Principles and experimental analysis of a measuring system for measuring spacesuit joint's damping parameters

Hao Wang; Ming he Jin; Hong Liu; Xiao hui Gao; Tan qiu Li; Yong jun Zhao

Principles and experimental analysis of a measuring system for measuring spacesuit joint's damping parameters

Hao Wang^*
, Ming he Jin
, Hong Liu
, Xiao hui Gao
, Tan qiu Li
, Yong jun Zhao

^*Corresponding author for this work

School of Mechatronics Engineering

Harbin Institute of Technology

Research output: Contribution to journal › Article › peer-review

3 Scopus citations

Abstract

Objective: To measure the damping parameters of the spacesuit joint. Method: The principles of the passive robot system for measuring spacesuit joint's damping parameters were presented. Basing on its special mechanical structure, a 3 DOF model of the flexible IVA (intra-vehicular activity) spacesuit's sleeve was built. The optimal approximation of inverse calculation based on 6 dimension space interval was described. The damping parameters of an actual IVA spacesuit's sleeve were measured on the actual testbed. Also, the potential application of the measuring system was discussed. Result: The model of spacesuit sleeve and the forward/inverse kinematics were proved by experimental measurements and real time 3D simulation. Conclusion: The principles and the proposed method of the measurement were testified.

Original language	English
Pages (from-to)	349-353
Number of pages	5
Journal	Hangtian Yixue Yu Yixue Gongcheng/Space Medicine and Medical Engineering
Volume	16
Issue number	5
State	Published - Oct 2003

Cite this

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title = "Principles and experimental analysis of a measuring system for measuring spacesuit joint's damping parameters",

abstract = "Objective: To measure the damping parameters of the spacesuit joint. Method: The principles of the passive robot system for measuring spacesuit joint's damping parameters were presented. Basing on its special mechanical structure, a 3 DOF model of the flexible IVA (intra-vehicular activity) spacesuit's sleeve was built. The optimal approximation of inverse calculation based on 6 dimension space interval was described. The damping parameters of an actual IVA spacesuit's sleeve were measured on the actual testbed. Also, the potential application of the measuring system was discussed. Result: The model of spacesuit sleeve and the forward/inverse kinematics were proved by experimental measurements and real time 3D simulation. Conclusion: The principles and the proposed method of the measurement were testified.",

author = "Hao Wang and Jin, \{Ming he\} and Hong Liu and Gao, \{Xiao hui\} and Li, \{Tan qiu\} and Zhao, \{Yong jun\}",

year = "2003",

month = oct,

language = "英语",

volume = "16",

pages = "349--353",

journal = "Hangtian Yixue Yu Yixue Gongcheng/Space Medicine and Medical Engineering",

issn = "1002-0837",

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T1 - Principles and experimental analysis of a measuring system for measuring spacesuit joint's damping parameters

AU - Wang, Hao

AU - Jin, Ming he

AU - Liu, Hong

AU - Gao, Xiao hui

AU - Li, Tan qiu

AU - Zhao, Yong jun

PY - 2003/10

Y1 - 2003/10

N2 - Objective: To measure the damping parameters of the spacesuit joint. Method: The principles of the passive robot system for measuring spacesuit joint's damping parameters were presented. Basing on its special mechanical structure, a 3 DOF model of the flexible IVA (intra-vehicular activity) spacesuit's sleeve was built. The optimal approximation of inverse calculation based on 6 dimension space interval was described. The damping parameters of an actual IVA spacesuit's sleeve were measured on the actual testbed. Also, the potential application of the measuring system was discussed. Result: The model of spacesuit sleeve and the forward/inverse kinematics were proved by experimental measurements and real time 3D simulation. Conclusion: The principles and the proposed method of the measurement were testified.

AB - Objective: To measure the damping parameters of the spacesuit joint. Method: The principles of the passive robot system for measuring spacesuit joint's damping parameters were presented. Basing on its special mechanical structure, a 3 DOF model of the flexible IVA (intra-vehicular activity) spacesuit's sleeve was built. The optimal approximation of inverse calculation based on 6 dimension space interval was described. The damping parameters of an actual IVA spacesuit's sleeve were measured on the actual testbed. Also, the potential application of the measuring system was discussed. Result: The model of spacesuit sleeve and the forward/inverse kinematics were proved by experimental measurements and real time 3D simulation. Conclusion: The principles and the proposed method of the measurement were testified.

UR - https://www.scopus.com/pages/publications/1442351584

M3 - 文章

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AN - SCOPUS:1442351584

SN - 1002-0837

VL - 16

SP - 349

EP - 353

JO - Hangtian Yixue Yu Yixue Gongcheng/Space Medicine and Medical Engineering

JF - Hangtian Yixue Yu Yixue Gongcheng/Space Medicine and Medical Engineering

IS - 5

ER -

Principles and experimental analysis of a measuring system for measuring spacesuit joint's damping parameters

Abstract

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