Curriculum Vitaes
Profile Information
- Affiliation
- Professor, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
- Degree
- Ph.D.(The University of Tokyo)
- researchmap Member ID
- 1000144488
Research Interests
2Education
4Committee Memberships
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Jun, 2008 - Jun, 2010
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Apr, 2005 - Mar, 2006
Papers
91-
Smart Materials and Structures, Aug 1, 2024 Peer-reviewedLead authorCorresponding author
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Smart Materials and Structures, 30(6) 065014-065014, Jun 1, 2021 Peer-reviewedLead authorCorresponding authorAbstract We propose and demonstrate a novel method to enhance vibration harvesting based on surge-induced synchronized switch harvesting on inductor (S3HI). S3HI allows harvesting of a large amount of energy even from low-amplitude vibrations by inducing a surge voltage during the voltage inversion of a synchronized switch harvesting on inductor (SSHI). The surge voltage and the voltage amplification from the conventional voltage inversion improve energy harvesting. S3HI modifies SSHI by both rewiring the circuit without adding components and using a novel switching pattern for voltage inversion, thus maintaining the simplicity of SSHI. We propose a novel switching strategy and circuit topology and analyze six methods that constitute the S3HI family, which includes traditional S3HI and high-frequency S3HI. We demonstrate that the six methods suitably harvest energy even from low-amplitude vibrations. Nevertheless, the harvestable energy per vibration cycle depends on the switching pattern and storage-capacitor voltage. The use of the proposed switching strategy, which allows energy harvesting before energy-dissipative voltage inversion, substantially increases the harvestable energy per vibration cycle. In the typical case considered in this study, the said increase is on the order of 11%–31% and 15%–450% compared to the traditional and existing high-frequency S3HI methods, respectively, depending on the storage-capacitor voltage. Additionally, the proposed circuit can be used as a traditional circuit. It could be considered a promising alternative to S3HI methods owing to its potential auto-reboot capability, which is not found in traditional S3HI circuit.
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Sensors and Actuators A: Physical, 281 55-66, Oct, 2018 Peer-reviewed
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Mechanical Systems and Signal Processing, 117, Aug, 2018 Peer-reviewed
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JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 28(7) 888-906, Apr, 2017 Peer-reviewedLead authorCorresponding author
Misc.
44Presentations
413-
Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2006, American Institute of Aeronautics and Astronautics Inc.
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Dyn Des Conf (CD-ROM), 2006
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SMART STRUCTURES AND MATERIALS 2006: DAMPING AND ISOLATION, 2006
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Performance investigation of energy-efficient active vibration control using energy-recycling methodSIXTEENTH INTERNATIONAL CONFERENCE ON ADAPTIVE STRUCTURES AND TECHNOLOGIES, Oct, 2005
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日本機械学会運動と振動の制御シンポジウム講演論文集, Aug 22, 2005
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International Astronautical Federation - 56th International Astronautical Congress 2005, 2005
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Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2005, American Institute of Aeronautics and Astronautics Inc.
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構造強度に関する講演会講演集, 2005
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2nd International Symposium on Innovative Aerial/Space Flyer Systems, 2005
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自動制御連合講演会講演論文集, Nov 25, 2004
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24th International Symposium on Space Technology and Science, Jun, 2004
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Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2004, American Institute of Aeronautics and Astronautics Inc.
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International Astronautical Congress, Sep, 2003
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構造強度に関する講演会講演集, Jul 30, 2003
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Dynamics of Machines, Feb, 2003
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4th MATHMOD (Mathematical Modeling) Conference, Feb, 2003
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54th International Astronautical Congress of the International Astronautical Federation (IAF), the International Academy of Astronautics and the International Institute of Space Law, 2003
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44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2003
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宇宙構造・材料シンポジウム 平成14年度 第18回, 2003
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International Astronautical Congress, Oct, 2002
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構造強度に関する講演会講演集, Jul 24, 2002
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構造強度に関する講演会講演集, Jul 24, 2002
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構造強度に関する講演会講演集, Jul 24, 2002
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International Astronautical Congress, Jun, 2002
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International Symposium on Space Technology and Science (ISTS), May, 2002
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International Symposium on Space Technology and Science (ISTS), May, 2002
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43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Apr, 2002
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Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Jan 1, 2002Carpenter tape hinge made of TiNi alloy (a shape memory alloy) was designed, fabricated, and investigated. A carpenter tape hinge is one mechanism that has the advantages of high-reliability of deployment, lightweight, and low-cost. However, a traditional carpenter tape hinge has the disadvantage that a large shock arises when it springs into the deployed position. Our aim is to use TiNi alloy for a carpenter tape hinge instead of conventional spring materials. When the hinge is gradually heated, it deploys slowly under the resulting shape recovery force. And it deploys without a large latch shock. First, we determinated the configuration of the hinge that maximizes the stiffness. Next, we fabricated various configurations of hinges. We demonstrated deployment of the fabricated hinge and evaluate its characteristics through experiments and FEM analysis using ABAQUS. Moreover, we compared its characteristics with those of a conventional carpenter tape hinge and a plate-like hinge made of TiNi alloy through experiments and equations.
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19th AIAA Applied Aerodynamics Conference, Dec, 2001This paper shows the effectiveness of a semiactive vibration isolator filled with liquid-crystal type electro-rheological (ER) fluid for disturbances generated by momentum-wheels. The principal characteristics of an ER isolator was measured in dynamic tests, and a mathematical model of the isolator was proposed. Two control laws for semiactive approach were proposed. Numerical simulation results indicated that the proposed semiactive control produced much better isolation performance than a passive system. © 2001 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
Professional Memberships
4Works
2Research Projects
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科学研究費助成事業 基盤研究(C), 日本学術振興会, Apr, 2020 - Mar, 2023
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2014 - Mar, 2017
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2008 - Mar, 2010
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, 2007 - 2008
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, 2006 - 2007