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‚¿‚Ȃ݂ɁC‰E‚̎ʐ^‚́C‚±‚ÌŒ¤‹†‚É—p‚¢‚½ƒoƒCƒRƒ“ƒxƒbƒNƒXƒu[ƒ€‚ŁC‘g•R‚Ŕ핢‚·‚邱‚Æ‚Å2‚‚̃Rƒ“ƒxƒbƒNƒXƒe[ƒv‚ª—£‚ê‚邱‚Æ‚ðŠÉ‚â‚©‚É–h‚¢‚Å‚¢‚Ü‚·iƒTƒJƒZEƒAƒhƒeƒbƒNiŠ”j»‚Å‚·jDƒoƒCƒRƒ“ƒxƒbƒNƒXƒu[ƒ€‚̍őå‚Ì—˜“_‚́C2‚‚̃e[ƒv‚ªŒÝ‚¢‚É’·Žè•ûŒü‚ɃXƒ‰ƒCƒh‚·‚邱‚Æ‚ª‚Å‚«‚邽‚߁CŠª‚«•t‚¯Žû”[Žž‚Ì“àŠOŽü·‚ð‹zŽû‚·‚邱‚Æ‚ª‚Å‚«C‚³‚ç‚ɁC‚¢‚ë‚¢‚ëH•v‚·‚邱‚ƂŁCŽû”[«‚ð‚‚ß‚é‚±‚Æ‚ª‚Å‚«‚Ü‚·D

[reference]

‹{èNs, uBCONƒu[ƒ€‚Ì‹È‚°—˜_v, ‘æ56‰ñ\‘¢‹­“x‚ÉŠÖ‚·‚éu‰‰‰ïu‰‰W, 1A18(JSASS-2014-3019), pp.48-50, •½¬26”N8ŒŽ6“ú`8ŒŽ9“ú, •l–k•¶‰»ƒZƒ“ƒ^[, 2014.

‘º“c—º, ˆäããđ¾, ‹{èNs, u‰F’ˆ\‘¢•¨‚̐L“W•”Þ—pƒRƒ“ƒxƒbƒNƒXƒe[ƒv‚Ì“WŠJ‹““®v, ‘æ56‰ñ\‘¢‹­“x‚ÉŠÖ‚·‚éu‰‰‰ïu‰‰W, 1A17(JSASS-2014-3018), pp.45-47, •½¬26”N8ŒŽ6“ú`8ŒŽ9“ú, •l–k•¶‰»ƒZƒ“ƒ^[, 2014.

‹{èNs, ‘º“c—º, ˆäããđ¾, —é]”¹‘¾, uƒRƒ“ƒxƒbƒNƒXƒe[ƒv‚ÌŠª‚«•t‚¯Žž‚Ì•ÏŒ`‚Ì—˜_‰ðv, ‘æ29‰ñ‰F’ˆ\‘¢Þ—¿ƒVƒ“ƒ|ƒWƒEƒ€, pp.1-11, •½¬25”N12ŒŽ3“ú, JAXA, ‘Š–ÍŒ´, 2013.


‚±‚ÌŒ¤‹†‚̈ê”Ԃ̐¬‰Ê‚́C2010”N5ŒŽ‚É‘Å‚¿ã‚°‚ç‚ꂽIKAROS‚Ì‹O“¹ãƒf[ƒ^‚Ɛ”’l—\‘ªŒ‹‰Ê‚Æ‚Ì”äŠr‚ðs‚¢C“WŠJ‹““®‚ɂ‚¢‚Ä‹c˜_‚Å‚«‚½‚±‚Æ‚Å‚·D‚Ü‚½CˆÈ‘O‚̉Ȍ¤”‹†uƒSƒTƒ}[Eƒ}ƒ‹ƒ`ƒ{ƒfƒBEƒ_ƒCƒiƒ~ƒNƒX‚Ì•Û‘¶Œ^‰ð–@v‚Å‚Í‚¶‚ß‚½C–Œ—v‘f‚̍‚¸“x‰»‚¨‚æ‚у‚ƒfƒ‹’᎟Œ³‰»Cu’´¬Œ^‰q¯‹Zp‚ð‰ž—p‚µ‚½ŽÀ‘H“I‚È‹O“¹ãƒT[ƒrƒXƒVƒXƒeƒ€‚Ì’T‹v‚ÅŽn‚ß‚½CŒ‡‘¹ƒf[ƒ^‚ð—L‚·‚éƒJƒƒ‰‰æ‘œ‚©‚ç‚Ì–Œ–ÊŒ`ó‚ÌŽOŽŸŒ³•œŒ³‚ÌŽè–@‚ð‚Ù‚ÚŠ®¬‚Å‚«‚½‚±‚Æ‚àC‚»‚ÌŒã‚ÌŒ¤‹†‚É”­“W‚µ‚½‚Æ‚¢‚¤ˆÓ–¡‚ŁCd—v‚Ȑ¬‰Ê‚Æ‚È‚è‚Ü‚µ‚½D‚Ü‚½CIKAROS‚ÉŠÖ‚·‚鋤“¯Œ¤‹†‚É‚æ‚èCAIAA‚©‚ç˜_•¶Ü‚ðŽóÜ‚Å‚«‚½‚±‚Æ‚àC‚Æ‚Ä‚àŠð‚µ‚¢¬‰Ê‚Æ‚È‚è‚Ü‚µ‚½D

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‰E‚̐}‚́CŒoŒ±“IŒÅ—L’¼Œð•ª‰ð‚ð—p‚¢‚½ƒ‚ƒfƒ‹’᎟Œ³‰»‚ÌŒvŽZ—á‚Å‚·DŽRè‚́C‚±‚̒᎟Œ³‰»Žè–@‚ÌŒ¤‹†‚ÅŠwˆÊ‚ðŽæ“¾‚µ‚Ä‚¢‚Ü‚·DŒÅ—L’¼Œð•ª‰ð‚Í—lX‚È•ª–ì‚ÅŽg‚í‚ê‚Ä‚¢‚Ü‚·‚ªC–Œ–Ê‚Ì“WŠJ‰ðÍ‚̂悤‚ÉŒvŽZŽžŠÔ‚Ì‚©‚©‚é–â‘è‚É‚¨‚¢‚ăpƒ‰ƒƒgƒŠƒbƒNƒXƒ^ƒfƒB‚ð‚·‚é‚悤‚ȏꍇ‚ɂ́CŒø—¦“I‚ɑÓ–‚ÈŒ‹‰Ê‚ðo‚·‚±‚Æ‚ª‚Å‚«‚éC‹­—͂ȃc[ƒ‹‚Æ‚È‚é‚ƍl‚¦‚Ä‚Ü‚·D‚à‚¿‚ë‚ñC‚»‚ê‚ð‚±‚Ì•ª–ì‚Å”F’m‚µ‚Ä‚à‚炤‚½‚߂ɂ́CŽÀŒ±Œ‹‰Ê‚ð’᎟Œ³‰»ƒ‚ƒfƒ‹‚Å—\‘ª‚µCŽÀŒ±Œ‹‰Ê‚©‚ç—\‘ª‚ª‘Ó–‚Å‚ ‚Á‚½‚±‚Æ‚ðŽ¦‚·‚ȂǁC’n“¹‚È“w—Í‚ª•K—v‚Æ‚È‚é‚Å‚µ‚傤‚ªC¥”ñC”F’m‚µ‚Ä‚¢‚½‚¾‚¢‚āCƒSƒbƒTƒ}[\‘¢‚ÌŒø—¦“I‚Ȑ݌vEŠJ”­‚ðŽÀŒ»‚µ‚Ä‚¢‚«‚½‚¢‚ƍl‚¦‚Ä‚¢‚Ü‚·D

‰E‚̐}‚́C”¼Œa1.2m‚Ì–Œ–Ê‚ð^‹ó‘w“à‚ʼn“S—Í“WŠJ‚µ‚½‚Æ‚«‚̉摜Œv‘ªŒ‹‰Ê‚Ì—á‚Å‚·D‚±‚ÌŒ¤‹†‚ð‚«‚Á‚©‚¯‚ɁCŒ‡‘¹ƒf[ƒ^‚ð—L‚·‚éŽÀŒ±ƒf[ƒ^‚Ɛ”’lŒvŽZŒ‹‰Ê‚©‚çŒoŒ±“IŒÅ—L’¼Œð•ª‰ð‚ð—˜—p‚µ‚ăf[ƒ^‚ªŒ‡‘¹‚µ‚½•”•ª‚àŠÜ‚ß‚Ä“WŠJŒ`ó‚𕜌³‚·‚邱‚Æ‚ª‚Å‚«‚é‚悤‚É‚È‚è‚Ü‚µ‚½D

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Hiraku Sakamoto, Yasuyuki Miyazaki, and Osamu Mori, Transient Dynamic Analysis of Gossamer Appendage Deployment Using Nonlinear Finite Element Method, Journal of Spacecraft and Rockets, 48(5), pp.881-890, September 2011, DOI: 10.2514/1.52552

Masahiko Yakazaki and Yasuyuki Miyazaki, Error Estimation of Low-Order Model for Gossamer Muti-body Structure, AIAA-2011-6281 (Proc. AIAA Modeling and Simulation Technologies Conference 2011), pp.1-9, August 2011, DOI:10.2514/6.2011-6281

Masahiko Yakazaki and Yasuyuki Miyazaki, Empirical Model Reduction of Geometrical Constrained Gossamer Structures, Journal of System Design and Dynamics, Special Issue of Asian Conference on Multi-Body Dynamics 2010, 5(3), pp.441-449, April 28, 2011, DOI: 10.1299/jsdd.5.441

Yoji Shirasawa, Osamu Mori, Yasuyuki Miyazaki, Hiraku Sakamoto, M Hasome, Nobukatsu Okuizumi, Horotaka Sawada, Hiroshi Furuya, Saburo Matunaga, and Michihiro Natori, Analysis of Membrane Dynamics using Multi-Particle Method for Solar Sail Demonstrator "IKAROS", AIAA-2011-1890 (Proc. 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference), pp.1-14, April 2011, DOI:10.2514/6.2011-1890

Hirotaka Sawada, Osamu Mori, Nobukatsu Okuizumi, Yoji Shirasawa, Yasuyuki Miyazaki, Michihiro Natori, Saburo Matunaga, Hiroshi Furuya, and Hiraku Sakamoto, Mission Report on The Solar Power Sail Deployment Demonstration of IKAROS, AIAA-2011- 1887 (Proc. 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference), pp.1-11, April 2011, DOI:10.2514/6.2011-1887

Masahiko Yakazaki and Yasuyuki Miyazaki, Low-Order Model of Spin Type Solar Sail Dynamics by Empirical Model Reduction, AIAA-2011-1891 (Proc. 52nd AIAA/ASME/ASCE/ AHS/ASC Structures, Structural Dynamics, and Materials Conference), pp.1-8, April 2011, DOI:10.2514/6.2011-1891

Yasuyuki Miyazaki, Yoji Shirasawa, Osamu Mori, Hirotaka Sawada, Nobukatsu Okuizumi, Hiraku Sakamoto, Saburo Matunaga, Hiroshi Furuya, and Michihiro Natori, Conserving Finite Element Dynamics of Gossamer Structure and Its Application to Spinning Solar Sail "IKAROS", AIAA-2011-2181 (Proceedings of 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference), pp.1-17, April 4-7, 2011, Denver, Colorado, DOI:10.2514/6.2011-2181


‚±‚ÌŒ¤‹†‚́C“ŒH‘åi“–Žžj‚̏¼‰iŽO˜Yæ¶‚ª‘ã•\ŽÒ‚Æ‚È‚Á‚Đi‚ß‚½Œ¤‹†‚Å‚·DÚ×‚͉Ȍ¤”ï‚̃f[ƒ^ƒx[ƒX‚ÅŠm”F‚Å‚«‚Ü‚·D‰äX‚ÌŒ¤‹†Žº‚ł́CƒJƒƒ‰‰æ‘œ‚ð—p‚¢‚Ä–Œ–Ê‚ÌŽOŽŸŒ³•œŒ³„’è‚ðs‚¢A–ŒŒ`ó‰ðÍ‚ðs‚¢‚Ü‚µ‚½D‚±‚ÌŒ¤‹†‚́CŒã‚ÌSPROUT‚Ì•¡‡–Œ–Ê“WŠJƒ~ƒbƒVƒ‡ƒ“‚É‚¨‚¯‚é‰æ‘œ‰ðÍ‚âCŒã‚̉Ȍ¤”‹†u‘åŒ^ƒSƒbƒTƒ}[‘½‘̉F’ˆ\‘¢•¨‚̉^“®—\‘ª–@‚ÌŠm—§‚Ɖ^“®‚Ì—‰ðv‚âuƒf[ƒ^‹ì“®Œ^ƒ‚ƒfƒŠƒ“ƒO‚É‚æ‚é‘åŒ^–Œ–Ê“WŠJ‰F’ˆ\‘¢•¨‚ÌŒ`óEƒ_ƒCƒiƒ~ƒNƒX„’èv‚╶‰ÈÈˆÏ‘õ”‹†uŠvV“I‰F’ˆ‰ÈŠw‚ðØ‚è‘ñ‚­æi“WŠJ\‘¢‚ÌŒ¤‹†E”­‹’“_Œ`¬v‚É‚¨‚¯‚é‰æ‘œ‰ðÍ‚Ö‚Æ”­“W‚µ‚Ä‚¢‚«‚Ü‚µ‚½D


‚±‚ÌŒ¤‹†‚̈ê”Ԃ̐¬‰Ê‚́C•Û‘¶Œ^‰ð–@‚̉ðÍƒR[ƒhNEDA‚ðƒo[ƒWƒ‡ƒ“ƒAƒbƒv‚µ‚½NEDA2.0‚ðŠJ”­‚µCJAXA‚̃\[ƒ‰[“d—̓ZƒCƒ‹¬Œ^ŽÀØ‹@IKAROS‚̃ZƒCƒ‹“WŠJ‚̃Vƒ~ƒ…ƒŒ[ƒVƒ‡ƒ“‚ðs‚¤‚ȂǁCŽÀÛ‚ÉIKAROS‚ÌŠJ”­‚É—˜—p‚Å‚«‚½‚±‚Æ‚Å‚·i—˜—p‚µ‚½Œ‹‰Ê‚Ì•]‰¿“™‚́CŽŸ‚̉Ȍ¤”ïuƒSƒTƒ}[‘½‘Ì—ÍŠw‚̉ð\‘¢v‚Ɉø‚«Œp‚ª‚ê‚Ü‚µ‚½jD‚»‚Ì‘¼C‰ðÍƒ‚ƒfƒ‹EƒR[ƒh‚ð‰ü—Ç‚µCŽÀŒ±‚ÅŒŸØ‚µ‚‚CŽÀ‹@‚Å‚àŽÀØ‚Å‚«‚éó‹µ‚É‚à‚Á‚Ä‚¢‚Á‚½‚Ì‚ªC‚±‚ÌŒ¤‹†‚Å‚µ‚½D‚»‚ê‚ç‚ÌŽå‚Ȑ¬‰Ê‚͈ȉº‚Ì’Ê‚è‚Å‚·D

‚Ü‚¸‚́CIKAROS‚̉ðÍ‚Å‚·DIKAROS‚͈ê•Ó‚ª14m‚ÅŒú‚³7.5ƒ~ƒNƒƒ“‚̐³•ûŒ`ó‚Ì”––Œ‚ð‰F’ˆ‚ŃXƒsƒ““WŠJ‚µ‚Ü‚µ‚½D‚»‚Ì“WŠJŽè‡‚́gˆêŽŸ“WŠJh‚Ɓg“ñŽŸ“WŠJh‚Ì2’iŠK‚É•ª‚©‚ê‚Ä‚¢‚Ü‚·iÚ×‚Íyoutube‚Ì“®‰æ‚ðŽQÆ‚­‚¾‚³‚¢jDIKAROS‚̉ðÍ‚ł́C1) Ü‚è–ڂ̃oƒl„«‚ÌŒø‰Ê‚ð•\‚·—v‘fC2) •â‹­ƒe[ƒv‚ÌŒø‰Ê‚ð•\‚·d‡–_—v‘fC3) –Œ“¯Žm‚̐ڐG‚ÌŒø‰Ê‚ð•\‚·—v‘fC4) „‘̂ƃP[ƒuƒ‹‚ÌŒ‹‡‚ÉŠÖ‚·‚éS‘©—v‘fC5) ‘äŒ`–Œ“¯Žm‚ð‚‚Ȃ®ƒuƒŠƒbƒW–Œ‚Æ‘äŒ`–Œ‚Æ‚ÌŒ‹‡‚É‚¨‚¯‚éd‡—v‘fC6) ŒõŠwƒpƒ‰ƒ[ƒ^‚ðl—¶‚µ‚½‘¾—zŒõˆ³‚ÌŒø‰Ê‚ð•\‚·•ª•zŠO—Í•\Œ»‚ȂǁC–Œ\‘¢Cƒ\[ƒ‰[ƒZƒCƒ‹\‘¢“Á—L‚ÌŒø‰Ê‚ðNEDA‚É‘g‚ݍž‚Ý‚Ü‚µ‚½D

‚»‚µ‚āCˆêŽŸ“WŠJ—p‚̃‚ƒfƒ‹‚ðMatlab”ÅNEDA‚É‘g‚ݍž‚ñ‚ŁC“ŒH‘å‚̍â–{æ¶‚ɉðÍ‚µ‚Ä‚¢‚½‚¾‚«C“ñŽŸ“WŠJ‚ÍC”Å‚ÌNEDA‚ōs‚¤‚±‚Æ‚É‚µ‚Ü‚µ‚½D‚»‚̍ہC IKAROS‚Å‚ÍŠJ”­ŠúŠÔ‚ª’Z‚©‚Á‚½‚½‚߁C‚»‚Ì’Z‚³‚É‚à‘Ήž‚Å‚«‚é‚悤C“ñŽŸ“WŠJ‚ÌŒvŽZ‚̍‚‘¬‰»‚ª•K—v‚Æ”»’f‚µCNEDA‚ðMPI‚Å•À—ñ‰»‚µ‚½CNEDA2.0‚ðŠJ”­‚µ‚Ü‚µ‚½D•À—ñ‰»‚ÌŽè–@‚Æ‚µ‚ẮC•¨‘̗̈æ‚ðŠô‰½Šw“I‚É•ªŠ„‚µCŠe—̈æ‚Ì•ÏŒ`‰ðÍ‚ð•À—ñ‚ōs‚¢‚È‚ª‚çCLagrangeæ”‚ÅŒ‹‡‚·‚éC—̈敪Š„Œ^‚Ì•À—ñ‰»‚ð—p‚¢‚Ü‚µ‚½DIKAROS‚ł́C6‚‚̗̈æi4‚‚̑äŒ`–Œ‚ƁC’T¸‹@–{‘̂ƁC–Œ‚Æ’T¸‹@‚ð‚‚Ȃ®ƒeƒU[j‚É•ª‚¯‚ÄŒvŽZ‚µ‚½Œ‹‰ÊC]—ˆ‚ÌNEDA‚æ‚è‚à4”{‹­‚̍‚‘¬‰»‚ðŽÀŒ»‚Å‚«C‚È‚ñ‚Æ‚©C‰ðÍ‚ð‰ñ‚·‚±‚Æ‚ª‚Å‚«‚Ü‚µ‚½D

‚±‚ÌŒ¤‹†‚Í2010”N3ŒŽ‚ɏI—¹‚µC‚»‚Ì2‚©ŒŽŒã‚Ì5ŒŽ21“ú‚ÉIKAROS‚ª‘Å‚¿ã‚°‚ç‚ꂽ‚킯‚Å‚·DNEDA2.0‚ðŠJ”­‚µC‚»‚ê‚ð‰F’ˆŒ¤‚ÅŽg‚Á‚Ä‚¢‚½‚¾‚¢‚½‚±‚ƂŁCŽÀ‹@ŠJ”­‚É‚±‚¤‚¢‚Á‚½‰ðÍ—˜_E‰ðÍƒR[ƒh‚ð“K—p‚·‚éÛ‚É’ˆÓ‚·‚ׂ«“_Ed—v‚È“_‚ðŠw‚Ô‚±‚Æ‚ª‚Å‚«C‘å•Ï‹Md‚È‹@‰ï‚Æ‚È‚è‚Ü‚µ‚½D

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‹{èNsCu¬Œ^ƒ\[ƒ‰[“d—̓ZƒCƒ‹ŽÀØ‹@IKAROS‚̃ZƒCƒ‹–Œ–ʂ̐”Šwƒ‚ƒfƒ‹‚ɂ‚¢‚āv‘æ25‰ñ‰F’ˆ\‘¢EÞ—¿ƒVƒ“ƒ|ƒWƒEƒ€u‰‰WCpp.72-75C2009”N12ŒŽ4“úC(“Ɓj‰F’ˆq‹óŒ¤‹†ŠJ”­‹@\C‘Š–ÍŒ´D

â–{Œ[C‹{èNsCXŽ¡C”’àV—mŽŸCu—LŒÀ—v‘f–@‚É‚æ‚éIKAROSƒZƒCƒ‹ˆêŽŸ“WŠJ‚Ì“®‰ðÍvC‘æ25‰ñ‰F’ˆ\‘¢EÞ—¿ƒVƒ“ƒ|ƒWƒEƒ€u‰‰WCpp.68-71C2009”N12ŒŽ4“úC(“Ɓj‰F’ˆq‹óŒ¤‹†ŠJ”­‹@\C‘Š–ÍŒ´D

Osamu Mori, Hirotaka Sawada, Fuminori Hanamura, Junichiro Kawaguchi, Yoji Shirasawa, Masayuki Sugita, Yasuyuki Miyazaki, Hiraku Sakamoto, and Ryu Funase, Development of Deployment System for Small Size Solar Sail Mission, Transactions of Japan Society for Aeronautical and Space Sciences, Space Technology Japan,@Vol. 7, pp.Pd_87-Pd_94, November 28, 2009, http://dx.doi.org/10.2322/tstj.7.Pd_87

‹{èNsCuƒSƒbƒTƒ}[‰F’ˆ\‘¢•¨‚Ì“WŠJ‰ðÍŽè–@vC‘æ58‰ñ—˜_‰ž—p—ÍŠwu‰‰‰ïu‰‰˜_•¶WCpp.425-426C2009”N6ŒŽ10“úC“ú–{Šwp‰ï‹cC“Œ‹žD

‹{èNsC—L“cŒö•ãCŽRè­•FCuƒ\[ƒ‰[ƒZƒCƒ‹‚Ì–Œ–ʐ݌v‚ÉŠÖ‚·‚éˆêlŽ@vC‘æ50‰ñ\‘¢‹­“x‚ÉŠÖ‚·‚éu‰‰‰ïu‰‰WCpp.232-234, 2008”N7ŒŽ30“ú\8ŒŽ1“úC–k‹ãBD

Yasuyuki MIYAZAKI, Dynamic Behavior of Spinning Square Solar Sail, Proceedings of the 18th Workshop on JAXA Astrodynamics and Flight Mechanics, pp. 38-42 , July 28-29, 2008, Sagamihara, Japan.

‚Ü‚½CŽÀÛ‚ÉIKAROS‚̉ðÍ‚ð‚µ‚Ä‚¢‚āC‚æ‚è’ZŠúŠÔ‚ɐ݌vEŠJ”­‚ð‚µ‚½‚èC‘Å‚¿ã‚°Œã‚Ì“úX‚̉^—p‚ɐ”’l‰ðÍŒ‹‰Ê‚ð–𗧂Ă½‚è‚·‚é‚ɂ́C’Z‚¢ŒvŽZŽžŠÔ‚ŃSƒbƒTƒ}[Eƒ}ƒ‹ƒ`ƒ{ƒfƒB‚̉^“®‚ð—\‘ª‚·‚é•K—v‚ª‚ ‚èC“Á‚ÉŠ´“x‰ðÍ‚â‚ ‚é’ö“x‚͈͓̔à‚ł̃pƒ‰ƒƒgƒŠƒbƒNEƒXƒ^ƒfƒB‚ð‚æ‚荂‘¬‚ɍs‚¦‚āC‚©‚C¸“x‚␔Šwƒ‚ƒfƒ‹‚ª‘Ó–‚È‚à‚Ì‚ª•K—v‚ƍl‚¦‚Ü‚µ‚½D‚»‚±‚ŁC•K—vÅ’áŒÀ‚̃tƒ‹ƒ‚ƒfƒ‹‰ðÍihigh fidelity model‚É‚æ‚é‰ðÍj‚ð‚à‚ƂɁC’᎟Œ³ƒ‚ƒfƒ‹‚ð\’z‚µC‚»‚ê‚ð—p‚¢‚ÄŠ´“x‰ðÍ“™‚ðs‚¤‚±‚Æ‚ðl‚¦‚Ü‚µ‚½D

‚±‚ÌŒ¤‹†‚ɂ‚¢‚ẮCŽRú±‚ª”ŽŽm‰Û’öŠw¶‚̍ ‚©‚çs‚Á‚Ä‚¨‚èC‚Ü‚¸‚́CKarhunen-Loève•ª‰ð‚ð—p‚¢‚āCŒn‚̃_ƒCƒiƒ~ƒNƒX‚Ì“Á’¥‚ð‚æ‚­‘¨‚¦‚½“KØ‚Èempirical eigenvector‚ð‹‚ßCƒtƒ‹ƒ‚ƒfƒ‹‚̏ó‘Ô‹óŠÔ‚©‚ç’᎟Œ³‚Ì•”•ª‹óŠÔ‚ɉ^“®‚ðŽË‰e‚µC’᎟Œ³‹óŠÔ“à‚ʼn^“®‚ðŒvŽZ‚µCÄ‚сCƒtƒ‹ƒ‚ƒfƒ‹‚Ì‹óŠÔ‚É–ß‚·C‚Æ‚¢‚¤‚±‚Æ‚ðs‚¢‚Ü‚µ‚½D‚»‚̗Ⴊ‰E‚̐}‚ŁC„‘̂ƃeƒU[‚ŘAŒ‹‚³‚ꂽ‰~Œ`–Œ‚©‚琬‚éƒVƒXƒeƒ€‚É‚¨‚¢‚āC„‘Ì‚ðŽp¨•Ï‰»‚³‚¹‚½‚Æ‚«‚Ì–Œ‚̒Ǐ]ó‹µ‚ð‚Ý‚½‚à‚Ì‚Å‚·Dƒtƒ‹ƒ‚ƒfƒ‹iÔj‚Æ1/10ƒ‚ƒfƒ‹i”jüj‚Í‚Ù‚Ú“¯‚¶‚à‚Ì‚É‚È‚è‚Ü‚·‚µCxÀ•W‚ÍyÀ–@‚Í‚Ù‚Úˆê’v‚µ‚Ä‚¢‚Ü‚·D

‚±‚̂悤‚ÈŒ¤‹†‚́C’᎟Œ³‰»–â‘肾‚¯‚Å‚È‚­CŽÀŒ±ƒf[ƒ^‚Ɛ”’lŒvŽZƒf[ƒ^‚ð—Z‡‚µ‚Ä‚æ‚萸“x‚Ì‚æ‚¢‰^“®—\‘ª‚ðs‚¤ê‡‚âCŒ‡‘¹ƒf[ƒ^‚ð—L‚·‚éŽÀŒ±ƒf[ƒ^‚ɑ΂µCŒvŽZŒ‹‰Ê‚ð—˜—p‚µ‚ÄŒ‡‘¹•”•ª‚ð•â‚¤ê‡‚ȂǁC—lX‚È‚à‚̂ɉž—p‚Å‚«‚é‚Í‚¸‚ŁC‚±‚ꂪCŽŸ‚̉Ȍ¤”ïuƒSƒTƒ}[‘½‘Ì—ÍŠw‚̉ð\‘¢v‚É”­“W‚µ‚Ä‚¢‚«‚Ü‚µ‚½D

[reference]

Masahiko Yamazaki and Yasuyuki Miyazaki, Empirical Model Reduction of Spinning Solar Sail, Transactions of Japan Society for Aeronautical and Space Sciences, Space Technology Japan, Vol.8, No.ists27, Pc_35-Pc_40, December 29, 2010, DOI: http://dx.doi.org/10.2322/tastj.8.Pc_35

ŽRè­•FC‹{èNsCuƒSƒTƒ}[‰F’ˆ\‘¢•¨‚ÌŒoŒ±“Iƒ‚ƒfƒ‹’᎟Œ³‰»vC‘æ18‰ñƒXƒy[ƒXEƒGƒ“ƒWƒjƒAƒŠƒ“ƒOEƒRƒ“ƒtƒ@ƒŒƒ“ƒXu‰‰WCpp.133-138C2010”N1ŒŽ29“úC“Œ‹žH‹Æ‘åŠwD

‚±‚ê‚ç‚ɉÁ‚¦‚āC–Œ–Ê‚Ì‹““®‚ðŒø—¦‚æ‚­C‚©‚C¸“x‚æ‚­–Í‹[‚·‚é‚ɂ́C–Œ‚̈³kŽž‚̍„«‚Ɛ܂è–ڂ̍„«‚ð‚«‚¿‚ñ‚Æ•]‰¿‚·‚邱‚Æ‚ª•K—v‚ƍl‚¦‚Ü‚µ‚½D‚»‚±‚ŁC‚Ü‚¸‚́C –Œ–ʂ̈³k„«‚̃‚ƒfƒ‹‰»‚ðC‚±‚ê‚܂ł̐üŒ`‹ßŽ—‚©‚çC—¼’[’PƒŽxŽ”‚̈ꎲˆ³k‚É‚æ‚éÀ‹üŒã‚ÌŽxŽ”½—Í‚Ì—˜_‰ð‚ÉŠî‚­”ñüŒ`‹ßŽ—‚É’u‚«Š·‚¦‚邱‚ƂŁCƒVƒFƒ‹—v‘f‚É‚æ‚éÀ‹üŒã‰ðÍ‚É‚æ‚­•„‡‚µ‚½Œ‹‰Ê‚𓾂邱‚Æ‚ª‚Å‚«‚Ü‚µ‚½D‚±‚ê‚ÉŠÖ‚µ‚ẮCˆäãi—L“cj‚ªISTS‚ÅŠw¶Ü‚ðŽóÜ‚µ‚Ä‚¢‚Ü‚·[Shoko Inoue, 2009]D‚Ü‚½C‚±‚ê‚ð‚æ‚èÚ×‚ɉðÍ‚µ‚½˜_•¶‚à—L“c‚ª2014”N‚É”­•\‚µ‚Ä‚¢‚Ü‚·[Shoko Arita, 2014]D


‚¹‚ñ’f‚ðŽó‚¯‚é‹éŒ`–Œ‚Ì‚µ‚í

[reference]

Shoko Arita, Takumi Okumiya, and Yasuyuki Miyazaki, Numerical model for prediction of wrinkling behavior on a thin-membrane structure, Mechanical Engineering Journal, Vo.1, No.4, Paper No.13-00086, pp.1-16, 2014, DOI: 10.1299/mej.2014se0041.

Shoko Inoue, Prediction Methods of Wrinkling in Thin-Membrane, Proceedings of 27th International Symposium on Space Technology and Science, ISTS2009-c-20s, pp.1-7, July 5-12, 2009, EPOCHHALL TSUKUBA, Tsukuba, Japan.

Yasuyuki Miyazaki, and Kosuke Arita, Simplified Model of Membrane for Wrinkle Analysis of Gossamer Structure, AIAA Paper 2008-2134, (CD-ROM Proceeding of 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Schaumburg), pp.1-10, IL, April 9, 2008, DOI:10.2514/6.2008-2134

Kosuke ARITA, Yasuyuki MIYAZAKI and Yoshitaka NAKAMURA, Evaluation of Numerical Analysis Model for Thin Membrane, CD-ROM Proceedings of 26th International Symposium on Space Technology and Science, ISTS2008-c-13, pp.1-6, June 1-8, 2008, Hamamatsu, Japan.

‚»‚µ‚āCÜ‚è–ڂɂ‚¢‚ẮCÜ‚è–Ú‚ð•t‚¯‚éÛ‚Ì’e‘Y«•ÏŒ`‚ðFEM‚ʼnðÍ‚µC‚»‚±‚©‚çC‚æ‚èŠÈ’P‚Ȑ܂è–ڍ„«ƒ‚ƒfƒ‹‚ð‚‚­‚è‚Ü‚µ‚½D‹ï‘Ì“I‚ɂ́CÜ‚è–Ú‚ð•t‚¯‚éH’ö‚ðCƒwƒ~ƒ“ƒO‰ÁH‚ÉŒ©—§‚āC’e‘Y«‰ðÍ‚ðs‚¢‚Ü‚µ‚½D

[reference]

Ryo Hayase, Yasuyuki Miyazaki, Hiroyuki Kamemura, and Shoko Inoue, A Study on Mechanical Model of Crease of Membrane, The 28th International Symposium on Space Technology and Science, 2011-c-31, pp.1-5, Okinawa Convention center, Okinawa, June 5-12, 2011.

‘£—ºC‹{èNsCu–Œ‚̐܂è–Ú‚Ì—ÍŠwƒ‚ƒfƒ‹‚ɂ‚¢‚Ă̈êlŽ@vC‘æ52‰ñ\‘¢‹­“x‚ÉŠÖ‚·‚éu‰‰‰ïCJSAS-S2010-3017Cpp.40-42C2010”N7ŒŽ21“ú|7ŒŽ23“úC‚Ƃ肬‚ñ•¶‰»‰ïŠÙC’¹ŽæD


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[reference]

“¡ˆä‘å•ãCuƒCƒ“ƒtƒŒ[ƒ^ƒuƒ‹ƒ`ƒ…[ƒu‚ð—p‚¢‚½–Œ–ʍ\‘¢•¨‚̐݌v–@‚ÉŠÖ‚·‚錤‹†vC•½¬2011”N“x“ú–{‘åŠw—HŠw•”CŽm˜_•¶C2012”N3ŒŽ.

“¡ˆä‘å•ãC‹{èNsCu•iŽ¿HŠw‚ð—p‚¢‚½ƒCƒ“ƒtƒŒ[ƒ^ƒuƒ‹ƒr[ƒ€‚̐݌v–@vC‘æ51‰ñ\‘¢‹­“x‚ÉŠÖ‚·‚éu‰‰‰ïCJSASS-2009-3071Cpp.205-207C2009”N7ŒŽ22“ú|7ŒŽ24“úC˜a‰ÌŽRŒ§—§î•ñŒð—¬ƒZƒ“ƒ^[BigEUC˜a‰ÌŽRD

‚±‚ê‚çC–Œ‚̈³k„«ƒ‚ƒfƒ‹CÜ‚è–Úƒ‚ƒfƒ‹CƒCƒ“ƒtƒŒ[ƒ^ƒuƒ‹ƒ`ƒ…[ƒu‚Ì“Á«•]‰¿‚Ȃǂ́C‘S‚āCuNEDA‚É‚æ‚é•Û‘¶Œ^‰ð–@‚Å‰ð‚¯‚é–â‘èC‚¨‚æ‚сC‚»‚ÌŒvŽZŒ‹‰Ê‚ðŽÀŒ±“™‚ÅŒŸØ‚Å‚«‚é–â‘è‚ð”@‰½‚É‘‚â‚·‚©v‚Æ‚¢‚¤‚±‚Æ‚ðl‚¦‚čs‚Á‚Ä‚¢‚Ü‚µ‚½DŽÀÛC‚±‚Ì‘¼‚É‚àC—Ⴆ‚΁C’ZŽüŠú‚Å‚ ‚é‰q¯‚ÌŽp¨‰^“®‚ðŒvŽZ‚µ‚‚C”\”N‚Æ‚¢‚¤’·ŠúŠÔ‚Ì‹O“¹ŒvŽZ‚ðs‚¤ÛCEM–@‚ð“K—p‚µC‘¼‚Ì•û–@‚Å‚Í”­ŽU‚µ‚ª‚¿‚È–â‘è‚Å‚àˆÀ’è‚ÉŒvŽZ‚Å‚«‚邱‚Æ‚ðŠm”F‚µ‚Ä‚¢‚Ü‚·D‚±‚̂悤‚ɁC•Û‘¶Œ^‰ð–@C“Á‚ɁC‰äXCHŠw‚Ì•ª–ì‚Å‚ÍEM–@‚ð“K—p‚µC‚æ‚èM—Š«‚̍‚‚¢ŒvŽZŒ‹‰Ê‚ðo‚·‚Æ‚¢‚¤—¬‚ê‚𐢂̒†‚ɍL‚ß‚Ä‚¢‚¯‚½‚ç‚È‚ÆŽv‚Á‚Ä‚¢‚Ü‚·D


‚±‚ÌŒ¤‹†‚ł́C‚±‚ê‚܂ł̉Ȍ¤”ï‚É‚æ‚錤‹†‚Ɉø‚«‘±‚«C–Œ–ʂ̐܂èô‚݁E“WŠJ•ûŽ®‚Ì•]‰¿–@‚ɂ‚¢‚ÄŒŸ“¢‚µC“Á‚ɁC“–ŽžCJAXA‚̃\[ƒ‰[ƒZƒCƒ‹Eƒ[ƒLƒ“ƒOƒOƒ‹[ƒv‚Å’ñˆÄ‚³‚ê‚Ä‚¢‚½‚¢‚­‚‚©‚̐܂èô‚݁E“WŠJ•ûŽ®‚Ì”äŠr‚ðs‚¢‚Ü‚µ‚½D‚Ü‚½C–ŒÞ‚̈³k„«‚ª–Œ–ʂɐ¶‚¶‚邵‚í‚Ì•ª•z‚É—^‚¦‚é‰e‹¿‚ɂ‚¢‚ÄŒŸ“¢‚µC‚æ‚萸“x‚æ‚­–Œ–ʂ̉^“®‚ð–Í‹[‚·‚é•û–@‚ðŽ¦‚µ‚Ü‚µ‚½D‚»‚̍ہC‹{è‚ªŠJ”­‚µ‚½‰ðÍƒR[ƒhNEDA‚¾‚¯‚Å‚Í‚È‚­CABAQUS‚Å‚à‰ðÍ‚ð‚µC—¼ŽÒ‚ð”äŠr‚·‚邱‚ƂŁCNEDA‚Ì—LŒø«‚à•¹‚¹‚ÄŽ¦‚µ‚Ü‚µ‚½D

‚Ü‚½CƒXƒsƒ““WŠJŒ^‚̃\[ƒ‰[ƒZƒCƒ‹‰F’ˆ‹@‚ÉŠÖ‚·‚éC–Œ–ʂ̉^“®‚Ì‘ŠŽ—‘¥‚ɂ‚¢‚ÄŒŸ“¢‚µC‘ŠŽ—ƒpƒ‰ƒ[ƒ^‚𗝘_“I‚É“±‚­‚Æ‚Æ‚à‚ɁC’nã(1G‚Å,1‹Cˆ³‰º‚ ‚é‚¢‚ÍŒ¸ˆ³‰ºE^‹ó‰º)‚É‚¨‚¯‚é–Œ–Ê‚Ì“WŠJŽÀŒ±‚©‚ç,‘ŠŽ—‘¥‚̑Ó–«‚ðŠm”F‚µ‚Ü‚µ‚½D‚½‚¾‚µCŽc”O‚È‚ª‚çC’nãŽÀŒ±‚ÌŒ‹‰Ê‚©‚ç‰F’ˆ‚Å‚Ì‹““®‚ð—\‘ª‚·‚邱‚Æ‚Í—eˆÕ‚Å‚Í‚È‚­Cq‹ó‹@‚â—Ž‰º“‚È‚Ç‚É‚æ‚é”÷¬d—͉º‚Å‚ÌŽÀŒ±‚ðs‚í‚È‚¢ŒÀ‚èC‰F’ˆ‚Å‚Ì‹““®‚ð—\‘ª‚Å‚«‚é‚悤‚È‘ŠŽ—‘¥‚𗝘_“I‚È— •t‚¯‚ð‚à‚Á‚č\’z‚·‚é‚͓̂‚¢‚Æ‚¢‚¤Œ‹‰Ê‚Æ‚È‚è‚Ü‚µ‚½i‚»‚ꂪCŒã‚̉Ȍ¤”‹†u‘åŒ^ƒSƒbƒTƒ}[‘½‘̉F’ˆ\‘¢•¨‚̉^“®—\‘ª–@‚ÌŠm—§‚Ɖ^“®‚Ì—‰ðv‚ɂ‚Ȃª‚Á‚Ä‚¢‚« ‚Ü‚µ‚½jD

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Hiraku Sakamoto, Yasuyuki Miyazaki, and K.C. Park, Finite Element Modeling of Sail Deformation Under Solar Radiation Pressure, Journal of Spacecraft and Rockets, Vol.44, No.3, pp.514-521, May-June 2007.

ŠÝ–{’¼ŽqC‹´–{Œ«ŽuC–¼Žæ’ʍOC‹{èNsC"¶•¨‚ÌŒ`‘ԕω»‚ÌŠÏŽ@‚ÉŠî‚­–Œ–ʍ\‘¢ƒ‚ƒfƒ‹‚Ì“WŠJ‹““®‚ÉŠÖ‚·‚錤‹†"C–Œ\‘¢Œ¤‹†˜_•¶W2006C“ú–{–Œ\‘¢‹¦‰ï, Vol.20, pp.59-63, 2007”N3ŒŽD

Kosuke Arita, Sotaro Hashiguchi, and Yasuyuki Miyazaki, Evaluation of deployment method of Spin-Deployable Membrane, ISAS 17th Workshop on Astrodynamics and Flight Mechanics, pp.251-254, July 23-24, 2007, Sagamihara.

‹{èNsC‹´Œû‘‘¾˜YC–öàV³OCuƒXƒsƒ““WŠJ–Œ–Ê‚Ì“WŠJ•ûŽ®‚Ì•]‰¿–@vC‘æ49‰ñ\‘¢‹­“x‚ÉŠÖ‚·‚éu‰‰‰ïu‰‰WCpp.205-207C2007”N7ŒŽ25`27“úC•Ÿ“‡D

‹{èNsCu–Œ–ʂ̃Šƒ“ƒNƒ‹•ª•z‚É‚¨‚¯‚é–Œ–ʂ̈³k„«‚̉e‹¿‚ɂ‚¢‚āvC‘æ22‰ñ‰F’ˆ\‘¢EÞ—¿ƒVƒ“ƒ|ƒWƒEƒ€˜_•¶WCpp.71-74C 2006”N12ŒŽ1“úC(“Ɓj‰F’ˆq‹óŒ¤‹†ŠJ”­‹@\C‘Š–ÍŒ´.

‹´Œû‘‘¾˜YC‹{èNsCu”’lŒvŽZ‚É‚¨‚¯‚éƒ\[ƒ‰[ƒZƒCƒ‹‚Ì–ŒŒ`ó‚Ì”äŠrvC‘æ50‰ñ‰F’ˆ‰ÈŠw‹Zp˜A‡u‰‰‰ïCD-ROMu‰‰WC3E02Cpp.1676-1681C2006”N11ŒŽC¬‘qD

Masashi Hashimoto, Naoko Kishimoto, Yasuyuki Miyazaki, and Michihiro C. Natori, Deployment Analysis on Membrane Structures Combined with Inflatable Tubes, CD-ROM Proceedings of 25th International Symposium on Space Technology and Science, ISTS06-c-13, pp.1-5, Kanazawa, Japan, June 2006.

Yasuyuki Miyazaki, Wrinkle/Slack Model and Finite Element Dynamics of Membrane, International Journal for Numerical Methods in Engineering, Vol.66, No.7, pp.1179-1209, May, 2006, DOI: 10.1002/nme.1588

‹´Œ³Œ«ŽuCŠÝ–{’¼ŽqC‹{èNsC–¼Žæ’ʍOCu•¡‡–Œ–ʍ\‘¢•¨‚Ì“WŠJ‰ðÍvC‘æ49‰ñ‰F’ˆ‰ÈŠw‹Zp˜A‡u‰‰‰ïCD-ROMu‰‰WC2C13, 2005”N11ŒŽCpp.1-4,L“‡D


‹{è‚Í2002”N“x–– ‚©‚çJAXA‚̃\[ƒ‰[ƒZƒCƒ‹‚̃[ƒLƒ“ƒOEƒOƒ‹[ƒv‚ÉŽQ‰Á‚µ‚Ä‚¨‚èC‚±‚ÌŒ¤‹†‚ł́Cƒ\[ƒ‰[ƒZƒCƒ‹‚ÌŽÀ‹@ŠJ”­‚É‚à‘Ήž‚Å‚«‚é‰ðÍƒR[ƒh‚ðŠJ”­‚µCŽÀÛ‚ɉ“S—Í“WŠJ–Œ‚Ì‹““®‚𒲂ׂ悤‚ƍl‚¦‚Ü‚µ‚½D

“Á‚ɁC–Œ–Ê“¯Žm‚̐ڐG‚̃‚ƒfƒ‹‰»‚ȂǁC×‚©‚ÈŒø‰Ê‚àl—¶‚É“ü‚ê‚邱‚Æ‚ª‚Å‚«‚é‚悤CNEDA‚ðƒAƒbƒvƒf[ƒg‚µ‚Ä‚¢‚«‚Ü‚µ‚½D‚»‚µ‚āCƒXƒsƒ““WŠJ–Œ‚Ì“WŠJ‰^“®‚ð•]‰¿‚·‚邽‚ß‚Ì‚¢‚­‚‚©‚ÌŽw•Wi“WŠJ—¦,—ݐϘcƒGƒlƒ‹ƒM–§“x,Å‘å˜cƒGƒlƒ‹ƒM•p“xj‚ð’ñˆÄ‚µC‚»‚ê‚ð—p‚¢‚Đ܏ô‚Ý•ûŽ®‚â“WŠJ•û–@‚Ì”äŠrE•]‰¿‚ðs‚¢‚Ü‚µ‚½DŽÀÛCÝŒvˆÄ‚ª‚¢‚­‚‚©‹“‚ª‚Á‚½‚Æ‚«‚ɁC‚»‚ê‚ç‚ð’è—Ê“I‚É”äŠr‚·‚éŽw•W‚ðÝ’è‚·‚é‚̂́CÝŒvEŠJ”­‚ł͋ɂ߂ďd—v‚Å‚ ‚èC‚»‚¤‚¢‚¤ó‹µ‚ª—ˆ‚é‚Å‚ ‚낤‚±‚Æ‚ðŒ©‰z‚µ‚āC‚±‚̂悤‚ÈŒ¤‹†‚ðs‚Á‚½‚Ì‚Å‚µ‚½D

[reference]

‹{èNsCŠâˆä—D‰ÀCuƒXƒsƒ““WŠJ–Œ–ʂ̐܂èô‚Ý•ûŽ®‚Ì•]‰¿–@‚ɂ‚¢‚āvC‘æ47‰ñ\‘¢‹­“x‚ÉŠÖ‚·‚éu‰‰‰ïu‰‰WCpp.254-256C2005”N7ŒŽC‹à‘òD

Y. Iwai and Y. Miyazaki, "Dynamics of Membrane Deployed by Centrifugal Force", CD-ROM Proceedings of 24th International Symposium on Space Technology and Science, ISTS04-c-12, pp.1-6, June 2004, Miyazaki.

Šâˆä—D‰ÀC‹{èNsCu‰“S—Í“WŠJŽ®ƒ\[ƒ‰[ƒZ[ƒ‹‚Ì“WŠJƒ_ƒCƒiƒ~ƒNƒXvC‘æ47‰ñ‰F’ˆ‰ÈŠw‹Zp˜A‡u‰‰‰ïu‰‰WCpp.1538-1543, 2003”N11ŒŽCVŠƒD


‚Ü‚½C2001”N‚©‚ç2002”N‚É‚©‚¯‚ăRƒƒ‰ƒh‘åŠw‚É—¯Šw’†‚ÉŠJ”­‚µ‚½Matlab”Å‚Ì–Œ‰ðÍƒR[ƒh‚ðC“–ŽžCƒRƒƒ‰ƒh‘å‚ÌPhD‚ÌŠw¶‚¾‚Á‚½â–{æ¶iŒ»E“ŒH‘åj‚ÉŽg‚Á‚Ä‚¢‚½‚¾‚«Câ–{æ¶CƒRƒƒ‰ƒh‘å‚ÌK.C.Park‹³Žö‚Æ‘åŒ^–Œ–ʍ\‘¢‚̐݌v–@‚ÌŒ¤‹†‚ði‚ß‚Ü‚µ‚½D

‘“àŠO‚ÌŽÀÛ‚̃\[ƒ‰[ƒZƒCƒ‹‚ÌŠJ”­ó‹µ‚ð‚Ý‚Ä‚¢‚é‚ƁC–Œ–Ê‚ª‘åŒ^‰ß‚¬‚āC¸–§‚É–Œ–Ê‚Ì’£—͂╽–Ê“x‚ðŠÇ—‚·‚é‚Æ‚±‚ë‚܂ł͏o—ˆ‚Ä‚¢‚È‚¢Š´‚ª‚ ‚è‚Ü‚·‚ªCd—ʂ̐§–ñ‚ªƒ\[ƒ‰[ƒZƒCƒ‹‚Ù‚Ç‚É‚ÍŒµ‚µ‚­‚È‚¢‚悤‚ȍ\‘¢‚Å‚ ‚ê‚΁Cƒ‚ƒWƒ…[ƒ‹\‘¢‚É‚µ‚āCŠeƒ‚ƒWƒ…[ƒ‹‚Ì–Œ–Ê‚Ì•½–Ê“x‚â’£—Í‚ðŠÇ—‚·‚邱‚Ƃ͉”\‚¾‚낤‚ƍl‚¦‚Ä‚¨‚èC‚»‚̂悤‚ȍ\‘¢•¨‚ðŠJ”­‚·‚邱‚Æ‚É‚È‚Á‚½‚çC‚±‚Ì“–Žž‚ÌŒ¤‹†‚ªŠˆ‚©‚³‚ê‚邱‚Æ‚É‚È‚é‚©‚Ȃƍl‚¦‚Ä‚¢‚Ü‚·D

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H. Sakamoto, Y. Miyazaki, and K.C. Park, Evaluation of Cable Suspended Membrane Structures for Wrinkle-Free Design, AIAA Paper 2003-1905, pp.1-10, April 2003. (Proceedings of 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM)), DOI:10.2514/6.2003-1905

‚³‚āC“–ŽžCJAXA‚ł́C‘½—±Žq–@‚ƌĂ΂ê‚éƒoƒlEƒ}ƒXŒn‚É‚æ‚è–Œ–Ê‚ð‹ßŽ—‚µ‚ĉðÍ‚·‚éŽè–@‚ð—p‚¢‚Ä‚¢‚Ü‚µ‚½‚ªC‚»‚̋ߎ—‚́CŠî–{“I‚É‚Í’¼ŠpŽOŠpŒ`–Œ‚𒼊pŽOŠpŒ`‚̃oƒl‚ŋߎ—‚·‚é‚Æ‚¢‚¤‚à‚̂ŁC‚»‚̔ėp«‚Ì‚È‚³‚É‹^–â‚ðŠ´‚¶C”CˆÓ‚Ì”ñ\‘¢ŠiŽq‚ɑΉž‚µ‚½‹ßŽ—–@‚ð’ñˆÄ‚µC–Œ—v‘f‚É‚æ‚é‰ðÍ‚Æ”äŠr‚·‚邱‚ƂŁC‚»‚̋ߎ—–@‚̑Ó–«‚ðŽ¦‚µ‚Ü‚µ‚½i‚à‚¿‚ë‚ñC‚µ‚í‚̉e‹¿‚ªŒø‚¢‚Ä‚­‚é‚悤‚È–â‘è‚É‚¨‚¢‚ẮCƒoƒlEƒ}ƒXŒn‚Å‚Í‚µ‚í‚Ì•ûŒü‚ªƒoƒl‚Ì•ûŒü‚Ì‚Ý‚ÉŒÀ’肳‚ê‚Ä‚µ‚Ü‚¤‚̂ŁC‹ßŽ—¸“x‚Í—Ž‚¿‚Ü‚·‚ªjD

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‹{èNsCŠâˆä—D‰ÀCuƒXƒsƒ““WŠJ–Œ–ʂ̐܂èô‚Ý•ûŽ®‚Ì•]‰¿–@‚ɂ‚¢‚āvC‘æ47‰ñ\‘¢‹­“x‚ÉŠÖ‚·‚éu‰‰‰ïu‰‰WCpp.254-256C2005”N7ŒŽC‹à‘òD

‹{èNsCŠâˆä—D‰ÀCu‰“S—Í“WŠJ–Œ–ʂ̃_ƒCƒiƒ~ƒNƒX‚ɂ‚¢‚āvC‘æ13‰ñƒXƒy[ƒXEƒGƒ“ƒWƒjƒAƒŠƒ“ƒOEƒRƒ“ƒtƒ@ƒŒƒ“ƒXu‰‰˜_•¶WCpp.59-64,2005”N1ŒŽC“Œ‹žD

Yasuyuki Miyazaki and Yuka Iwai, Dynamics Model of Solar Sail Membrane, 2004 ISAS 14th Workshop on Astrodynamics and Flight Mechanics, pp.32-37, July 2004, Sagamihara.

Y. Iwai and Y. Miyazaki, Dynamics of Membrane Deployed by Centrifugal Force, CD-ROM Proceedings of 24th International Symposium on Space Technology and Science, ISTS04-c-12, pp.1-6, June 2004, Miyazaki.

‚Ü‚½CƒCƒ“ƒtƒŒ[ƒ^ƒuƒ‹\‘¢‚ɂ‚¢‚Ä‚àˆø‚«‘±‚«Œ¤‹†‚ði‚߁Cƒ[ƒ‹ƒAƒbƒvƒ`ƒ…[ƒu‚̐L“W‚Ì“Á«‚ðCLS-DYNA‚ł̉ðÍ‚ƒ݂艺‚°Ž®‚ÌŽÀŒ±‚É‚æ‚è–¾‚ç‚©‚É‚µ‚Ü‚µ‚½D

[reference]

Yohei Hamamoto, Yasuyuki Miyazaki and Yoshitaka Nakamura, Deployment Dynamics of a Rolled-up Inflatable Tube, Collected Papers of 24th International Symposium on Space Technology and Science, ISTS04-c-13, pp.297-302, Miyazaki, Japan, October 2004.

•l–{—m•½C‹{èNsCuƒ[ƒ‹ƒAƒbƒvŽ®ƒCƒ“ƒtƒŒ[ƒ^ƒuƒ‹ƒ`ƒ…[ƒu‚Ì“WŠJ‹““®‚ɂ‚¢‚āvC‘æ47‰ñ‰F’ˆ‰ÈŠw‹Zp˜A‡u‰‰‰ïu‰‰WC pp.1526-1531, 2003”N11ŒŽCVŠƒD

Yohei Hamamoto and Yasuyuki Miyazaki, Stable Deployment of Rolled-up Inflatable Tube by Control of Gas Flow, IAC-03-I.2.07, CD-ROM Proceedings of 54th International Astronautical Congress (IAC), pp.1-6, Bremen, Germany, September 2003.


‚±‚ÌŒ¤‹†‚ł̈ê”Ԃ̐¬‰Ê‚́CNEDA‚ðŠJ”­‚µ‚½‚±‚Æ‚É‚ ‚è‚Ü‚·D

Œ³X‚́C“–ŽžCƒCƒ“ƒtƒŒ[ƒ^ƒuƒ‹\‘¢‚ÍŽŸ¢‘ã‚Ì‘åŒ^\‘¢•¨—lŽ®‚Æ‚µ‚Ä—L—ÍŽ‹‚³‚ê‚Ä‚¢‚½‚½‚߁C‚»‚ê‚܂ł̃Gƒlƒ‹ƒM•Û‘¶Œ^‚̉ð–@‚ðƒCƒ“ƒtƒŒ[ƒ^ƒuƒ‹\‘¢‚É“K—p‚µ‚悤‚ƍl‚¦C1999”N‚É‚Í‚ ‚é’ö“x‚̃R[ƒh‚ðŠJ”­‚µC‰E‚Ì“®‰æ‚̂悤‚ȃVƒ~ƒ…ƒŒ[ƒVƒ‡ƒ“‚ª‚Å‚«‚é‚Ü‚Å‚É‚Í‚È‚Á‚Ä‚¢‚Ü‚µ‚½D ‚»‚±‚ŁC2000”N‚©‚ç‚Í‚»‚ê‚ð‰ü—Ç‚µC¸“x‚Ì‚æ‚¢‰ðÍƒR[ƒh‚ð‚‚­‚èCƒCƒ“ƒtƒŒ\ƒ^ƒuƒ‹\‘¢•¨‚Ì“WŠJƒVƒ~ƒ…ƒŒ[ƒVƒ‡ƒ“‚ª‚Å‚«‚é‚悤‚ɂȂ낤‚ÆŽv‚¢C‰ÈŒ¤”ï‚ɉž•å‚µ‚½‚Ì‚Å‚µ‚½D

‚»‚µ‚āCÌ‘ð‚³‚êC‚Ü‚¸C2000”N“x‚́C—˜_‚ƃR[ƒh‚̉ü—Ç‚ðl‚¦‚Ü‚µ‚½D‚¿‚傤‚ǁC‚±‚ÌŒ¤‹†‚Æ“¯Žž•Às‚ŁC“ú–{‘åŠw—HŠw•”Œ¤‹†”ï‚É‚æ‚錤‹†uƒCƒ“ƒtƒŒ[ƒ^ƒuƒ‹ƒ`ƒ…[ƒu‚Ì”÷¬d—͉º‚Å‚Ì“WŠJŽÀŒ±v‚ðŽÀŽ{‚µ‚½‚½‚߁C‚±‚ÌŒ¤‹†‚ł́C‚Ü‚¸‚Í‚±‚Ì”÷¬d—ÍŽÀŒ±‚ÌŒ‹‰Ê‚ð–Í‹[‚Å‚«‚é‚悤‚É‚µ‚悤‚ƍl‚¦‚Ü‚µ‚½D

‚»‚ÌŒ‹‰Ê‚ª‰º‚̐}‚¨‚æ‚Ñ“®‰æ‚ŁCŠw“à‚Ì‹£‘ˆ“IŽ‘‹à‚ðƒXƒeƒbƒv‚ɁC‰ÈŒ¤”ï‚Å‚³‚ç‚Ȃ鐬‰Ê‚ðo‚·C‚¢‚¢Œ`‚ÌŒ¤‹†‚ª‚Å‚«‚½‚ÆŽv‚Á‚Ä‚¢‚Ü‚·D

‚»‚µ‚āC‚±‚Ì—˜_‚âƒR[ƒh‚̉ü—Ç‚ð‹@‚ɁCNEDA‚ðŠJ”­‚µ‚Ü‚µ‚½D‚»‚µ‚āCEM–@‚ɂ‚¢‚Ä‚æ‚è[‚­Œ¤‹†‚·‚é‚悤‚É‚È‚èC‚»‚Ì—˜_‚ðŠm‚©‚߂邽‚߂ɁC_“îƒ}ƒ‹ƒ`ƒ{ƒfƒBEƒ_ƒCƒiƒ~ƒNƒX‚̉ðÍƒR[ƒhlag‚ðŠJ”­‚µC‚»‚±‚Å“¾‚½’mŒ©‚ðNEDA‚É”½‰f‚·‚邱‚ƂŁCNEDA‚ð‚æ‚è‹­—͂ȃc[ƒ‹‚ɉü—Ç‚µ‚Ä‚¢‚«‚Ü‚µ‚½D‚Ü‚½C‚»‚ê‚Æ‚Æ‚à‚ɁC“–ŽžC‰F’ˆŒ¤‚Ì–¼ŽæŒ¤‚̏CŽm‰Û’ö‚ÌŠw¶‚Å‚ ‚Á‚½â–{æ¶iŒ»E“ŒH‘åj‚Ƀ}ƒ‹ƒ`ƒZƒ‹EƒCƒ“ƒtƒŒ[ƒ^ƒuƒ‹\‘¢‚̉ðÍ‚ÉNEDA‚ðŽg‚Á‚Ä‚à‚ç‚¢CƒR[ƒh‚Ì”÷’²®‚ð‚µ‚Ä‚¢‚«‚Ü‚µ‚½D

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Ž™‹Ê@„, ‹{è@Ns, "ƒGƒlƒ‹ƒMEƒ‚[ƒƒ“ƒ^ƒ€–@‚É‚¨‚¯‚é‰^“®•û’öŽ®‚Ì“±oŽè‡‚ƉðŽß‚ɂ‚¢‚Ä", “ú–{‹@ŠBŠw‰ï˜_•¶WiC•Òj, 69Šª684†, pp.1954-1959, 2003”N9ŒŽ.

‹{èNsC¢ƒGƒlƒ‹ƒMEƒ‚[ƒƒ“ƒ^ƒ€–@‚É‚¨‚¯‚éŠô‰½Šw“IS‘©ðŒ‚ÌŽæ‚舵‚¢‚ɂ‚¢‚āvC‘æ52‰ñ—˜_‰ž—p—ÍŠwu‰‰‰ïu‰‰˜_•¶WCpp.143-144C2003”N1ŒŽC“Œ‹žD

Hiraku Sakamoto, Michihiro C. Natori, and Yasuyuki Miyazaki, Deflection of Multicellular Inflatable Tubes for Redundant Space Structures, Journal of Spacecraft and Rockets, Vol.39, No.5, pp.695-700, September 2002.

Yasuyuki Miyazaki and Tsuyoshi Kodama, A Conservation Scheme of Energy and Momentum for Flexible Multibody Dynamics, Proceedings of The First Asian Conference on Multibody Dynamics 2002, T-3-1-4, pp.1-6, August 2002, Iwaki (CD-ROM).

Yasuyuki Miyazaki and Michiharu Uchiki, Deployment dynamics of Inflatable Tube, AIAA Paper 2002-1254, pp.1-10, April 2002. (CD-ROM Proceedings of 43rd AIAA/ASME/ASCE/ AHS/ASC Structures, Structural Dynamics, and Materials Conference ), doi: 10.2514/6.2002-1254.

ˆé•”—mC…–ì–­ŽqC‹{èNsCu”÷¬d—͉º‚ł̃Cƒ“ƒtƒŒ[ƒ^ƒuƒ‹ƒ`ƒ…[ƒu‚Ì“WŠJ‹““®i‘æ2•ñjvC‘æ43‰ñ\‘¢‹­“x‚ÉŠÖ‚·‚éu‰‰‰ïu‰‰WCpp.125-128C2001”N8ŒŽD

…–ì–­ŽqC‹{èNsC’†‘º‹`—²Cu”÷¬d—͉º‚ł̃Cƒ“ƒtƒŒ[ƒ^ƒuƒ‹ƒ`ƒ…[ƒu‚Ì“WŠJ‹““®vC‘æ44‰ñ‰F’ˆ‰ÈŠw‹Zp˜A‡u‰‰‰ïC1E-1C2000”N10ŒŽD


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[reference]

Masaki Namaizawa, Yoshitaka Nakamura, and Yasuyuki Miyazaki, Dynamic Analysis of Membrane Structures with Wrinkling Members, Proceedings of Asia-Pacific Vibration Conference, Vol.2, pp.782-787, December 1999.

Yasuyuki Miyazaki and Yoshitaka Nakamura, A Geometrically nonlinear finite element of flexible structures that conserves total energy, Modeling and Simulations based Engineering (Proceedings of ICES'98), Vol.1, pp.349-358, October 1998.

Yasuyuki Miyazaki and Yoshitaka Nakamura, Dynamic Analysis of Deployable Cable-Membrane Structures with Slackening Members, Proceedings of 21st International Symposium on Space Technology and Science, ISTS98-b-13, pp.1-6, May 1998.


College of Science and Technology, Nihon University
Department of Aerospace Engineering
Miyazaki and Yamazaki Laboratory
College of Science and Technology, Nihon University
7-24-1 Narashinodai, Funabashi, Chiba 274-8501, Japan
e-mail: asel (at) forth.aero.cst.nihon-u.ac.jp