Development of Wire Actuation 2 Stage Extension Mechanism Considering to Use for Spacecraft
Extension mechanism is attracting attention to use for capturing mechanism of the active debris removal spacecraft. Authors developed the debris capturing end effector consist of multiple wire action 2 stage extension mechanism. This mechanism is selected because of its high extension ratio, fast ex...
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Veröffentlicht in: | Journal of the Japan Society for Precision Engineering 2020/10/05, Vol.86(10), pp.800-805 |
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creator | TANISHIMA, Nobutaka OKAMOTO, Hiroyuki IKI, Kentaro |
description | Extension mechanism is attracting attention to use for capturing mechanism of the active debris removal spacecraft. Authors developed the debris capturing end effector consist of multiple wire action 2 stage extension mechanism. This mechanism is selected because of its high extension ratio, fast extending speed, high stiffness and retry capability using single motor. This end effector and mechanism's experimental results showed that it satisfies the requirements. However, this mechanism is not yet evaluated to use in space environment. In this study, wire actuation 2 stage extension mecha- nism's movement is discussed, and equation of motion is proposed to discuss which data to be acquired to evaluate the mechanism to use in space. The device to obtain the data is introduced, and experimental results shows that the introduced device can well acquire the data. Experiment inside the vacuum chamber is also conducted, and the results showed that this mechanism can be used in space environment. |
doi_str_mv | 10.2493/jjspe.86.800 |
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Authors developed the debris capturing end effector consist of multiple wire action 2 stage extension mechanism. This mechanism is selected because of its high extension ratio, fast extending speed, high stiffness and retry capability using single motor. This end effector and mechanism's experimental results showed that it satisfies the requirements. However, this mechanism is not yet evaluated to use in space environment. In this study, wire actuation 2 stage extension mecha- nism's movement is discussed, and equation of motion is proposed to discuss which data to be acquired to evaluate the mechanism to use in space. The device to obtain the data is introduced, and experimental results shows that the introduced device can well acquire the data. Experiment inside the vacuum chamber is also conducted, and the results showed that this mechanism can be used in space environment.</description><identifier>ISSN: 0912-0289</identifier><identifier>EISSN: 1882-675X</identifier><identifier>DOI: 10.2493/jjspe.86.800</identifier><language>eng ; jpn</language><publisher>Tokyo: The Japan Society for Precision Engineering</publisher><subject>Actuation ; Aerospace environments ; Data acquisition ; Debris ; End effectors ; Equations of motion ; space robotics ; Spacecraft ; Stiffness ; Vacuum chambers ; Wire ; wire actuation mechanism</subject><ispartof>Journal of the Japan Society for Precision Engineering, 2020/10/05, Vol.86(10), pp.800-805</ispartof><rights>2020 The Japan Society for Precision Engineering</rights><rights>Copyright Japan Science and Technology Agency 2020</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c2300-b3cdd59c38e343810ae8e36f6571926bd7980ff618340c9180639e3800460cfb3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>TANISHIMA, Nobutaka</creatorcontrib><creatorcontrib>OKAMOTO, Hiroyuki</creatorcontrib><creatorcontrib>IKI, Kentaro</creatorcontrib><title>Development of Wire Actuation 2 Stage Extension Mechanism Considering to Use for Spacecraft</title><title>Journal of the Japan Society for Precision Engineering</title><addtitle>Journal of the Japan Society for Precision Engineering</addtitle><description>Extension mechanism is attracting attention to use for capturing mechanism of the active debris removal spacecraft. Authors developed the debris capturing end effector consist of multiple wire action 2 stage extension mechanism. This mechanism is selected because of its high extension ratio, fast extending speed, high stiffness and retry capability using single motor. This end effector and mechanism's experimental results showed that it satisfies the requirements. However, this mechanism is not yet evaluated to use in space environment. In this study, wire actuation 2 stage extension mecha- nism's movement is discussed, and equation of motion is proposed to discuss which data to be acquired to evaluate the mechanism to use in space. The device to obtain the data is introduced, and experimental results shows that the introduced device can well acquire the data. Experiment inside the vacuum chamber is also conducted, and the results showed that this mechanism can be used in space environment.</description><subject>Actuation</subject><subject>Aerospace environments</subject><subject>Data acquisition</subject><subject>Debris</subject><subject>End effectors</subject><subject>Equations of motion</subject><subject>space robotics</subject><subject>Spacecraft</subject><subject>Stiffness</subject><subject>Vacuum chambers</subject><subject>Wire</subject><subject>wire actuation mechanism</subject><issn>0912-0289</issn><issn>1882-675X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><recordid>eNpFkE1LAzEQhoMoWGpv_oCAV7fmY5vN3iy1fkDFQy0KHkKandQt7WZNUtF_b-pKPc0w87zvMC9C55QMWV7yq_U6tDCUYigJOUI9KiXLRDF6PUY9UlKWESbLUzQIoV4SwkRBGGc99HYDn7Bx7RaaiJ3FL7UHPDZxp2PtGszwPOoV4OlXhCbsJ49g3nVThy2euDSpwNfNCkeHFwGwdR7PW23AeG3jGTqxehNg8Ff7aHE7fZ7cZ7Onu4fJeJYZxgnJltxU1ag0XALPuaREQ-qEFaOClkwsq6KUxFpBJc-JKakkgpfA05u5IMYueR9ddL6tdx87CFGt3c436aRi-UjkgvIiT9RlRxnvQvBgVevrrfbfihK1T1D9JqikUMk64dcdvg77BA6w9rE2G_iHk7qTHFYpIK-g4T81x3rx</recordid><startdate>20201005</startdate><enddate>20201005</enddate><creator>TANISHIMA, Nobutaka</creator><creator>OKAMOTO, Hiroyuki</creator><creator>IKI, Kentaro</creator><general>The Japan Society for Precision Engineering</general><general>Japan Science and Technology Agency</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope></search><sort><creationdate>20201005</creationdate><title>Development of Wire Actuation 2 Stage Extension Mechanism Considering to Use for Spacecraft</title><author>TANISHIMA, Nobutaka ; OKAMOTO, Hiroyuki ; IKI, Kentaro</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c2300-b3cdd59c38e343810ae8e36f6571926bd7980ff618340c9180639e3800460cfb3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng ; jpn</language><creationdate>2020</creationdate><topic>Actuation</topic><topic>Aerospace environments</topic><topic>Data acquisition</topic><topic>Debris</topic><topic>End effectors</topic><topic>Equations of motion</topic><topic>space robotics</topic><topic>Spacecraft</topic><topic>Stiffness</topic><topic>Vacuum chambers</topic><topic>Wire</topic><topic>wire actuation mechanism</topic><toplevel>online_resources</toplevel><creatorcontrib>TANISHIMA, Nobutaka</creatorcontrib><creatorcontrib>OKAMOTO, Hiroyuki</creatorcontrib><creatorcontrib>IKI, Kentaro</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><jtitle>Journal of the Japan Society for Precision Engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>TANISHIMA, Nobutaka</au><au>OKAMOTO, Hiroyuki</au><au>IKI, Kentaro</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Development of Wire Actuation 2 Stage Extension Mechanism Considering to Use for Spacecraft</atitle><jtitle>Journal of the Japan Society for Precision Engineering</jtitle><addtitle>Journal of the Japan Society for Precision Engineering</addtitle><date>2020-10-05</date><risdate>2020</risdate><volume>86</volume><issue>10</issue><spage>800</spage><epage>805</epage><pages>800-805</pages><issn>0912-0289</issn><eissn>1882-675X</eissn><abstract>Extension mechanism is attracting attention to use for capturing mechanism of the active debris removal spacecraft. Authors developed the debris capturing end effector consist of multiple wire action 2 stage extension mechanism. This mechanism is selected because of its high extension ratio, fast extending speed, high stiffness and retry capability using single motor. This end effector and mechanism's experimental results showed that it satisfies the requirements. However, this mechanism is not yet evaluated to use in space environment. In this study, wire actuation 2 stage extension mecha- nism's movement is discussed, and equation of motion is proposed to discuss which data to be acquired to evaluate the mechanism to use in space. The device to obtain the data is introduced, and experimental results shows that the introduced device can well acquire the data. Experiment inside the vacuum chamber is also conducted, and the results showed that this mechanism can be used in space environment.</abstract><cop>Tokyo</cop><pub>The Japan Society for Precision Engineering</pub><doi>10.2493/jjspe.86.800</doi><tpages>6</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Actuation Aerospace environments Data acquisition Debris End effectors Equations of motion space robotics Spacecraft Stiffness Vacuum chambers Wire wire actuation mechanism |
title | Development of Wire Actuation 2 Stage Extension Mechanism Considering to Use for Spacecraft |
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