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-
20th International Symposium on Space Technology and Science (ISTS), May, 1996
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日本機械学会通常総会講演会講演論文集, Apr, 1996
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日本機械学会通常総会講演会講演論文集, Apr, 1996
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37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference, Apr, 1996, American Institute of Aeronautics and Astronautics Inc, AIAATo semiactively suppress the vibration of space truss structures, a variable damper using Electro- Rheological (ER) fluid is designed and fabricated. The characteristics of the damper are measured, and a simple mathematical model of the damper is proposed. Based on this mathematical model, several semiactive control laws are proposed for vibration suppression of multiple degree- of-freedom (MDOF) structures with multiple dampers. To investigate the performances of the scheme, numerical simulations of semiactive vibration suppression of a ten-bay truss beam with ER fluid dampers are performed. Simulation results indicate that the most of the proposed semiactive control laws result in much higher performances than that of the optimally tuned passive system. A semiactive vibration suppression experiment of the ten-bay truss beam with the ER fluid damper is also performed. The experiment results also demonstrate the effectiveness of the scheme for the actual MDOF structure.
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構造強度に関する講演会講演集, 1996
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37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference, 1996, American Institute of Aeronautics and Astronautics Inc, AIAAPassive damping augmentation is one of the effective method for vibration suppression because it is definitely stable and generally simple. Thin film with viscous lamina showed a remarkable effect for passive vibration suppression in the practical application to a satellite. To investigate its damping capability, several kinds of experiments have been performed. The results show that the non-linear relation between shear load and shear deformation velocity in the viscous lamina of the thin film contributes to the damping capability. Simple mathematical model is made to represent the behavior of the film.
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37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference, 1996, American Institute of Aeronautics and Astronautics Inc, AIAAThis paper discusses that optimal design of passive damping is effective for performance improvement on the simultaneous structure/controller optimization problem for flexible space structures. In this study, structural passive damping is assumed to viscous passive damping, and the simultaneous optimization of active controller gains, structural stiffness, and viscous passive damping elements is performed. In order to control lower modes, the Linear Quadratic Gaussian (LQG) controller is adopted. Besides, in order to damp residual modes actively, the Direct Velocity Feedback (DVFB) controller, whose function is similar to viscous passive damping elements, is adopted. In this paper, effects of the quality of the DVFB controller are also investigated. As one of typical numerical examples, a controlled simply supported sandwich beam structure that has a viscoelastic layer is investigated. Through the observation of the numerical results, it is confirmed that the optimal design of the viscous damping elements is useful for the performance improvement on the simultaneous optimization of the structure and the control system.
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宇宙科学技術連合講演会講演集, Oct, 1995
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46th International Astronautical Congress, Oct, 1995
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46th International Astronautical Congress, Oct, 1995
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AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Apr, 1995
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Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Jan 1, 1995Vibration environment at lift-off of satellite launchers is one of critical conditions for electrical devices or systems on board. Countermeasure against the vibration is sometimes required, however, it is difficult to find an effective and practical one under the restrictions of weight increase and space. In this paper, a polyimid tape with viscous lamina is noted on the application to the passive vibration suppression, since it has shown a remarkable effect for vibration suppression in the practical application to a satellite. In order to investigate its damping mechanism, several kinds of experiments have been performed and their results are reported in this paper.
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45th International Astronautical Congress, Oct, 1994
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19th International Symposium on Space Technology and Science, May, 1994
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19th International Symposium on Space Technology and Science, May, 1994
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19th International Symposium on Space Technology and Science, May, 1994
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19th International Symposium on Space Technology and Science, May, 1994
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AIAA/ASME Adaptive Structures Forum, Apr, 1994
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AIAA/ASME Adaptive Structures Forum, Apr, 1994
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AIAA Dynamic Specialist Conference, Apr, 1994
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