang, LI Meng. Design and experiment of pleated isotensoid spacesuit soft joint [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(12): 3868-3875.
[7]	WANG Shengnan, LI Yunze, ZHOU Hang, ZHOU Guodong. Characteristic Analysis of Extravehicular Spacesuit Life Support Cooling-power Integrated System [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(6): 1285-1292.
[8]	Wang Xuanyin;Li Qiang;Cheng Jia. Synchronous Tracking Control for Hydraulic Stewart Platform Based on Combination Tracking Errors in Operation Workspace [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(4): 719-725.
[9]	Zhao Jingdong;Jin Minghe;Gao Zhiqiang;Cui Pingyuan;Liu Hong;. Passive Robot Based Measuring Method for Intravehicular andExtravehicular Mobility Unit Spacesuit Arm [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2008, 29(5): 1370-1380.
[10]	YUAN Li-peng;ZHAO Ke-ding;XU Hong-guang. Study on Vertex Space of Stewart Platform [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(5): 979-984.
[11]	HAN Long-zhu;YUAN Xiu-gan;DING Li;CHEN Shou-ping;YANG Chun-xin. Experimental Investigations of Work Efficiency Evaluation of EVA Spacesuit Glove under Three Temperature Standards [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2005, 26(6): 665-669.
[12]	QIU Yi-fen;CHEN Yong-hua;YUAN Xiu-gan;YANG Chun-xin. A Method of Calculating External Heat Flux on Spacesuit Used for EVA [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2004, 25(3): 221-224.