Updated on 2026/03/10

写真a

 
NAKANISHI HIROKI
 
Organization
School of Engineering Professor
Title
Professor
External link

Degree

  • 博士(工学) ( 2010.3   東北大学 )

  • 修士(工学) ( 2003.3   東北大学 )

Research Interests

  • Space Engineering

  • Robotics

Research Areas

  • Informatics / Mechanics and mechatronics

  • Informatics / Robotics and intelligent system

  • Frontier Technology (Aerospace Engineering, Marine and Maritime Engineering) / Aerospace engineering

Education

  • Tohoku University   Graduate School, Division of Engineering   Dept. of Aeronautics and Space Engineering

    - 2003

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    Country: Japan

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  • Tohoku University   Faculty of Engineering   Dept. of Aeronautics and Space Engineering

    - 2001

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    Country: Japan

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Research History

  • Institute of Science Tokyo   School of Engineering   Professor

    2025.4

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    Country:Japan

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  • Tokyo Institute of Technology   School of Engineering   Associate Professor

    2017.6 - 2025.3

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    Country:Japan

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  • Tokyo Institute of Technology   Assistant Professor

    2013.4 - 2017.5

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    Country:Japan

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  • Japan Aerospace Exploration Agency

    2010.6 - 2013.3

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  • Tohoku University   Graduate School of Engineering, Department of Aerospace Engineering   Assistant Professor

    2010.3 - 2010.5

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Professional Memberships

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Papers

  • Modeling and Control of Contact Dynamics for a Free-Flying Space Robot in Target Capture Operation

    Hiroki Nakanishi

    2010.3

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    Language:English   Publishing type:Doctoral thesis  

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  • On-orbit demonstration of near real-time communication via Globalstar for time-domain astronomy

    Katsuki Tashiro, Shogo Nerome, Minori Fukuda, Hibiki Seki, Yusaku Ozeki, Hiroyuki Kobayashi, Yuki Amaki, Daiki Kobayashi, Kiyona Miyamoto, Kei Watanabe, Toshihiro Chujo, Hiroki Nakanishi, Satoru Ozawa, Saburo Matunaga, Yoichi Yatsu

    Acta Astronautica   240   208 - 218   2026.3

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    Publishing type:Research paper (scientific journal)   Publisher:Elsevier BV  

    DOI: 10.1016/j.actaastro.2025.12.003

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  • Scheduling Optimization of Landing-Site-Candidates Observation on Phobos from Quasi-Satellite-Orbit in MMX Mission Reviewed

    Yosuke TAKEO, Satoru OZAWA, Toshihiro CHUJO, Hiroki NAKANISHI, Tomoki NAKAMURA, Koji MATSUMOTO, Koji WADA, Hitoshi IKEDA

    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES   Vol. 68 ( No. 2 )   2025.3

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    Language:English   Publishing type:Research paper (scientific journal)  

    DOI: 10.2322/tjsass.68.84

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  • Star Tracker Algorithm for Large-Angle Attitude Change Reviewed

    Katsuki Tashiro, Toshihiro Chujo, Hiroki Nakanishi, Saburo Matunaga

    Journal of Evolving Space Activities   Vol. 2 ( No. 163 )   2024.9

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    Language:English   Publishing type:Research paper (scientific journal)  

    DOI: 10.57350/jesa.163

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  • Numerical Evaluation of Number of Observation Points and Preciseness in Multi-point Earth Observations Using Variable Shape Attitude Control Reviewed

    Yusaku OZEKI, Toshihiro CHUJO, Hiroki NAKANISHI, Saburo MATUNAGA

    Journal of Evolving Space Activities   Vol. 2 ( Article ID: 162 )   2024.9

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    Language:English   Publishing type:Research paper (scientific journal)  

    DOI: 10.57350/jesa.162

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  • Proposal of Magnetic Movable Robot on Membrane and Path-Planning Method for Moving Motion Reviewed

    Takaomi Chubachi, Hiroki Nakanishi

    Journal of Evolving Space Activities   Vol. 2 ( Article ID: 172 )   2024.9

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    Language:English   Publishing type:Research paper (scientific journal)  

    DOI: 10.57350/jesa.172

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  • INSPIRE: Challenge of 50 kg-class satellite to open up MeV gamma-ray astronomy Reviewed

    Jun Kataoka, Ryoji Iwashita, Kazuo Tanaka, Ryohei Mori, Shojun Ogasawara, Tomoya Suga, Nanase Koshikawa, Kei Watanabe, Moe Yasuda, Hiroyuki Kobayashi, Daiki Kobayashi, Keito Otsubo, Asuka Ohira, Yuki Amaki, Yusuke Arai, Katsuki Tashiro, Yusaku Ozeki, Yusei Kawaguchi, Daiki Yoshimura, Hideo Yoshida, Kenichiro Takahashi, Yoichi Yatsu, Toshihiro Chujo, Hiroki Nakanishi, Mitsunobu Onishi, Shinichiro Takeda

    Nuclear Instruments and Methods in Physics Research Section A: Accelerators, Spectrometers, Detectors and Associated Equipment   Vol. 1065 ( No. 169518 )   2024.8

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    Language:English   Publishing type:Research paper (scientific journal)  

    DOI: 10.1016/j.nima.2024.169518

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  • UNISEC CanSat の20 年–缶サットの奥深さと電子工作の面白さ–

    鶴田佳宏, 佐原宏典, 中西洋喜, 桒原聡文

    電子情報通信学会誌   2023.4

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    Language:Japanese  

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  • 無人システムに求められる「強さ」 Invited Reviewed

    中西洋喜

    計測と制御   2021.4

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    Language:Japanese  

    DOI: 10.11499/sicejl.60.248

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  • Development and Analysis of Debris Capturing System Using Bi-Stable Convex Spring Reviewed

    Hiroki NAKANISHI, Yuto MASUDA, Takaya OZAWA

    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN   Volume 18 ( Issue 6 )   2020.11

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    Language:English   Publishing type:Research paper (scientific journal)  

    DOI: 10.2322/tastj.18.356

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  • Significance of 3U CubeSat OrigamiSat-1 for space demonstration of multifunctional deployable membrane Reviewed

    Kosuke Ikeya, Hiraku Sakamoto, Hiroki Nakanishi, Hiroshi Furuya, Takashi Tomura, Ryoga Ide, Ryo Iijima, Yohei Iwasaki, Keigo Ohno, Keisuke Omoto, Takashi Furuya, Teruaki Hayashi, Masaki Kato, Sae Koide, Madoka Kurosaki, Yuki Nakatsuka, Shigeaki Okuyama, Reo Kashiyama, Junya Nakamura, Wataru Nio, Tsubasa Tsunemitsu, Yutaka Yamazaki, Keisuke Taga, Britta Hohmann, Towa Amamoto, Takaomi Chubachi, Sho Tamura, Hideaki Okada, Akihito Watanabe, Nobuyoshi Kawabata, Toshiyuki Hori, Hiroaki Ito, Takeshi Kuratomi, Yuya Shimoda, Nana Hidaka, Kazuki Watanabe, Ayako Torisaka, Masahiko Yamazaki

    Acta Astronautica   173   363 - 377   2020.8

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    Language:English   Publishing type:Research paper (scientific journal)   Publisher:Elsevier BV  

    DOI: 10.1016/j.actaastro.2020.04.016

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  • Dynamics Analysis of Weathercock like Passive Sun-oriented Control Using Solar Pressure Reviewed

    Hiroki NAKANISHI, Ryuhei TAKAGI, Mitsushige ODA

    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN   17 ( 4 )   483 - 490   2019.1

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    Publishing type:Research paper (scientific journal)   Publisher:Japan Society for Aeronautical and Space Sciences  

    DOI: 10.2322/tastj.17.483

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  • A Study on the End-Effector Exchange Mechanism of a Space Robot Reviewed

    Rui Qu, Yuto Takei, Mitsushige Oda, Hiroki Nakanishi, Armin Wedler, Kent Yoshikawa

    Journal of Mechanics Engineering and Automation   Volume 7 ( Number 5 )   2017.5

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  • On-orbit demonstration of tether-based robot locomotion in REX-J mission Reviewed

    Nakanishi, H., Yamazumi, M., Karakama, S., Oda, M., Nishida, S.-I., Kato, H., Watanabe, K., Ueta, A., Yoshii, M., Suzuki, S.

    Journal of Robotics and Mechatronics   29 ( 5 )   2017

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    Publishing type:Research paper (scientific journal)  

    DOI: 10.20965/jrm.2017.p0792

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  • REX-J ミッションにおける画像処理を用いたテザー移動の評価 Reviewed

    鈴木悟史, 吉井正広, 中西洋喜, 山隅允裕, 小田光茂, 上田敦史, 渡邊恵佑, 加藤裕基, 星 亜友美, 西田信一郎

    日本機械学会論文集   Vol. 81 ( No. 824 )   2015.3

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    Language:Japanese   Publishing type:Research paper (scientific journal)  

    DOI: 10.1299/transjsme.14-00298

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  • Vibration Analysis for the Extendable Robot Arm of REX-J Reviewed

    Hiroki Nakanishi, Satoshi Suzuki, Atsushi Ueta, Keisuke Watanabe, Hiroki Kato, Masahiro Yoshii, Shinichiro Nishida, Mitsushige Oda

    Transactions of the Japan Society for Aeronautical and Space Science, Space Technology Japan   Vol. 12 ( No. ists29 )   2015.3

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  • 宇宙ステーション補給機HTV 捕獲のハイブリッドモーションシミュレータの構築 Reviewed

    高橋 一平, 安孫子聡子, 姜欣, 辻田 哲平, 内山勝, 中西洋喜, 上野浩史, 小田光茂

    日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences   Vol. 62 ( No. 6 )   2014.12

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  • Development of Detachable Wrist Interface Mechanism (DWIM) for Dexterous Manipulator on Astronaut Supporting Robot Reviewed

    Yuto Takei, Mitsushige Oda, Hiroki Nakanishi

    Transactions of the Japan Society for Aeronautical and Space Science, Space Technology Japan   Vol. 12   2014.11

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  • 高精度画像処理アルゴリズムによる「いぶき」太陽電池パネル挙動計測 Reviewed

    鈴木悟史, 中村俊之, 吉井正広, 中島正勝, 中西洋喜, 本田瑛彦, 小田光茂

    日本機械学会論文集C編   Vol. 79 ( No. 807 )   2014.11

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  • EVA 支援ロボット実証実験REX-J の知能化技術 Reviewed

    上田敦史, 加藤裕基, 渡邊恵佑, 中西洋喜, 西田信一郎, 小田光茂

    人工知能学会誌   Vol. 29 ( No. 4 )   2014.7

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  • Contact Dynamics Analysis for HTV Capturing by SSRMS Reviewed

    Akihiko Honda, Mitsushige Oda, Hiroki Nakanishi, Satoshi Suzuki

    Transactions of the Japan Society for Aeronautical and Space Science, Space Technology Japan   Vol. 12   2014.6

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  • Modeling and Analysis of Tether-Based Mobile Robot Based on Flight Experiments Reviewed

    Daichi Hirano, Akinori Kobayashi, Kenji Nagaoka, Kazuya Yoshida, Hiroki Kato, Keisuke Watanabe, Atsushi Ueta, Satoko Abiko, Shinichiro Nishida, Mitsushige Oda, Hiroki Nakanishi, Masahiro Yoshii, Satoshi Suzuki

    2014 IEEE AEROSPACE CONFERENCE   2014

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    Language:English   Publishing type:Research paper (international conference proceedings)  

    DOI: 10.1109/AERO.2014.6836266

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  • Measurement of the "IBUKI" solar array panel's behavior using high precision image processing Reviewed

    Suzuki, S., Nakamura, T., Yoshii, M., Nakajima, M., Nakanishi, H., Honda, A., Oda, M.

    Nihon Kikai Gakkai Ronbunshu, C Hen/Transactions of the Japan Society of Mechanical Engineers, Part C   79 ( 807 )   2013

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  • 2P1-N02 A Study on Space Intra-Vehicular Activity Support Robot(Space Engineering and Robotics and Mechatronics)

    NISHIDA Shin-Ichiro, KATAYAMA Yasuhiro, KATO Hiroki, WATANABE Keisuke, UETA Atsushi, ODA Mitsushige

    The Proceedings of JSME annual Conference on Robotics and Mechatronics (Robomec)   2013   _2P1-N02_1 - _2P1-N02_4   2013

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    Language:Japanese   Publisher:The Japan Society of Mechanical Engineers  

    The cost of launch of a manned rocket and crew training are very high. Moreover, the crew's number and activity time are restricted and the required cost per time of crew work including these is large. JAXA is carrying out research and development of a intravehicular human support robot. This paper gives study results on a space robot supporting crew intra-vehicular activity.

    DOI: 10.1299/jsmermd.2013._2p1-n02_1

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  • Contact Dynamics Modeling for Snare Wire Type of End Effector in Capture Operation Reviewed

    Naohiro UYAMA, Kazuya YOSHIDA, Hiroki NAKANISHI, Mitsushige ODA, Satoshi Suzuki

    Transactions of the Japan Society for Aeronautical and Space Science, Aerospace Technology Japan   Vol. 10   2012

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  • Experimental Verification of Vivration Control of a Flexible Arm for REX-J Robotic Demonstration on JEM Reviewed

    Daichi Hirano, Kazuya Yoshida, Mitsushige Oda, Nakanishi

    Transaction of the Japan Society for Aeronautical and Space Science, Space Technology Japan   Vol. 10   2012

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  • Impedance-Based Contact Control of a Free-Flying Space Robot with a Compliant Wrist for Non-Cooperative Satellite Capture Reviewed

    Naohiro Uyama, Hiroki Nakanishi, Kenji Nagaoka, Kazuya Yoshida

    2012 IEEE/RSJ INTERNATIONAL CONFERENCE ON INTELLIGENT ROBOTS AND SYSTEMS (IROS)   4477 - 4482   2012

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    Language:English   Publishing type:Research paper (international conference proceedings)  

    DOI: 10.1109/IROS.2012.6386082

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  • Time-Optimal Detumbling Maneuver along an Arbitrary Arm Motion during the Capture of a Target Satellite Reviewed

    Tomohisa Oki, Satoko Abiko, Hiroki Nakanishi, Kazuya Yoshida

    2011 IEEE/RSJ INTERNATIONAL CONFERENCE ON INTELLIGENT ROBOTS AND SYSTEMS   625 - 630   2011

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    Language:English   Publishing type:Research paper (international conference proceedings)  

    DOI: 10.1109/IROS.2011.6048758

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  • Impedance-based contact control of a free-flying space robot with respect to coefficient of restitution Reviewed

    Naohiro Uyama, Daichi Hirano, Hiroki Nakanishi, Kenji Nagaoka, Kazuya Yoshida

    2011 IEEE/SICE International Symposium on System Integration, SII 2011   1196 - 1201   2011

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    Language:English   Publishing type:Research paper (international conference proceedings)  

    DOI: 10.1109/SII.2011.6147619

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  • Virtual Mass of Impedance System for Free-Flying Target Capture Reviewed

    Hiroki Nakanishi, Naohiro Uyama, Kazuya Yoshida

    IEEE/RSJ 2010 INTERNATIONAL CONFERENCE ON INTELLIGENT ROBOTS AND SYSTEMS (IROS 2010)   2010

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  • Analysis of Contact Dynamics for Free-Flying Target Capture Operation with Hybrid Simulation(Mechanical Systems) Reviewed

    NAKANISHI Hiroki, SATO Hayato, YOSHIDA Kazuya, SAWADA Hirotaka, ODA Mitsushige

    Transactions of the Japan Society of Mechanical Engineers Series C   76 ( 769 )   2294 - 2299   2010

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    Language:Japanese   Publisher:The Japan Society of Mechanical Engineers  

    In order to make space missions successful reliably and safely, numerical dynamics simulation is important. In the simulation, identifying the contact force model and parameters is a key issue. In general, the identification experiment of space systems on the ground is difficult because of the gravity. This paper describes a strategy for identifying the contact parameters using a hybrid simulator. The hybrid simulator includes fatal control time delay which varies the contact force. However, the contact parameter can be identified by comparing the results of the hybrid simulation and pure numerical simulations including a time delay model. In this method, that the control time delay has little influence on the determination of contact parameters. In this paper, the dynamics model, including the time delay that exists in a hybrid simulator, is studied in detail. For verification of this method, the determined contact parameters are compared with the result of the contact experiments with a real floating object.

    DOI: 10.1299/kikaic.76.2294

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  • Integrated experimental environment for orbital robotic systems, using ground-based and free-floating manipulators Reviewed

    Naohiro Uyama, Håavard Lund, Koki Asakimori, Yuki Ikeda, Daichi Hirano, Hiroki Nakanishi, Kazuya Yoshida

    2010 IEEE/SICE International Symposium on System Integration: SI International 2010 - The 3rd Symposium on System Integration, SII 2010, Proceedings   108 - 113   2010

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    Language:English   Publishing type:Research paper (international conference proceedings)  

    DOI: 10.1109/SII.2010.5708310

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  • Time-Optimal Manipulator Control for Management of Angular Momentum Distribution during the Capture of a Tumbling Target Reviewed

    Tomohisa Oki, Hiroki Nakanishi, Kazuya Yoshida

    ADVANCED ROBOTICS   24 ( 3 )   441 - 466   2010

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    Language:English   Publishing type:Research paper (scientific journal)  

    DOI: 10.1163/016918609X12619993300584

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  • Influence of Control Time Delay on the Dynamics of Satellite Capture Reviewed

    NAKANISHI Hiroki, KODAMA Masaaki, YOSHIDA Kazuya

    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES   7 ( 26 )   Pf_29 - Pf_34   2009

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    Language:English   Publisher:SPACE TECHNOLOGY JAPAN  

    One of the most important phases of satellite servicing operations by a space robot is the "contact" phase. During the contact between the end-effector and grasping point, there is a risk that the target and the robot can be pushed away from each other by the contact force. Therefore, the method to control the end-effector by the impedance control so as not to deflect the target was suggested. However, all of real control systems have the control time delay. In case of the target capture operation, the time delay of the impedance control makes the impulse of the contact larger. In this paper, to verify the effect of the time delay of the impedance control, experiments with a air-floating testbed and numerical simulations are carried out.

    DOI: 10.2322/tstj.7.Pf_29

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  • Time-Optimal Manipulator Control of a Free-Floating Space Robot with Constraint on Reaction Torque

    Tomohisa Oki, Hiroki Nakanishi, Kazuya Yoshida

    2008 IEEE/RSJ INTERNATIONAL CONFERENCE ON ROBOTS AND INTELLIGENT SYSTEMS, VOLS 1-3, CONFERENCE PROCEEDINGS   2828 - 2833   2008

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    Language:English   Publishing type:Research paper (international conference proceedings)  

    DOI: 10.1109/IROS.2008.4650835

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  • Balloon-borne telescope system for optical remote sensing of planetary atmospheres and plasmas Reviewed

    Makoto Taguchi, Kazuya Yoshida, Hiroki Nakanishi, Yasuhiro Shoji, Kohei Kawasaki, Junichi Shimasaki, Yukihiro Takahashi, Jun Yoshida, Daisuke Tamura, Takeshi Sakanoi

    Advances in Geosciences: Volume 7: Planetary Science (PS)   ,169-179   169 - 179   2007.1

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    Language:English   Publishing type:Part of collection (book)   Publisher:World Scientific Publishing Co.  

    DOI: 10.1142/6494-vol7

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  • Whole-body motion control for capturing a tumbling target by a free-floating space robot

    Tomohisa Oki, Hiroki Nakanishi, Kazuya Yoshida

    2007 IEEE/RSJ INTERNATIONAL CONFERENCE ON INTELLIGENT ROBOTS AND SYSTEMS, VOLS 1-9   2262 - 2267   2007

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  • Impedance Control of Free-flying Space Robot for Orbital Servicing Reviewed

    Nakanishi, H., Yoshida, K.

    Journal of Robotics and Mechatronics   18 ( 5 )   608 - 617   2006

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    Publishing type:Research paper (scientific journal)   Publisher:Robotics Society of Japan (RSJ)  

    DOI: 10.20965/jrm.2006.p0608

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  • On the capture of tumbling satellite by a space robot

    Kazuya Yoshida, Dimitar Dimitrov, Hiroki Nakanishi

    2006 IEEE/RSJ INTERNATIONAL CONFERENCE ON INTELLIGENT ROBOTS AND SYSTEMS, VOLS 1-12   4127 - +   2006

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    Language:English   Publishing type:Research paper (international conference proceedings)  

    DOI: 10.1109/IROS.2006.281900

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  • Impedance control for free-flying space robots - Basic equations and applications

    Hiroki Nakanishi, Kazuya Yoshida

    2006 IEEE/RSJ INTERNATIONAL CONFERENCE ON INTELLIGENT ROBOTS AND SYSTEMS, VOLS 1-12   3137 - +   2006

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    Language:English   Publishing type:Research paper (international conference proceedings)  

    DOI: 10.1109/IROS.2006.282334

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  • Dynamics, control and impedance matching for robotic capture of a non-cooperative satellite Reviewed

    K Yoshida, H Nakanishi, H Ueno, N Inaba, T Nishimaki, M Oda

    ADVANCED ROBOTICS   18 ( 2 )   175 - 198   2004

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    Language:English   Publishing type:Research paper (scientific journal)  

    DOI: 10.1163/156855304322758015

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  • Leonid Meteor Observer in LEO: a University Microsatellite to Observe the 2002 Leonid from Space

    Smaller Satellites: Bigger Business? Concepts, Applications and Markets for Micro/Nanosatellites in a New Information World   423-425   2002

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  • The TAKO (Target Collaborativize) Flyer

    a New Concept for Future Satellite ServicingSmaller Satellites: Bigger Business? Concepts, Applications and Markets for Micro/Nanosatellites in a New Information World, Edited by M. Rycroft, N. Crosby, SPACE STUDIES VOLUME 6, Kluwer Academic Publishers   6   397 - 399   2002

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Books

  • 宇宙デブリ捕獲・把持システムの開発

    中西洋喜

    宇宙ビジネスとスペースデブリ対策  2025.5  ( ISBN:9784860439385

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    Language:Japanese  

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  • ロボット工学ハンドブック

    中西洋喜, 他多数

    ロボット工学ハンドブック  2023.3  ( ISBN:9784339046793

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MISC

  • REX-Jにおける軌道上の照度変化を考慮した3次元復元に関する基礎実験

    天野萌, 鳴海智博, 木村真一, 鵜山尚大, 吉井正広, 鈴木悟史, 加藤裕基, 渡邊恵佑, 上田敦史, 西田信一郎, 中西洋喜, 小田光茂

    宇宙科学技術連合講演会講演集(CD-ROM)   58th   2014

  • REX-Jロボット位置・姿勢の計測のための画像処理方法

    鈴木悟史, 吉井正広, 山隅允裕, 中西洋喜, 小田光茂, 上田敦史, 渡邊恵佑, 加藤裕基, 西田信一郎

    宇宙科学技術連合講演会講演集(CD-ROM)   57th   2013

  • REX-Jにおけるテザーを用いた宇宙ロボットの移動実験

    山隅允裕, 中西洋喜, 小田光茂, 西田信一郎, 加藤裕基, 渡邊恵佑, 上田敦史, 吉井正広, 鈴木悟史

    宇宙科学技術連合講演会講演集(CD-ROM)   57th   2013

  • REX-Jにおける軌道上自律画像誘導に向けた画像取得に関する基礎実験

    益子裕尭, 天野萌, 鵜山尚大, 鳴海智博, 木村真一, 吉井正広, 鈴木悟史, 加藤裕基, 渡邊恵佑, 上田敦史, 西田信一郎, 中西洋喜, 小田光茂

    宇宙科学技術連合講演会講演集(CD-ROM)   57th   2013

  • フリーフライング宇宙ロボットにおける慣性特性を考慮した最適角運動量分配制御

    前田敏博, 中西洋喜, 大木智久, 吉田和哉

    ロボティクスシンポジア予稿集   15th   2010

  • 軌道上サービスロボットによる衛星捕獲時の反発係数制御

    鵜山尚大, 中西洋喜, 吉田和哉

    日本機械学会ロボティクス・メカトロニクス講演会講演論文集(CD-ROM)   2010   2010

  • Vibration Control of Flexible Arm for an Extravehicular Activity Robot on ISS

    平野大地, 中西洋喜, 吉田和哉, 上野泰平, 小田光茂

    日本ロボット学会学術講演会予稿集(CD-ROM)   27th   2009

  • The Analysis of the Contact Dynamics for Satellite Capture under Impedance Control with Control Time Delay

    中西洋喜, 児玉正明, 吉田和哉

    日本機械学会ロボティクス・メカトロニクス講演会講演論文集(CD-ROM)   2008   2008

  • 空気浮上実験装置を用いた非協力衛星とマニピュレータとの接触力学解析

    児玉正明, 中西洋喜, 吉田和哉

    アストロダイナミクスシンポジウム講演後刷り集(Web)   17th   2008

  • Experiments of the Adaptive Vibration Suppression Control for the Macro-Micro Manipulator using a Hybrid Simulation

    中西洋喜, 柴原匡, 吉田和哉

    日本機械学会ロボティクス・メカトロニクス講演会講演論文集(CD-ROM)   2007   2007

  • The Analysis of the Contact Dynamics for Capturing a Target with a Space Station Manipulator

    中西洋喜, 佐藤隼人, 吉田和哉, 澤田弘崇, 小田光茂

    日本機械学会ロボティクス・メカトロニクス講演会講演論文集(CD-ROM)   2007   2007

  • 超小型衛星による雷・sprite及び地球ガンマ線の観測

    上田真也, 高橋幸弘, 坂野井健, 田村大輔, 荘司泰弘, 吉田和哉, 中西洋喜

    大気圏シンポジウム   20th   2006

  • 宇宙望遠鏡TOPSが実現する惑星大気科学

    高橋幸弘, 坂野井健, 吉田純, 田村大輔, 上田真也, 吉田和哉, 中西洋喜, 荘司泰弘, 田口真

    大気圏シンポジウム   20th   2006

  • A Control Strategy of a Free-Floating Space Robot for Capturing a Tumbling Target Using Angular Momentum Distribution

    吉田和哉, 大木智久, NICOLAEV Dimitar Dimitrov, 中西洋喜

    日本機械学会ロボティクス・メカトロニクス講演会講演論文集(CD-ROM)   2006   2006

  • MEISS (Moving Eyes for Inspection of International Space Station)-Conceptual Design and Mission Analysis-

    吉田和哉, 妻木勇一, 増田和三, 山口孝夫, 中西洋喜, 恩田隼, 松本潤, 佐藤光

    日本機械学会ロボティクス・メカトロニクス講演会講演論文集(CD-ROM)   2006   2006

  • 空気浮上型テストベッドを用いた宇宙機の衝突模擬実験と接触力の数値モデリング

    田中大輔, 中西洋喜, 吉田和哉

    日本機械学会東北支部総会・講演会講演論文集   41st   2006

  • フリーフライング宇宙ロボットの手先インピーダンス制御-軌道上サービスミッションへの応用-

    中西洋喜, 吉田和哉

    ロボティクスシンポジア予稿集   11th   2006

  • 宇宙用柔軟ベースマニピュレータの制御におけるロバスト性向上

    吉田和哉, 渡邉紘充, 中西洋喜

    日本航空宇宙学会北部支部講演会講演論文集   2006   2006

  • Impedance Control for Free-flying Space Robot-Formulation of the Basic Equations-

    中西洋喜, 吉田和哉

    日本機械学会ロボティクス・メカトロニクス講演会講演論文集(CD-ROM)   2005   2005

  • Dynamics of Satellite Capture by Space Robot under Impedance Control

    中西洋喜, 吉田和哉, 稲場典康, 上野浩史, 小田光茂

    日本ロボット学会学術講演会予稿集(CD-ROM)   22nd   2004

  • Impedance Matching of Space Robot at Satellite Capture

    中西洋喜, 吉田和哉, 稲場典康, 上野浩史, 小田光茂, 西槙健司

    日本ロボット学会学術講演会予稿集(CD-ROM)   21st   2003

  • フリーフライングロボットを用いた衛星捕獲の力学解析

    中西洋喜, 吉田和哉

    日本航空宇宙学会北部支部講演会講演論文集   2003   2003

  • Force Feedback Control for Stable Robotic Satellite Capture

    稲場典康, 小田光茂, 吉田和哉, 中西洋喜

    日本ロボット学会学術講演会予稿集(CD-ROM)   21st   2003

  • Study on Contact Dynamics and its Control for Capturing a Non-cooperative Satellite.

    吉田和哉, 中西洋喜, 上野浩史

    日本機械学会年次大会講演論文集   2002 ( Vol.1 )   2002

  • LEOLEO(Leonid-Meteor Observer in Low Earth Orbit) II 小型衛星を用いた軌道上からの流星群観測

    中西洋喜, 渡辺敏暢, 加藤治久, 石上玄也, 西牧洋一, 丸木武志, 吉田和哉

    日本航空宇宙学会北部支部講演会講演論文集   2002   2002

  • 衛星捕獲における接触ダイナミクスと安定制御

    上野浩史, 稲場典康, 小田光茂, 吉田和哉, 中西洋喜

    誘導制御シンポジウム資料   19th   2002

  • LEOLEO(Leonid-meteor Observer in Low Earth Orbit)-II.

    中西洋喜, 加藤治久, 渡辺敏暢, 石上玄也, 西牧洋一, 丸木武志, 吉田和哉

    電子情報通信学会技術研究報告   101 ( 655(SAT2001 144-162) )   2002

  • The TAKO(Target Collaborativize)-Flyer a New Concept for Future Satellite Servicing.

    中西洋喜, 小笠原克久, 沼田亜紀子, 野口新, 吉田和哉

    電子情報通信学会技術研究報告   100 ( 638(SAT2000 125-139) )   2001

▼display all

Presentations

  • Relative Orbit Control Using Aerodynamic Force with a Shape-Change Function for Symmetrical Two-Wing Satellites

    Keito Otsubo, Toshihiro Chujo, Hiroki Nakanishi

    AAS/AIAA Space Flight Mechanics Meeting 2025 

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    Event date: 2025.1

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  • 紫外線天文学・陸・海観測超小型衛星うみつばめプロジェクトの開発状況

    安田萌恵, 谷津陽一, 小林大輝, 渡邉奎, 小林寛之, 天木祐希, 大坪恵人, 荒井湧介, 尾関優作, 田代克樹, 斉藤遼, 吉村大樹, 川口雄生, 吉田英生, 福田美実, 早津俊佑, 関響, 宮本清菜, 中条俊大, 中西洋喜, 若生一広, 青柳賢英, 武山芸英, 江野口章人, 白籏麻衣, 小林宏章, 村田悠, 中野徹, 卯尾匡史, 楠絵莉子, 飯塚千晴

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

    Venue:兵庫県姫路市  

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  • 可変形状姿勢制御による多地点観測のための観測スケジューリング手法の初期検討

    尾関優作, 中条俊大, 中西洋喜

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

    Venue:兵庫県姫路市  

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  • 柔軟な大型宇宙構造物の保守点検を目的とした磁気式移動ロボットの地上動作検証

    仲鉢貴臣, 中西洋喜

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

    Venue:兵庫県姫路市  

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  • 撮像画像を利用した自律軌道推定手法に関する研究

    田代克樹, 中条俊大, 小澤悟, 中西洋喜

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

    Venue:兵庫  

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  • 軌道上での可変形状機能による外力トルク変化結果を用いた環境力推定と角運動量制御への応用理論

    天木祐希, 渡邉奎, 宮本清菜, 小林寛之, 小林大輝, 中条俊大, 中西洋喜, 松永三郎

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

    Venue:兵庫県姫路市  

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  • 超小型ソーラーセイルの研究開発状況と深宇宙探査への展望

    高尾勇輝, PIERIS研究開発チーム, 中条俊大, 宮崎康行, 高尾勇輝, 渡邉奎, 荒井湧介, 中西洋喜, 谷津陽一, 森治, PIERIS研究開発チーム, 超小型ソーラーセイルRG

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

    Venue:兵庫県姫路市  

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  • 軌道上宇宙物体の資源管理と保護のための複数宇宙物体繋留システムの提案と繋留手順に関する研究

    高橋 健一郎, 中条 俊大, 中西 洋喜

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

    Venue:兵庫県姫路市  

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  • 軌道上サービスに向けた超小型宇宙用ロボットアームに関する検討

    小林寛之, 中条俊大, 中西洋喜

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

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  • 小型衛星編隊飛行システムへの可変形状空力制御の適用に関する検討

    大坪恵人, 渡邉奎, 天木祐希, 荒井湧介, 喜多村章悟, 中条俊大, 中西洋喜

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

    Venue:兵庫県姫路市  

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  • 深宇宙RVDにおける安定した分離を実現するドッキング機構の検討

    田中友悠, 中西洋喜

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

    Venue:兵庫県姫路市  

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  • 紫外線天文学・陸・海観測超小型衛星うみつばめのEM熱設計

    吉田英生, 大坪恵人, 正木青空, 福田美実, 早津俊祐, 上嶋茂諒, 小林大輝, 小林寛之, 谷津陽一, 中西洋喜, 中条俊大, 中野徹, 石橋剛志, 江野口章人, うみつばめ開発チーム

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

    Venue:兵庫県姫路市  

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  • 保持性と展開性を考慮した超小型衛星用保持開放機構の設計

    吉村大樹, 高橋健一郎, 安田萌恵, 荒井湧介, 正木青空, 渡邉奎, 小林寛之, 小林大輝, 中西洋喜, 中条俊大, 谷津陽一, 中野徹, 片岡淳, 田中香津生, 宮崎康行, ひばり開発チーム, うみつばめ開発チーム, GRAPHIUM開発チーム, PIERIS開発チーム

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

    Venue:兵庫県姫路市  

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  • ソーラーセイルによる月遷移軌道から月低軌道への軌道設計

    大上耕平, 中条俊大, 中西洋喜, 尾崎直哉

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

    Venue:兵庫県姫路市  

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  • 一軸ジンバル付き超小型ソーラーセイルの角運動量管理に関する研究

    中嶋哲大, 中条俊大, 中西洋喜

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

    Venue:兵庫県姫路市  

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  • 超小型ソーラーセイル「PIERIS」の軌道上実証計画

    荒井湧介, 川口雄生, 中条俊大, 菅野宏伸, 三貝龍輝, 島袋英明, 立川璃子, 宮崎康行, 渡邉奎, 戸村崇, 中山弦, 吉田英生, 斎藤遼, 正木青空, 高橋健一郎, 安田萌恵, 小林大輝, 吉村大樹, 大坪恵人, 小林寛之, 天木祐希, 小澤翼, 高尾勇輝, 中西洋喜, 谷津陽一, 松下将典, 杉原アフマッド清志, 森治, 酒井良次, 渡邊秋人, PIERIS研究開発チーム

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

    Venue:兵庫県姫路市  

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  • 可変形状機能を用いた編隊飛行技術実証衛星GRAPHIUMのミッション設計

    渡邉奎, 中条俊大, 中西洋喜, 谷津陽一, 小林寛之, 高橋健一郎, 天木祐希, 大坪恵人, 安田萌恵, 小林大輝, 荒井湧介, 田代克樹, 尾関優作, 吉村大樹, 川口雄生, 吉田英生, 宮本清菜, 片岡淳, 田中香津生, 森椋平, 須賀友也, 小笠原聖純, 山本一毅, GRAPHIUM衛星開発チーム

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

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  • 可変形状姿勢制御実証衛星HIBARIにおける教訓と今後の展望 ~HIBARIのはばたき~

    小林大輝, 渡邉奎, 小林寛之, 天木祐希, ?橋健一郎, 尾関優作, 田代克樹, 西尾陸, 斎藤遼, 川口雄生, 宮本清菜, 中条俊大, 中西洋喜, 谷津陽一, 松永三郎

    第68回宇宙科学技術連合講演会 

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    Event date: 2024.11

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  • A Study of Claw-type Docking Mechanism for Deep Space RVD

    Akihiro TOKUYASU, Tomoharu TANAKA, Hideo YOSHIDA, Hiroki NAKANISHI

    International Symposium on Artificial Intelligence, Robotics and Automation in Space (i-SAIRAS) 2024  2024.11 

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    Event date: 2024.11

    Language:English  

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  • Applying Fictitious Reference Iterative Tuning to Quaternion Feedback and Quantitative Evaluation

    Ozeki Yusaku, Chujo Toshihiro, Nakanishi Hiroki

    International Astronautical Congress 2024 

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    Event date: 2024.10

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  • Radiation-Induced Degradation of Si-CMOS Detector Aboard HIBARI Satellite in Low Earth Orbit

    Minori Fukuda, Yoichi Yatsu, Kei Watanabe, Hiroyuki Kobayashi, Kiyona Miyamoto, Yuki Amaki, Kenichiro Takahashi, Daiki Kobayashi, Yusaku Ozeki, Katsuki Tashiro, Ryo Saito, Yusei Kawaguchi, Toshihiro Chujo, Hiroki Nakanishi, on behalf of HIBARI Consortium

    Small Satellite Conference 2024 

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    Event date: 2024.8

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  • Concept Design of 50-kg Class Satellite 'INSPIRE': On-Orbit Demonstration of Orbit Control and Formation Flight by Atmospheric Drag Using Variable Shape Function

    Yuki Amaki, Kei Watanabe, Hiroyuki Kobayashi, Yoichi Yatsu, Toshihiro Chujo, Hiroki Nakanishi, Jun Kataoka, Kazuo Tanaka

    Small Satellite Conference 2024 

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    Event date: 2024.8

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  • Lessons Learned in the Operation of the HIBARI: Variable Shape Satellite

    Daiki Kobayashi, Kei Watanabe, Hiroyuki Kobayashi, Yuki Amaki, Kenichiro Takahashi, Yusaku Ozeki, Katsuki Tashiro, Riku Nishio, Ryo Saito, Yusei Kawaguchi, Kiyona Miyamoto, Toshihiro Chujo, Hiroki Nakanishi, Yoichi Yatsu, Saburo Matunaga

    Small Satellite Conference 2024 

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    Event date: 2024.8

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  • Feasibility Study of Technology Demonstration Mission for Integrated Attitude-Orbit Control of Solar Sail

    Yusuke Arai, Yusei Kawaguchi, Toshihiro Chujo, Hironobu Sugano, Ryuki Mikai, Hideaki Hideaki, Riko Tachikawa, Yasuyuki Miyazaki, Kei Watanabe, Takashi Tomura, Gen Nakayama, Hideo Yoshida, Ryo Saito, Sora Masaki, Kenichiro Takahashi, Yuki Amaki, Moe Yasuda, Daiki Kobayashi, Daiki Yoshimura, Keito Otsubo, Hiroyuki Kobayashi, Tsubasa Ozawa, Yuki Takao, Hiroki Nakanishi, Yoichi Yatsu, Masanori Matsushita, Ahmed Kiyoshi Sugihara, Osamu Mori, Momoko Fukunaga, Hiroyuki Ono, PIERIS R&D Team

    Small Satellite Conference 2024 

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    Event date: 2024.8

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  • パドルを用いた空力による編隊飛行制御手法に関する検討

    大坪恵人, 渡邉奎, 天木祐希, 小林大輝, 荒井湧介, 吉村大樹, 尾関優作, 川口雄生, 喜多村章悟, 中条俊大, 中西洋喜

    第34回アストロダイナミクスシンポジウム 

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    Event date: 2024.7

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  • 深宇宙サンプルリターンのための親子型探査機間の自動囲い込み式爪型ドッキング機構の検討

    田中友悠, 徳安彰大, 吉田英生, 中西洋喜

    第34回アストロダイナミクスシンポジウム 

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    Event date: 2024.7

    Language:Japanese   Presentation type:Oral presentation (general)  

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  • 可変形状空力FF実証のためのFFターゲット分離シーケンスおよび分離機構

    高橋健一郎, 渡邉奎, 中条俊大, 中西洋喜, 谷津陽一, 小林寛之, 天木祐希, 大坪恵人, 安田萌恵, 小林大輝, 荒井湧介, 田代克樹, 尾関優作, 吉村大樹, 川口雄生, 吉田英生, 宮本清菜, 片岡淳, 田中香津生, 森椋平, 須賀友也, 小笠原聖純, 山本一毅

    第34回アストロダイナミクスシンポジウム 

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    Event date: 2024.7

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  • 地球周回軌道における大気抵抗差とvision-based航法を用いた相対軌道制御に関する研究

    渡邉奎, 中条俊大, 中西洋喜, 谷津陽一, 小林寛之, 高橋健一郎, 天木祐希, 大坪恵人, 安田萌恵, 小林大輝, 荒井湧介, 田代克樹, 尾関優作, 吉村大樹, 川口雄生, 吉田英生, 宮本清菜, 片岡淳, 田中香津生, 森椋平, 須賀友也, 小笠原聖純, 山本一毅

    第34回アストロダイナミクスシンポジウム 

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    Event date: 2024.7

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  • Shadow-Aware Formation Flying Using Solar Radiation Pressure with Neural Network

    Shogo Kitamura, Keito Otsubo, Toshihiro Chujo, Hiroki Nakanishi

    IEEE International Conference on Space Robotics (iSpaRo), 2024 

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    Event date: 2024.6

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  • 小惑星表面探査のためのモーファブルビーム脚における 位置誤差補償に関する検討

    石井泰大, 中西洋喜

    日本機械学会ロボティクス・メカトロニクス講演会2024 

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    Event date: 2024.5 - 2024.6

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  • 初期接触のみにより拘束可能な深宇宙探査機のドッキング機構の検討と評価

    吉田英生, 田中友悠, 中西洋喜

    日本機械学会ロボティクス・メカトロニクス講演会2024 

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    Event date: 2024.5 - 2024.6

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  • Design Optimization of Cheetah Inspired Soft Running Robot

    Kai-Yun Tseng, Jhen-Heng Hu, Brijesh Patel, Hirohito Kobayashi, Yu-Hsun Chen, Ching-Wei Chuang, Hiroki Nakanishi, Satoshi Miura, Po Ting Lin

    The 20th International Conference on Automation Technology (Automation 2023) 

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    Event date: 2023.12

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  • 可変形状機能による外力トルク変化を利用した角運動量制御

    天木祐希, 中条 俊大, 中西洋喜, 松永三郎

    第67回宇宙科学技術連合講演会 

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    Event date: 2023.10

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  • A Study of Adaptive Capture Mechanism Based on Thigmotropism of Vine for Capturing Non-Cooperative Target

    Kenichiro Takahashi, Teruaki Hayashi, Hiroki Nakanishi

    34th International Symposium on Space Technology and Science  2023.6 

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    Event date: 2023.6

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  • Path Planning of Magnetic Movable Robot on Deployable Membrane

    Takaomi Chubachi, Hiroki Nakanishi

    34th International Symposium on Space Technology and Science  2023.6 

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    Event date: 2023.6

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  • 3-Axis Attitude Control Method of Spacecraft Using Reflectivity Control Device

    Hiroyuki Kobayashi, Toshihiro Chujo, Hiroki Nakanishi

    33rd AAS/AIAA Space Flight Mechanics Meeting 

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    Event date: 2023.1

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  • 可変反射率デバイスによる宇宙機の三軸姿勢制御に関する初期検討

    小林 寛之, 中条 俊大, 中西 洋喜

    第32回アストロダイナミクスシンポジウム 

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    Event date: 2022.7

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  • 接触屈性を模倣した適応的巻き付きによる軌道上非協力物体捕獲機構の研究

    ?橋健一郎, 林輝明, 中西洋喜

    ロボティクス・メカトロニクス講演会2022  2022.6 

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    Event date: 2022.6

    Venue:北海道札幌市  

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  • コンベックスばね型宇宙機捕獲機構の機能向上法に関する研究

    徳安彰大, 橋本拓哉, 中西洋喜

    ロボティクス・メカトロニクス講演会2022  2022.6 

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    Event date: 2022.6

    Venue:北海道札幌市  

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  • Development of a Truss Structure Grasping End-Effector for On-orbit servicing

    Hiroki Nakanishi, Naoki Kawaguchi

    33rd International Symposium on Space Technology and Science 

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    Event date: 2022.2 - 2022.3

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  • Revival and Successive Operation of 3U CubeSat OrigamiSat-1 with Multifunctional Deployable Membrane

    Shuhei Koike, Motoki Moritani, Misato Ishiwata, Shinya Tamura, Kazuki Nagai, Hiraku Sakamoto, Hiroki Nakanishi, Takashi Tomura, HIROSHI FURUYA, Akihito Watanabe

    33rd International Symposium on Space Technology and Science 

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    Event date: 2022.2 - 2022.3

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  • 軌道上非協力物体捕獲のための接触屈性を応用した 適応的巻き付き機構の検討

    林輝明, 中西洋喜

    第65回宇宙科学技術連合講演会 

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    Event date: 2021.11

    Venue:山形県山形市(オンライン開催)  

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  • 自由度相対位置固定が可能なトラス把持エンドエフェクタの 設計に関する研究

    川口直毅, 中西洋喜

    第65回宇宙科学技術連合講演会 

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    Event date: 2021.11

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  • On-Orbit Demonstration of Innovative Multifunctional Membrane Structure for Ultra-Lightweight Solar Arrays and Array Antennas by 3U CubeSat OrigamiSat-1

    Hiraku Sakamoto, HIROSHI FURUYA, Hiroki Nakanishi, Akihito Watanabe, Nobuyoshi Kawabata, Toshiyuki Hori, Hiroaki Ito, Takeshi Kuratomi, Yuya Shimoda, Nana Hidaka, Kazuki Watanabe

    Small Satellite Conference 2021 

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    Event date: 2021.8

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  • トラス構造を有する宇宙構造物捕獲のためのエンドエフェクタの設計及び運用に関する研究

    川口直毅, 鷲優希, 中西洋喜

    ロボティクス・メカトロニクス講演会2021 

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    Event date: 2021.6

    Venue:大阪府大阪市(オンライン)  

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  • 宇宙ロボットのためのモーファブルビームの動力学解析

    中塚祐貴, 中西洋喜

    ロボティクス・メカトロニクス講演会2021 

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    Event date: 2021.6

    Venue:大阪府大阪市(オンライン)  

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  • 大気抵抗を用いたスペースデブリの コントロールドデオービット法に関する研究

    林輝明, 中西洋喜

    第63回宇宙科学技術連合講演会 

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    Event date: 2019.11

    Venue:徳島県徳島市  

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  • 多機能展開膜実証3UキューブサットOrigamiSat-1の打ち上げ報告

    中西洋喜, 坂本啓, OrigamiSat-1開発チーム

    第63回宇宙科学技術連合講演会 

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    Event date: 2019.11

    Venue:徳島県徳島市  

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  • Development and analysis of debris capturing system using bi-stable convex spring

    Hiroki Nakanishi, Yuto Masuda, Takaya Ozawa

    32th International symposium on Space Technology and Science (ISTS2019) 

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    Event date: 2019.6

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  • スペースデブリ捕獲のための 球面螺旋形状インフレータブル機構の検討

    中塚祐貴, 中西洋喜

    ロボティクス・メカトロニクス講演会2019 

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    Event date: 2019.6

    Venue:広島市  

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  • 伸縮・曲げ機構を持つ超多自由度伸展式ロボットアームの研究

    岩崎陽平, 中西洋喜

    ロボティクス・メカトロニクス講演会2019 

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    Event date: 2019.6

    Venue:広島市  

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  • デブリ捕獲機構のためのコンベックスバネの力学解析

    増田雄斗, 中西洋喜

    ロボティクス・メカトロニクス講演会2019 

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    Event date: 2019.6

    Venue:広島市  

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  • スペースデブリ除去デバイス取り付けのための機構・制御の検討

    中西洋喜

    第8回スペースデブリワークショップ 

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    Event date: 2018.12

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  • コンベックスバネの力学特性を用いたデブリ把持機構の研究

    増田 雄斗, 中西 洋喜

    第62回宇宙科学技術連合講演会 

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    Event date: 2018.10

    Venue:福岡県久留米市  

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  • 多機能展開膜実証3UキューブサットOrigamiSat-1の地上検証と将来構想

    坂本啓, 中西洋喜

    第62回宇宙科学技術連合講演会 

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    Event date: 2018.10

    Venue:福岡県久留米市  

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  • A Study of an Astronaut Support Robot with a Morphable-beam-based Extendable Arm

    Hiroki Nakanishi, Yusuke Ota, Mitsushige Oda, Saburo Matunaga

    The International Symposium on Artificial Intelligence, Robotics and Automation in Space (i-SAIRAS 2018) 

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    Event date: 2018.6

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  • PRELIMINARY INVESTIGATIONS ON GROUND EXPERIMENTS OF VARIABLE SHAPE ATTITUDE CONTROL FOR MICRO SATELLITES

    Yusuke Shintani, Tsubasa Tsunemitsu, Kei Watanabe, Yohei Iwasaki, Kyosuke Tawara, Hiroki Nakanishi, Saburo Matunaga

    The International Symposium on Artificial Intelligence, Robotics and Automation in Space (i-SAIRAS 2018) 

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    Event date: 2018.6

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  • 多機能展開膜実証3UキューブサットOrigamiSat-1の開発

    坂本啓, 中西洋喜, OrigamiSat-1開発チーム

    第61回宇宙科学技術連合講演会 

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    Event date: 2017.10

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  • モーファブルビームを用いた宇宙用伸展式超多自 由度ロボットアームの開発

    太田裕介, 中西洋喜, 小田光茂, 松永三郎

    アストロダイナミクスシンポジウム 

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    Event date: 2017.7

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  • Development of CubeSat OrigamiSat-1 for Space Demonstration of Deployable Membrane Structure Technologies

    Hiraku Sakamoto, Hiroki Nakanishi, Hiroshi Furuya, Masahiko Yamazaki, Yasuyuki Miyazaki, Akihito Watanabe, Kazuki Watanabe, Ayako Torisaka

    34th International Symposium on Space Technology and Science (ISTS) 

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    Event date: 2017.6

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  • Development of a Retractable Twine Gripper for Debris-Capture

    Keisuke Taga, Hiroki Nakanishi, Mitsushige Oda

    International Symposium on Space Technology and Science 2017 

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    Event date: 2017.6

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  • Development of Nano-Satellite OrigamiSat-1with Highly Functional Deployable Membrane

    Hiroki NAKANISHI, Hiraku SAKAMOTO, Hiroshi FURUYA, Masahiko YAMAZAKI, Yasuyuki MIYAZAKI, Akihito WATANABE, Kazuki WATANABE, Ayako TORISAKA-KAYABA, Mitsushige ODA

    4th International Symposium on Solar Sailing 

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    Event date: 2017.1

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  • Development of Stereo Camera System for Accurate Observation of Deployable Membranes onboard CubeSat

    Yuya Shimoda, Kazuki Watanabe, Nobuomi Sakamoto, Takeshi Kuratomi, Nana Hidaka, Mutsuhiro Ogawa, Hiraku Sakamoto, Hiroki Nakanishi

    AIAA SciTech2017 

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    Event date: 2017.1

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  • ESTIMATION OF A DYANAMIC BEHAVIOR FOR A CAPTURE MISSION USING FLEXIBLE MECHANISM

    Akihiko Honda, Hiroki Nakanishi, Mitsushige Oda

    13th International Symposium on Artificial Intelligence, Robotics and Automation in Space (iSAIRAS 2016) 

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    Event date: 2016.6

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  • Development of stereo camera system for accurate observation of large deployable membranes in orbit

    Shimoda, Y., Watanabe, K., Sakamoto, N., Kuratomi, T., Naito, Y., Nishizawa, T., Sakamoto, H., Hiroki Nakanishi, Yamazaki, M.

    3rd AIAA Spacecraft Structures Conference 

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    Event date: 2016.1

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  • CubeSat Design for Space Demonstration of Deployable Membrane Structure Technologies

    Hiraku Sakamoto, Hiroki Nakanishi, Masahiko Yamazaki, Yasuyuki Miyazaki, Hiroshi Furuya, Akihito Watanabe, Kazuki Watanabe, M. Oda

    30th International Symposium on Space Technology and Science 

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    Event date: 2015.7

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  • Hybrid Motion Simulator for Capturing H-II Transfer Vehicle by Flexible Space Manipulator

    Ippei Takahashi, Satoko Abiko, Xin Jiang, Teppei Tsujita, Masaru Uchiyama, Hiroki Nakanishi, Hiroshi Ueno, Mitsushige Oda

    12th International Symposium on Artificial Intelligence, Robotics and Automation in Space (i-SAIRAS 2014)  2014.6 

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    Event date: 2014.6

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  • Tether-based Robot Locomotion Experiments in REX-J mission

    H. Nakanishi, M. Yamazumi, S. Karakama, M. Oda, S. Nishida, H. Kato, K. Watanabe, A. Ueta, M. Yoshii, S. Suzuki

    12th International Symposium on Artificial Intelligence, Robotics and Automation in Space  2014.6 

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  • The Design of key mechanical functions for a super multi-DoF and extendable Space Robotic Arm

    Kent Yoshikawa, Yuichiro Tanaka, Mitsushige Oda, Hiroki Nakanishi

    12th International Symposium on Artificial Intelligence, Robotics and Automation in Space  2014.6 

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    Event date: 2014.6

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  • 宇宙平板状構造物把持グリッパの開発

    中西洋喜, 荒川清一郎, 小田光茂, 西田 信一郎

    日本機械学会2013年度年次大会 

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    Event date: 2013.9

    Venue:鳥取県米子市  

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  • A Proposal of Human Support Robot for Intra-Vehicular Activity

    Shin-Ichiro Nishida, Yasuhiro Katayama, Masahiro Yoshii, Hiroki Nakanishi, Hiroki Kato, Keisuke Watanabe, Atsushi Ueta, Mitsushige Oda

    29th International Symposium on Space Technology and Science 

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    Event date: 2013.6

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  • 推進系取付のストラテジ・機構の検討

    中西洋喜, 河本 聡美

    第5回スペースデブリワークショップ 

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    Event date: 2013.1

    Venue:東京都調布市  

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  • デブリ捕獲機構の検討

    中西洋喜, 河本聡美

    第56回宇宙科学技術連合講演会 

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    Event date: 2012.11

    Venue:大分県別府市  

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  • 宇宙大型マニピュレータによる宇宙ステーション補給機「こうのとり」捕獲時の運動解析

    中西洋喜, 小田光茂, 鈴木悟史

    ロボティクス・メカトロニクス講演会2012 

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    Event date: 2012.5

    Venue:静岡県浜松市  

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  • Virtual Mass of Impedance System for Free-flying Target Capture

    Hiroki Nakanishi, Naohiro Uyama, Kazuya Yoshida

    2010 IEEE/RSJ International Conference on Intelligent Robots and Systems 

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    Event date: 2010.10

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  • 1A2-C06 Restitution Coefficient Control by a Free-Flying Space Robot for Capturing a Floating Satellite

    UYAMA Naohiro, NAKANISHI Hiroki, YOSHIDA Kazuya

    2010  The Japan Society of Mechanical Engineers

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    Event date: 2010

    Language:Japanese  

    This paper presents the Restitution Coefficient Control method by a free-flying space robot for capturing a floating target in space. One of the most difficult tasks by a space robot is to capture a floating object autonomously in space because too much momentum exchange might push the object away from the operational space of a space robot. In order to overcome this issue, the authors propose a new control method, named the Restitution Coefficient Control, for controlling the restitution coefficient between the manipulator hand of a space robot and a floating object. The restitution coefficient is defined through a simplified dynamics model, and the control input is derived from the inverse problem of the derivation of the restitution coefficient. The dynamics simulation verifies that the Restitution Coefficient Control is capable of realizing the restitution coefficient of zero.

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  • 軌道上サービスロボットによる衛星捕獲時の反発係数制御

    鵜山 尚大, 中西 洋喜, 吉田和哉

    ロボティクス・メカトロニクス講演会2010 

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    Event date: 2009.5

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  • 2P2-A14 The Analysis of the Contact Dynamics for Satellite Capture under Impedance Control with Control Time Delay

    NAKANISHI Hiroki, KODAMA Masaaki, YOSHIDA Kazuya

    2008.6  The Japan Society of Mechanical Engineers

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    Event date: 2008.6

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    One of the most important phases of satellite servicing operarions by a space robot is the "contact" phase. During the contact between the end-effector and grasping point, there is a risk that the target and the robot can be pushed away from each other by the contact force. Therefore, the method to control the end-effector by the impedance control so as not to deflect the target was suggested. However, all of real control systems have the control time delay. In case of the target capture operation, the time delay of the impedance control makes the impulse of the contact larger. In this paper, to velify the effect; of the time delay of the impedance control, experiments with a air-floating testbed and numerical simulations are carried out.

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  • むだ時間要素を含むインピーダンス制御を用いた非協力衛星捕獲の接触力学解析(宇宙ロボティクス・メカトロニクス)

    中西 洋喜, 児玉 正明, 吉田和哉

    ロボティクス・メカトロニクス講演会2008 

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    Event date: 2008.6

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  • Time-Optimal Manipulator Control of a Free-Floating Space Robot with Constraint on Reaction Torque

    Tomohisa Oki, Hiroki Nakanishi, Kazuya Yoshida

    2008 IEEE/RSJ INTERNATIONAL CONFERENCE ON ROBOTS AND INTELLIGENT SYSTEMS, VOLS 1-3, CONFERENCE PROCEEDINGS  2008 

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    Event date: 2008

    Language:English  

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  • 2A2-L08 The Analysis of the Contact Dynamics for Capturing a Target with a Space St ation Manipulator

    NAKANISHI Hiroki, SATO Hayato, YOSHIDA Kazuya, SAWADA Hirotaka, ODA Mitsushige

    2007.5  The Japan Society of Mechanical Engineers

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    Event date: 2007.5

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    In order to make space missions succeed surely and safely, it is necessary to assume various cases and take measures at the stage of development or designing an operation! plan. For this purpose, computer simulations play a key role in the development and operation of space systems because of the difficulty in performing ground-based hardware testing. In a dynamics simulation for space missions, the most difficult thing to model, and can easily cause sonic simulation errors is the contact force. In this paper, a novel strategy of identifying contact dynamics parameters by a hybrid simulator is described. The evaluation of the time delay which exists in the hybrid simulator is also described. The parameter identification with a hybrid simulator is substantially enabled by this evaluation.

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  • 2A2-L09 Experiments of the Adaptive Vibration Suppression Control for the Macro-Micro o Manipulator using a Hybrid Simulation

    NAKANISHI Hiroki, SHIBAHARA Masashi, YOSHIDA Kazuya

    2007.5  The Japan Society of Mechanical Engineers

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    Event date: 2007.5

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    Space arms such as SSRMS and JEMRMS are modeled as a macro-micro manipulator system, where a macro arm perform a passive flexible base during the operation of a micro arm. Paying attention to the reaction dynamics, it is possible to perform vibration suppression control with arbitrary positioning of the endtip. In this paper, the application of the adaptive control methods for the adaptive control under the parameter errors is verified through the hardware in the loop simulations.

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  • ハイブリッドシミュレーションによる宇宙冗長マクロ・マイクロマニピュレータの適応振動抑制制御(宇宙ロボット・メカトロニクス)

    中西 洋喜, 柴原 匡, 吉田和哉

    ロボティクス・メカトロニクス講演会2007 

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    Event date: 2007.5

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  • 宇宙ステーション搭載アームによるターゲット捕獲時の接触力学解析(宇宙ロボット・メカトロニクス)

    中西 洋喜, 佐藤隼人, 吉田和哉, 澤田弘崇, 小田光茂

    ロボティクス・メカトロニクス講演会2007 

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    Event date: 2007.5

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  • Whole-body motion control for capturing a tumbling target by a free-floating space robot

    Tomohisa Oki, Hiroki Nakanishi, Kazuya Yoshida

    2007 IEEE/RSJ INTERNATIONAL CONFERENCE ON INTELLIGENT ROBOTS AND SYSTEMS, VOLS 1-9  2007 

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    Event date: 2007

    Language:English  

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  • 角運動量分配制御を用いたフリーフライング宇宙ロボットによるターゲット捕獲

    吉田和哉, 大木 智久, 中西 洋喜

    ロボティクス・メカトロニクス講演会2006 

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    Event date: 2006.5

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  • 宇宙空間での検査機能を持ったロボティクス・システム構想検討 : 概念設計とミッション解析

    吉田和哉, 妻木 勇一, 増田 和三, 山口 孝夫, 中西 洋喜, 恩田 隼, 佐藤 光, 松本 潤

    ロボティクス・メカトロニクス講演会2006 

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    Event date: 2006.5

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  • 1P1-B11 空気浮上型テストベッドを用いた衛星捕獲の接触力学解析

    中西 洋喜, 田中大輔, 吉田和哉

    ロボティクス・メカトロニクス講演会2006 

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    Event date: 2006.5

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  • Development of a 10 Kg-class Micro Satellite for the Observation of Sprites and Atmospheric Lightning Events(WSANE2006)

    Kazuya Yoshida, Yukihiro Takahashi, Nakanishi Hiroki, Yasuhiro Shoji, Takafumi Horichi, Kazutaka Kimura, Shinya Ueda, Tomonao Hayashi, Koji Yokoyama, Shigeru Hosokawa, Yoshinari Masumoto

    Workshop for Space, Aeronautical and Navigateional Electronics 

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    Event date: 2006.4

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  • 525 Spacecraft Contact Dynamics Modeling and Experiment Using Air Floating Test Bed.

    Tanaka Daisuke, Nakanishi Hiroki, Yoshida Kazuya

    2006.3  The Japan Society of Mechanical Engineers

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    Event date: 2006.3

    Language:Japanese  

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  • 宇宙用柔軟ベースマニピュレータの制御におけるロバスト性の向上

    吉田和哉, 渡辺紘充, 中西洋喜

    日本航空宇宙学会北部支部2006年講演会論文集  2006.3 

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    Event date: 2006.3

    Language:Japanese  

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  • フリーフライング宇宙ロボットの手先インピーダンス制御

    中西洋喜, 吉田和哉

    第11回ロボティクスシンポジア論文集  2006.3 

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    Event date: 2006.3

    Language:Japanese  

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  • Development of a 10 Kg-class Micro Satellite for the Observation

    IEICE Technical Report  2006 

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    Event date: 2006

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  • On the capture of tumbling satellite by a space robot

    Kazuya Yoshida, Dimitar Dimitrov, Hiroki Nakanishi

    2006 IEEE/RSJ INTERNATIONAL CONFERENCE ON INTELLIGENT ROBOTS AND SYSTEMS, VOLS 1-12  2006 

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    Event date: 2006

    Language:English  

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  • Impedance control for free-flying space robots -basic equations and applications-

    Hiroki Nakanishi, Kazuya Yoshida

    IEEE International Conference on Intelligent Robots and Systems  2006 

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    Event date: 2006

    Language:English  

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  • Contact Dynamics Analysis of a Spacecraft in Micro Gravity with an Air-Floating Test Bed

    Proc. of the 25th International Symposium on Space Technology and Science (Selected papers)  2006 

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    Event date: 2006

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  • 1P1-B12 A Control Strategy of a Free-Floating Space Robot for Capturing a Tumbling Target Using Angular Momentum Distribution

    Yoshida Kazuya, Oki Tomohisa, Nicolaev Dimitar Dimitrov, Nakanisi Hiroki

    2006  The Japan Society of Mechanical Engineers

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    Event date: 2006

    Language:Japanese  

    A control strategy of a free-floating space robot for capturing a tumbling target is proposed, which uses angular momentum distribution. Angular momentum distribution is utilized in order to minimize the base attitude deviation of the robot. This minimization is assumed to be the priority task for target capturing. During the impact phase of the capturing operation impedance control that guarantees that the target is not pushed away is applied. In addition, during the post-impact phase a strategy for the control of the reaction wheels that absorbs the angular momentum stored in the manipulator arm is proposed.

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  • フリーフライング宇宙ロボットの手先インピーダンス制御 : 基礎方程式の定式化(宇宙ロボティクス2,生活を支援するロボメカ技術のメガインテグレーション)

    中西 洋喜, 吉田和哉

    ロボティクス・メカトロニクス講演会2005 

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    Event date: 2005.6

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  • ターゲット捕獲時におけるフリーフライング宇宙ロボットの手先インピーダンス制御

    中西洋喜, 吉田和哉

    ISAS 15th Workshop on Astrodynamics and Flight Mechanics  2005 

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    Event date: 2005

    Language:Japanese  

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  • フリーフライングロボットの手先インピーダンス制御-基礎方程式の定式化

    中西洋喜, 吉田和哉

    ロボティクス・メカトロニクス講演会’05 講演論文集(CD-ROM)1P1-S-053(1-4)  2005 

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    Event date: 2005

    Language:Japanese  

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  • Contact Dynamics and Control Strategy Based on Impedance Matching for Robotic Capture of a Non-cooperative Satellite

    Proc. of the RoManSy 2004, 15th CISM-IFToMM Symposium, Montreal, Canada  2004 

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    Event date: 2004

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  • CAPTURE OF A NON-COOPERATIVE SATELLITE BY A ROBOT MANIPULATOR UNDER THE IMPEDANCE CONTROL

    Proc. of 24th International Symposium on Space Technology and Science, Miyazaki, Japan (Selected papers)  2004 

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    Event date: 2004

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  • Impedance matching in capturing a satellite by a space robot

    K Yoshida, H Nakanishi

    IROS 2003: PROCEEDINGS OF THE 2003 IEEE/RSJ INTERNATIONAL CONFERENCE ON INTELLIGENT ROBOTS AND SYSTEMS, VOLS 1-4  2003 

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    Event date: 2003

    Language:English  

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  • Dynamics and Control for Robotic Capture of a Non-cooperative Satellite

    Proc. of iSAIRAS 2003, Nara, Japan, 19-23 May, 2003  2003 

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    Event date: 2003

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  • 衛星捕獲におけるコンタクトダイナミクスと制御の検討

    吉田和哉, 中西 洋喜, 上野 浩史

    日本機械学会年次大会2002 

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    Event date: 2002.9

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  • LEOLEO(Leonid-Meteor Observer in Low Earth Orbit)-II

    NAKANISHI Hiroki, KATOH Haruhisa, WATANABE Toshinobu, ISHIGAMI Genya, NISHIMAKI Youichi, MARUKI Takeshi, YOSHIDA Kazuya

    Technical report of IEICE. SAT  2002.2  The Institute of Electronics, Information and Communication Engineers

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    Event date: 2002.2

    Language:Japanese  

    In this paper, we propose a mission to observe various meteor showers from low Earth orbit in the years from 2004 to 2006. The Leonid-Meteor Observer in Low Earth Orbit(LEOLEO)-II satellite equips I.I.CCD imagers including a spectrometer. Meteor is the phenomena that dust from comets ablate and illuminate in the Earth's atmosphere. It is suggested that these dust may possibly contain organic materials and could be the origin of life on the Earth. The spectorometer detects specific emission of organic materials in the visible-UV band, which is difficult to observe from the ground due to the absorption by atmosphere. The mission will bring us precious data that has never obtained.

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  • Study on Contact Dynamics and its Control for Capturing a Non-cooperative Satellite

    YOSHIDA Kazuya, NAKANISHI Hiroki, UENO Hiroshi

    The proceedings of the JSME annual meeting  2002  The Japan Society of Mechanical Engineers

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    Event date: 2002

    Language:Japanese  

    This paper describes preliminary study on contact dynamics and its control for capturing non-cooperative satellite. Key-technologies of contact dynamics and goal of control capturing are investigated.

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  • The TAKO (Target Collaborativize) -Flyer : a New Concept for Future Satellite Servicing

    NAKANISHI H., OGASAWARA K., NUMATA A., NOGUCHI A., YOSHIDA K.

    Technical report of IEICE. SANE  2001.2  The Institute of Electronics, Information and Communication Engineers

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    Event date: 2001.2

    Language:Japanese  

    In order to keep the orbital environment safe and clean, free from collisions, the technology for satellite retrieval by robotic devices is highly expected. Rendezvous-docking and capture-berthing technologies are demonstrated recently. However, targets are requested to have specific fixtures to be grasped and optical cue markers for vision based control. Such targets are called collaborative. On the contrary, most of satellites in trouble are non-collaborative. The technology for the robotic capture of a non-collaborative satellite has not been established yet. This paper proposes the idea of the satellite servicing system named "The TAKO-Flyer". This system holds a target adaptively with a multiple articulated gripper system named "TAKO-Gripper", then makes the target collaborative.

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  • 展開構造/高速ダウンリンク技術実証機 OrigamiSat-1の打ち上げ報告

    坂本啓, 中西洋喜, 古谷寛, 池谷亘介, 飯島亮, 井手亮我, 大野奎悟, 大本圭祐, 岩崎陽平, 古谷航志, 奥山茂亮, 加藤雅己, 黒崎まどか, 小出紗瑛, 中塚祐貴, 林輝明, 柏山礼興, 中村惇哉, 仁尾航, 恒光翼, 山崎泰, B. Hohmann, 太田裕介, 多賀啓介, 上田直樹, 安部拓洋, 小沢尭也, 高木隆平, 寺田百合, 西澤匡士, 早崎一彬, 後藤宏太, 小川睦大, 間中一輝, 稲垣章弥, 天本十和, 仲鉢貴臣, 田村匠, 岡田秀明, 佐藤亮, 中野太輔, 中倉拓哉, 横松卓, 八島京平, 横山正太朗, 泉山将大, 戸村崇, 小田光茂, 鳥阪綾子, 渡邊秋人, 川端信義, 堀利行, 伊藤裕明, 倉冨剛, 下田優弥, 日高菜奈, 坂本信臣, 内藤祐貴, 渡辺和樹, 山崎政彦

    9th UNISEC Space Takumi Conference for Practical Study of Problem Finding and Solving in Space Systems  2019.3 

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  • リンク特異点とばね力を用いたデブリ除去デバイス取付機構の研究

    多賀, 中西洋喜, 平野 大地

    ロボティクス・メカトロニクス講演会2019  2019.6 

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    Venue:広島市  

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  • 展開構造/高速ダウンリンク技術実証機 OrigamiSat-1の打ち上げ報告

    坂本啓, 中西洋喜, 古谷寛, 池谷亘介, 飯島亮, 井手亮我, 大野奎悟, 大本圭祐, 岩崎陽平, 古谷航志, 奥山茂亮, 加藤雅己, 黒崎まどか, 小出紗瑛, 中塚祐貴, 林輝明, 柏山礼興, 中村惇哉, 仁尾航, 恒光翼, 山崎泰, B. Hohmann, 太田裕介, 多賀啓介, 上田直樹, 安部拓洋, 小沢尭也, 高木隆平, 寺田百合, 西澤匡士, 早崎一彬, 後藤宏太, 小川睦大, 間中一輝, 稲垣章弥, 天本十和, 仲鉢貴臣, 田村匠, 岡田秀明, 佐藤亮, 中野太輔, 中倉拓哉, 横松卓, 八島京平, 横山正太朗, 泉山将大, 戸村崇, 小田光茂, 鳥阪綾子, 渡邊秋人, 川端信義, 堀利行, 伊藤裕明, 倉冨剛, 下田優弥, 日高菜奈, 坂本信臣, 内藤祐貴, 渡辺和樹, 山崎政彦

    9th UNISEC Space Takumi Conference for Practical Study of Problem Finding and Solving in Space Systems  2019.3 

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  • 柔軟構造を持つ探査ローバーの状態推定と走行制御

    本田瑛彦, 中西洋喜, 小田光茂, 妻木俊道, 渡辺恵佑

    第59 回宇宙科学技術連合講演会  2015.10 

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  • 超小型衛星による薄膜展開技術の実証に向けたステレオカメラシステムの設計

    下田優弥, 渡辺和樹, 坂本信臣, 倉冨剛, 内藤佑貴, 坂本啓, 中西洋喜, 山崎政彦

    第59回宇宙科学連合講演会  2015.10 

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  • 多関節機構を用いた非協力衛星把持方法に関する研究

    濱島大輝, 本田瑛彦, 中西洋喜, 小田光茂

    第59 回宇宙科学技術連合講演会  2015.10 

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    Venue:鹿児島県鹿児島市  

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  • 超多自由度伸展ロボットアームの形状および位置姿勢計測に関する研究

    上田直樹, 田中優一郎, 吉川健人, 中西洋喜, 小田光茂

    ロボティクス・メカトロニクス講演会2015  2015.5 

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    Venue:京都  

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  • 塑性を持つように振る舞う棒状部材で構成された宇宙用伸展ロボットアームの制御方法に関する研究

    田中優一郎, 上田直樹, 吉川健人, 中西洋喜, 小田光茂

    ロボティクス・メカトロニクス講演会2015  2015.5 

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    Venue:京都  

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  • 動力学シミュレータを用いた非協力ターゲット捕獲装置の最適形状と運動状態に関する研究

    濱島大輝, 本田瑛彦, 中西洋喜, 小田光茂

    ロボティクス・メカトロニクス講演会  2015.5 

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    Venue:京都  

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  • Impedance-Based Contact Control of a Free-Flying Space Robot with a Compliant Wrist for Non-Cooperative Satellite Capture

    Naohiro Uyama, Hiroki Nakanishi, Kenji Nagaoka, Kazuya Yoshida

    2012 IEEE/RSJ International Conference on Intelligent Robots and Systems  2014.10 

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  • 超小型衛星による薄膜展開技術の実証に向けたステレオカメラシステムの設計II

    下田優弥, 渡辺和樹, 坂本信臣, 倉冨剛, 内藤佑貴, 日高奈菜, 小川睦大, 坂本啓, 中西洋喜

    第60回宇宙科学技術連合講演会  2016.9 

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  • 磁気吸着を用いた宇宙用エンドエフェクタの提案と把持力の定式化に関する研究

    安部 拓洋, 中西 洋喜, 小田 光茂

    第60回宇宙科学技術連合講演会  2016.9 

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  • デブリ捕獲のための高収納効率を持つワイヤ駆動型把持機構の検討

    多賀 啓介, 小田 光茂, 中西 洋喜

    第60回宇宙科学技術連合講演会  2016.9 

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  • コンベックスバネを用いた非協力衛星捕獲機構の動力学特性に関する研究

    小沢 尭也, 中西 洋喜, 小田 光茂

    第60回宇宙科学技術連合講演会  2016.9 

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  • 宇宙用磁気吸着式エンドエフェクタの基礎検討と試作

    安部拓洋, 中西洋喜, 小田光茂

    日本機械学会ロボティクス・メカトロニクス講演会2016  2016.6 

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  • 高収納効率と広い把持範囲を持つワイヤ駆動型把持機構の検討

    多賀啓介, 中西洋喜, 小田光茂

    日本機械学会ロボティクス・メカトロニクス講演会2016  2016.6 

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  • 超多自由度三次元伸展式ロボットアームの提案と制御方法に関する研究

    太田 裕介, 小田 光茂, 中西 洋喜

    第60回宇宙科学技術連合講演会  2016.9 

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  • 輻射圧トルクと調光デバイスを用いた受動的太陽指向制御

    高木 隆平, 中西 洋喜, 小田 光茂

    第60回宇宙科学技術連合講演会  2016.9 

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  • 非協力衛星捕獲機構に用いるコンベックスバネの動力学特性における研究

    小沢尭也, 中西洋喜, 小田光茂

    日本機械学会ロボティクス・メカトロニクス講演会2016  2016.6 

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  • Impedance-Based Contact Control of a Free-Flying Space Robot with Respect to Coefficient of Restitution

    Naohiro Uyama, Daichi Hirano, Hiroki Nakanishi, Kenji Nagaoka, Kazuya Yoshida

    2011 IEEE/SICE International Symposium on System Integration (SII)  2011.12 

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  • Preparation of the REX-J Mission to Demonstrate Technologies for the Astronaut Support Robot

    Mitsushige Oda, Masahiro Yoshii, Hiroki Nakanishi, Hiroki Kato, Atsushi Ueta, Yuusuke Hagiwara, Mitsuhiro Yamazumi

    28th International Symposium on Space Technology and Science  2011.6 

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  • Space Robotics Research in JAXA

    Hiroki Nakanishi, Mitsushige Oda

    10th BroadSky Workshop  2012.9 

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  • Vibration Analysis for the Extendable Robot Arm of REX-J

    Hiroki Nakanishi, Satoshi Suzuki, Atsushi Ueta, Keisuke Watanabe, Hiroki Kato, Masahiro Yoshii, Shinichiro Nishida, Mitsushige Oda

    29th International Symposium on Space Technology and Science  2014.6 

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  • せん断粘着を利用した平板状宇宙構造物把持機構の開発

    中西洋喜, 武井 悠人, 本田瑛彦, 小田光茂, 妻木 俊道

    日本機械学会ロボティクス・メカトロニクス講演会2014  2014.5 

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    Venue:富山県富山市  

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  • Modeling and Analysis of Tether-Based Mobile Robot Based on Flight Experiments

    Daichi Hirano, Akinori kobayashi, Kenji Nagaoka, Kazuya Yoshida, Satoko Abiko, Mitsushige Oda, Hiroki Nakanishi, Hiroki Kato, Keisuke Watanabe, Atsushi Ueta, Shinichiro Nishida, Masahiro Yoshii, Satoshi Suzuki

    IEEE Aerospace Conference 2014  2014.5 

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  • REX-J におけるテザーを用いた宇宙ロボットの移動実験

    山隅允裕, 中西洋喜, 小田光茂, 西田信一郎, 加藤 裕基, 渡邊 恵佑, 上田 敦史, 吉井 正広, 鈴木悟史

    第57 回宇宙科学技術連合講演会  2013.10 

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    Venue:鳥取県米子市  

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  • 高摩擦材を利用した平板状宇宙構造物把持システム

    中西洋喜, 荒川清一郎, 小田光茂

    日本機械学会ロボティクス・メカトロニクス講演会2013  2013.5 

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    Venue:茨城県つくば市  

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  • パドル角変更機能を用いた空力制御による編隊飛行制御手法の検討

    大坪恵人, 喜多村章悟, 中条 俊大, 中西洋喜

    第67回宇宙科学技術連合講演会 

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  • 超々小型衛星フォーメーションフライトの制御の検討

    久保田裕大, 野田篤司, 中西洋喜

    第 67 回宇宙科学技術連合講演会講演集 

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    Venue:富山県富山市  

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  • 3UキューブサットOrigamiSat-1 Lessons Learnedの次号機開発での活用

    坂本啓, 中西洋喜, 森谷元喜

    第 67 回宇宙科学技術連合講演会講演集 

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    Venue:富山県富山市  

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  • 可変形状姿勢制御を用いたひばりによる多地点観測の軌道上実証に関する詳細検討

    尾関優作, 中条俊大, 中西洋喜

    第67回宇宙科学技術連合講演会 

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    Venue:富山  

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  • 可変形状宇宙機における反射光が太陽方向決定に及ぼす影響の軌道上評価と対策の検討

    小林大輝, 中条 俊大, 中西洋喜, 松永三郎

    第67回宇宙科学技術連合講演会 

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  • 空気浮上型テストベッドを用いた宇宙機の衝突模擬実験と接触力の数値モデリング(学生賞IV)

    田中 大輔, 中西 洋喜, 吉田和哉

    日本機械学会東北支部講演会  2006.3 

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  • 気球搭載望遠鏡による惑星観測計画

    田口 真, 吉田和哉, 中西 洋喜

    第5回宇宙科学シンポジウム  2005.1 

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  • LEOLEO(Leonid-Meteor Observer in Low Earth Orbit)-II : 小型衛星を用いた軌道上からの流星群観測

    中西 洋喜, 加藤治久, 渡辺敏暢, 石上玄也, 西牧洋一, 丸木武志, 吉田和哉

    電子情報通信学会航行エレクトロニクス部門講演会  2002.1 

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  • The TAKO(Target Collaborativize)-Flyer : ターゲットを強力化させる衛星回収システム

    中西 洋喜, 小笠原克久, 沼田亜紀子, 野口新, 吉田和哉

    電子情報通信学会航行エレクトロニクス部門講演会  2001.2 

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  • 深宇宙RVD用のドッキング機構の検討

    徳安彰大, 田中友悠, 中西洋喜

    第 67 回宇宙科学技術連合講演会講演集 

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    Venue:富山県富山市  

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  • 両端に伸縮・曲げ機構を持つ 超多自由度伸展式ロボットアームの制御法の研究

    岩崎陽平, 中西洋喜

    第30回 アストロダイナミクスシンポジウム  2020.7 

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    Venue:神奈川県相模原市  

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  • 微小重力天体探査のためのモーファブルビーム脚での着陸に関する検討

    中塚祐貴, 中西洋喜

    ロボティクス・メカトロニクス講演会2020  2020.5 

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    Venue:石川県金沢市  

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  • 軌道上ロボットについて

    中西洋喜

    第9回ニュースペース研究会  2020.2 

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  • ADR作業の為の非協力的ターゲット捕獲・把持機構の検討

    中西洋喜

    第9回スペースデブリワークショップ  2021.2 

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    Venue:東京都調布市  

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  • 多機能展開膜実証3UキューブサットOrigamiSat-1の 成果と発展

    坂本啓, 中西洋喜

    第64回宇宙科学技術連合講演会  2020.10 

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    Venue:富山県富山市  

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  • デオービットデバイス取り付けのための低接触?把 持ハンドの設計に関する研究

    川? 直毅, 中西洋喜, 平野 ?地

    第64回宇宙科学技術連合講演会  2020.10 

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    Venue:富山県富山市  

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  • 接触検知型適応的巻き付きデバイスの研究

    林 輝明, 中西洋喜

    第64回宇宙科学技術連合講演会  2020.10 

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    Venue:富山県富山市  

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  • 非協力的ターゲット捕獲・把持機構の検討

    中西洋喜, 高橋健一郎, 川口直毅, 橋本拓哉, 徳安彰大

    第10回スペースデブリワークショップ  2022.11 

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    Venue:東京都調布市  

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  • 軌道上非協力物体捕獲のための接触屈性を応用した 適応的巻き付き機構 の設計に関する研究

    ?橋健一郎, 林輝明, 中西洋喜

    第66回宇宙科学技術連合講演会  2022.11 

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    Venue:熊本県熊本市  

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  • 宇宙膜展開構造物を保守する磁力式膜上移動ロボットの提案

    仲鉢貴臣, 中西洋喜

    第66回宇宙科学技術連合講演会  2022.11 

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    Venue:熊本県熊本市  

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  • 3UキューブサットOrigamiSat-1多機能展開膜の軌道上展張形状に関する考察

    坂本 啓, 小池 修平, 森谷 元喜, 石渡 美里, 永井 和希, 田村 真也, 仲鉢 貴臣, 中西 洋喜, 武田 裕貴, 中山 弦, 戸村 崇, 古谷 寛, 下田 優弥, 渡邊 秋人

    第66回宇宙科学技術連合講演会  2022.11 

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    Venue:熊本県熊本市  

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  • 初期接触のみにより拘束可能な宇宙機ドッキング機構の設計に関する研究

    田中友悠, 徳安彰大, 中西洋喜

    ロボティクス・メカトロニクス講演会2023  2023.6 

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    Venue:愛知県名古屋市  

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  • Input Shapingを用いた可変形状宇宙機の形状変化時に発生する振動の抑制と姿勢制御

    西尾陸, 中条俊大, 佐藤泰貴, 中西洋喜

    第32回スペース・エンジニアリング・コンファレンス  2023.11 

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    Venue:秋田県仙北市  

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  • 分離-ランデブドッキングを用いた軌道上組立て/構造再構成手法に関する概念検討

    小林寛之, 中条俊大, 中西洋喜

    第32回スペース・エンジニアリング・コンファレンス  2023.11 

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    Venue:秋田県仙北市  

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  • 展開構造/高速ダウンリンク技術実証機 OrigamiSat-1の開発

    中西洋喜, 坂本啓

    UNISEC Takumi Conference  2018.3 

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  • 低コストな国際宇宙ステーション投棄のための定量的トレードオフ

    池谷 亘介, 小田 光茂, 中西 洋喜, 坂本 啓

    日本機械学会 2018年度年次大会  2018.9 

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  • 無人システムに求められる「強さ」

    中西洋喜

    2021.4 

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Awards

  • 一般表彰スペースフロンティア

    2025   日本機械学会宇宙工学部門  

    ひばりプロジェクトチーム

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  • 一般表彰スペースフロンティア

    2014   日本機械学会宇宙工学部門  

    EVA支援ロボット実証実験「REX-J」開発/運用チーム

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  • 経済産業省

    2014   社会人基礎力を育成する授業30選入選

    中西洋喜・東京工業大学

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  • Student Best Presentation Award

    2003  

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    Country:Japan

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  • 2003年大学院研究奨励賞

    2003   社団法人自動車技術会  

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    Country:Japan

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Research Projects

  • Study of low-reaction robotic systems capable of moving on space membrane structures

    Grant number:24K07416  2024.4 - 2027.3

    Japan Society for the Promotion of Science  Grants-in-Aid for Scientific Research  Grant-in-Aid for Scientific Research (C)

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    Grant amount:\4550000 ( Direct Cost: \3500000 、 Indirect Cost:\1050000 )

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  • A study of an super-multidegree-of-freedom capture mechanism for non-cooperative spacecraft capture that mimics a thigmotropism of vines.

    Grant number:20K04396  2020.4 - 2023.3

    Japan Society for the Promotion of Science  Grants-in-Aid for Scientific Research  Grant-in-Aid for Scientific Research (C)

    Nakanishi Hiroki

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    Grant amount:\4290000 ( Direct Cost: \3300000 、 Indirect Cost:\990000 )

    In this research project, the research group proposed a modular type coiling mechanism that focuses on a thigmotropism of vines as a mechanism for actively capturing space debris. The unit module consists of a link with a joint and a contact detector. The capture mechanism consists of the unit modules. Each link rotates triggered by a contact force to mimic the coiling of a plant. The motion plan and algorithm for capturing the target were clarified. Then, a real capture mechanism is designed and developed a prototype. Experiments and simulations demonstrated that the mechanism is able to capture the target by wrapping around the free-flying target.

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  • Research and Demonstration for Design and Its Advanced Attitude Control Methods of Reconfigurable Space Systems with Shape Change Function

    Grant number:17H01349  2017.4 - 2020.3

    Japan Society for the Promotion of Science  Grants-in-Aid for Scientific Research  Grant-in-Aid for Scientific Research (A)

    Matunaga Saburo

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    Grant amount:\44070000 ( Direct Cost: \33900000 、 Indirect Cost:\10170000 )

    A variable shape attitude control satellite was developed to EM level and will be launched in orbit in 2021. We showed influences of variable shape change on structure optimization, magnetic torque and RW combination attitude control, solar power generation, heat control and communication interference, and found orbit solutions to transition between EML and to Mars for variable shape solar sail, which showed usefulness of simultaneous orbit and attitude control. Deployable booms with corrugated closed section and planar self-deployable structures with corrugated panels were proposed and the deployment properties were clarified. 3-axis attitude determination with 1-degree precision is achieved by AI image identification in orbit with visible light camera of 3 gram. An occulter mission with deployable truss structure, and an ultraviolet astronomy observation/land-sea remote sensing mission were proposed and their conceptual design was conducted. The latter is planned to launch in 2022.

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  • Construction of design and verification methodology for large deployable space structures through development of CubeSat demonstrator

    Grant number:17H03477  2017.4 - 2020.3

    Japan Society for the Promotion of Science  Grants-in-Aid for Scientific Research  Grant-in-Aid for Scientific Research (B)

    Sakamoto Hiraku

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    Grant amount:\16900000 ( Direct Cost: \13000000 、 Indirect Cost:\3900000 )

    Space deployable membrane structures are expected to realize innovative space applications; however, their designs and fabrications are difficult to be verified on the ground. As a result, structural designs tend to be conservative and massive. To this end, this study develops a new lightweight membrane structure to be tested on orbit. A 3U CubeSat (nano-satellite) is developed and launched to space. Through the development, design/verification strategies for space membrane structures are constructed.
    Specifically, the three insights are obtained. First, the new designs and ground test methods were practically developed. Second, the experimental results were used to derive design methodology for larger membrane space structures. Third, designs for solar power generation satellites and membrane array antennas were proposed though the knowledge obtained through the CubeSat development.

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  • Dynamics analysis of gripper for space debris capture using convex spring

    Grant number:16K21033  2016.4 - 2019.3

    Japan Society for the Promotion of Science  Grants-in-Aid for Scientific Research  Grant-in-Aid for Young Scientists (B)

    Nakanishi Hiroki, ODA Mitsushige, OZAWA Takaya, MASUDA Yuto

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    Grant amount:\4290000 ( Direct Cost: \3300000 、 Indirect Cost:\990000 )

    In this research, for capturing space debris by a robot, the researcher investigated a gripper mechanism that can automatically detects the initial contact with debris and capture it without using electric actuators and sensors. The necessary mechanics, mechanism and design method are clarified. In particular, focusing on the convex spring used in wristbands, the dynamics characteristics of the spring were formulated. Then the method of freely designing the motion of the spring for gripper was clarified.

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  • Robot Control for Lunar, Planetary and Asteroid Exploration with Understanding of Geometry and Physical Characteristics of the Environment

    Grant number:21246122  2009 - 2012

    Japan Society for the Promotion of Science  Grants-in-Aid for Scientific Research  Grant-in-Aid for Scientific Research (A)

    YOSHIDA Kazuya, NAGATANI Keiji, KENJI Nagaoka

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    Grant amount:\43290000 ( Direct Cost: \33300000 、 Indirect Cost:\9990000 )

    Robotics technologies for lunar, planetary and asteroid exploration were investigated with understanding of geometry and physical characteristics of the environment. Traction model of wheels and tracks for traversing over loose-soil terrain was studied. Rover localization with integrating different types of sensors was also investigated and tested in outdoor field.

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  • Dynamics and Control for Satellite Capture Robot based on the Impedance Theory

    Grant number:20760155  2008 - 2010

    Japan Society for the Promotion of Science  Grants-in-Aid for Scientific Research  Grant-in-Aid for Young Scientists (B)

    NAKANISHI Hiroki, ABIKO Satoko, ROBERTO Lampariello

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    Grant amount:\4160000 ( Direct Cost: \3200000 、 Indirect Cost:\960000 )

    Contact is a critical phase in satellite capture because it involves the risk that the contact will push the target and robot away from each other. In this study, effective contact control methods based on the contact dynamics analyses were developed to prevent the target from being pushed and to maintain contact until the capture completed.

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  • マイクロサテライトが拓くスプライト及び雷放電逃走電子の科学

    Grant number:17204042  2005 - 2008

    日本学術振興会  科学研究費助成事業  基盤研究(A)

    高橋 幸弘, 坂井野 健, 吉田 和哉, 中西 洋樹, 高島 健, 田口 真

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    Grant amount:\41340000 ( Direct Cost: \31800000 、 Indirect Cost:\9540000 )

    雲地上間の雷放電に伴う上空放電のひとつであるスプライトと呼ばれる現象は、1990年の最初の報告以来、精力的な研究が、観測、理論の両面から続けられている。しかし、これまでの地上観測ではスプライトを真下から見ることができないため、その水平構造については三角測量観測による数例しか調べられていない。一方、高エネルギー電子によって放射される地球ガンマ線が、雷雲活動に同期して人工衛星で観測されている。本研究では、CMOS及びCCDイメージャーとガンマ線センサーを搭載した、スプライト・地球ガンマ線観測専用のマイクロサテライトを開発、打ち上げ、それらの解明を目指す。検討の結果、本計画では、衛星を50cm立方、40kg級に変更することとした。2006年度は、以下の機器開発、校正、環境試験を実施するとともに、TLEおよびTGF観測戦略を作成するために、それらの地上および衛星観測データの解析を行い、海外研究者と議論する機会をもった。
    1.搭載機器の製作・環境試験・校正
    2005年度に引き続き、CMOS及びCCDを用いた超小型・軽量のイメージセンサーの製作・環境試験、及び校正を行い、ソフトウェアも含め、フライト品の製作に目途をつけた。また、米国カリフォルニア大学サンタクルズ校のスミス博士の助言に基づき、ガンマ線センサーの最終的な仕様を確定した。
    2.衛星BUSの設計・開発および環境試験
    BUSの最終設計を完了し、各パーツのフライト部品の仕様決定・購入を行った。必要部品を購入して構造モデルを製作し、振動試験を実施した。
    3.海外研究者との打合せおよび成果発表
    10月にフランスを訪れ、同様の衛星計画(打上は本計画の3年後)を持つフランスチームと会合を持ち、観測戦略についての意見交換を行った。また、12月のAGU(米国)学会に参加し、研究経過の発表(招待講演)と、海外研究者(スミス博士及びイナン教授他)と議論を行った。

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  • Study on planetary atmospheres and plasmas by a balloon-borne telescope

    Grant number:17540426  2005 - 2006

    Japan Society for the Promotion of Science  Grants-in-Aid for Scientific Research  Grant-in-Aid for Scientific Research (C)

    TAGUCHI Makoto, YOSHIDA Kazuya, NAKANISHI Hiroki, TAKAHASHI Yukihiro, SAKANOI Takeshi

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    Grant amount:\3300000 ( Direct Cost: \3300000 )

    This research has promoted the ongoing development of a balloon-borne telescope system for remote sensing of planetary atmospheres and plasmas. In this system, a Schmidt-Cassegrain telescope with a 300-mm clear aperture is mounted on a gondola whose attitude is controlled by control moment gyros, an active decoupling motor, and a Sun sensor. The gondola can float in the stratosphere for periods in excess of 1 week. A pointing stability of 10 arcsec/sec will be achieved via the cooperative operation of the following three-stage pointing devices: a gondola-attitude control system, two-axis telescope gimbals for coarse guiding, and a tip/tilt mirror mount for guiding error correction. The tip/tilt mirror is controlled by a real-time correction signal from a position-sensitive photomultiplier tube. Video images of an object in near-infrared and ultraviolet are obtained by analog and digital CCD video cameras, respectively. Power is supplied by solar cell panels and Ni-MH batteries, of which low temperature characteristics have been tested. A pressurized cell contains two PCs, DC/DC converters, pre-amplifiers and a high-voltage power supply for a tip/tilt mirror mount. System performance under a low-temperature and low-pressure condition has been confirmed by a thermal vacuum test. ESRANGE in Kiruna, Sweden was investigated for a candidate launch site of a future experiment in the Arctic. The first target for the system is Venus. Wind vectors in the Venusian upper atmosphere will be derived from the tracking of cloud patterns observed in the ultraviolet and near-infrared regions. An experiment designed to test the system performance is scheduled to take place in Japan during June 2007, and a long-duration flight in the Arctic is scheduled for 2008.

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  • Space Robotics for Capture and Service to Non-Cooperative Satellites

    Grant number:14350125  2002 - 2005

    Japan Society for the Promotion of Science  Grants-in-Aid for Scientific Research  Grant-in-Aid for Scientific Research (B)

    YOSHIDA Kazuya, NAKANISHI Hiroki

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    Grant amount:\14000000 ( Direct Cost: \14000000 )

    We have studied control technologies and basic system design of space robots for orbital servicing, which are able to capture and repair malfunctioning non-cooperative satellites using their manipulator arm(s). In this project, the following results have been obtained :
    1. Modeling of Contact Dynamics
    Modeling and analysis of the contact dynamics for free-flying objects have been carried out both theoretically and experimentally. A method for identifying the mechanical impedance of the target object has been established. We developed a micro-gravity experimental setup using a spacecraft model that floats slightly on a horizontal granite table by pressurized air. The validity of our model and theory have been confirmed throughout the experiments
    2. Manipulator Control to Prevent Pushing the Target Away in the Capture
    When a free-flying space robot captures a target satellite, the target object can be easily bounced away by the contact force. Impedance control is effective to reduce the contact force. We have investigated the dynamic conditions to maintain the contact between the free-flying manipulator arm and the target based on the "Impedance Matching" theory. It is proved throughout experiments that the equivalent mass of the end tip of the arm coming from the impedance control is a reasonable criterion for preventing pushing the target away.
    3. Advanced Control for Space Redundant Macro-Micro Manipulators
    The macro-micro manipulator is a promising system for orbital servicing, which consists of a long (macro) arm and a small fine (micro) arm. The macro arm provides a long-reach capability and the micro arm performs the dexterous manipulation. However, the macro part can generate vibrations due to structural flexibility. The motion of the small arm induces vibrations onto the macro part, hence, resulting in the reduction of its positioning accuracy. In this study, a control method for an accurate and quick manipulation preventing such vibrations has been established.

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