Curriculum Vitaes
Profile Information
- Affiliation
- Professor, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
- Degree
- Ph.D. in Engineering(Mar, 1991, The University of Tokyo)
- J-GLOBAL ID
- 201801002275500853
- researchmap Member ID
- B000340311
Papers
55-
SMART MATERIALS AND STRUCTURES, 33(8), Aug 1, 2024
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Smart Materials and Structures, 30(6) 065014-065014, Jun 1, 2021Abstract 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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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 16(2) 181-187, 2018<p>An Extensible Optical Bench (EOB) for a X-ray satellite (ASTRO-H) had a length of 6.4m in extended configuration. Although the same type of extensible mast was used in Space Radio Telescope (Halca) in 1997, the tip mass was quite different in the case of ASTRO-H. Due to the tip mass of 150 kg, the natural frequency of EOB was less than 1Hz in the extended configuration. ASTRO-H was launched on Feb. 17, 2016, and the EOB was extended on Feb. 28, 2016, successfully. However, because the vibration of EOB occurred during the extension, the extension operation was carried out over four passes intermittently. When the amplitude of induced vibration excessed the predefined threshold, we stopped the extension, then stayed until the vibration was damped. In this paper, the induced vibration during extension and its mechanism are reported. Through simulations, it is confirmed that one of the major causes of the vibration is a periodic change of gap between mast and canister at the root of EOB.</p>
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Journal of Astronomical Telescopes, Instruments, and Systems, 4(1), Jan 1, 2018 Peer-reviewed
Misc.
93-
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 53(613) 43-50, Feb 5, 2005Passive damping augmentation is one of attractive methods for vibration suppression to various kinds of structures because it is definitely stable and generally simple. The system using thin film with viscous adhesive indicated a remarkable effect to the vibration suppression in the practical application to a satellite. To investigate its damping characteristic, several kinds of experiments have been performed. The results show that the non-linear behavior cause of non-Newtonian flow between shear load and shear deformation velocity in the viscous lamina of the thin film contributes to the damping capability. A mathematical model which consists of spring elements as film and friction elements as viscous lamina has been proposed from experiments. The simulational results with this present model are in good agreement with experimental ones.
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The Proceedings of the Symposium on the Motion and Vibration Control, 2005 271-276, 2005A novel self-sensing method using piezoelectric actuators for semi-active vibration suppression is proposed. By using extended system equations, this self-sensing method can be implemented with a Kalman filter instead of the conventional bridge circuit technique. This method is so advanced that it can be applied to multiple-degree-of-freedom (MDOF) structures with multiple piezoelectric actuators. A numerical simulation demonstrated that the self-sensing method works well on a truss structure and has significant robustness against parameter variations. Experimental results also confirmed that the self-sensing method suppresses not only single-mode vibrations but also complicated multiple-mode vibrations.
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The Proceedings of the Dynamics & Design Conference, 2005 _713-1_-_713-6_, 2005A novel method of hybrid vibration suppression using piezoelectric materials is proposed. It combines bangbang active control and energy-recycling semi-active control. The hybrid method saves actively supplied energy and is thus a low energy-consumption vibration control. Its effectiveness in suppressing vibrations was proven in numerical simulations and experiments using a 10-bay truss structure. Moreover, an innovative method to prevent undesired control chattering is proposed to further save energy supplied from the external source.
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構造強度に関する講演会講演集, 44th 134-136, Jul 24, 2002
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構造強度に関する講演会講演集, 43rd 181-184, Aug 1, 2001
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Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2 986-991, Jan 1, 2001
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構造強度に関する講演会講演集, 41st 241-244, Jul 14, 1999
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鉄鋼及び各種金属材料の種々の環境下における変形・破壊 平成11年, 47-53, 1999
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宇宙科学技術連合講演会講演集, 42nd 1093-1098, Oct, 1998
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宇宙科学研究所報告, 100 1-34, Mar, 1998In this paper, the trajectory dispersion of the Viper rocket caused by the elastic vibration of the vehicle and rocket launcher is investigated. In order to estimate the trajectory dispersion, a three dimensional numerical simulation of the launch was carried out considering the elastical effect of the vehicle and rocket launcher. The accuracy of the numerical simulation was validated first by the comparison with the vibration data measured on actual launch, and after that the trajectory dispersion was estimated by the simulation. As the result, it is confirmed that the trajectory dispersion caused by th elastic vibration is no matter on actual launch mission.
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Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 3 1813-1821, Jan 1, 1998
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Development of Filament Wound Second Stage Motor Casing for M-V Satellite Launcher. (Second Report).構造強度に関する講演会講演集, 40th 241-244, 1998
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構造強度に関する講演会講演集, 39th 241-244, 1997
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構造強度に関する講演会講演集, 39th 233-236, 1997
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構造強度に関する講演会講演集, 39th 337-340, 1997
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37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference, 1569-1577, Jan 1, 1996
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37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference, 1016-1023, Jan 1, 1996
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構造強度に関する講演会講演集, 38th 225-228, 1996
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Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 1 200-206, Jan 1, 1995
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Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2 1060-1067, Jan 1, 1995
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Collection of Technical Papers - AIAA/ASME Structures, Structural Dynamics and Materials Conference, 2095-2100, Jan 1, 1993
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構造強度に関する講演会講演集, 35th 194-197, 1993
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構造強度に関する講演会講演集, 35th 62-65, 1993
Presentations
13-
33rd International Symposium on Space Technology and Science, Mar 1, 2022
Teaching Experience
2-
Oct, 2024 - Jan, 2025飛翔体構造工学概論 (東京大学大学院工学系研究科航空宇宙工学専攻)
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Sep, 2024 - Sep, 2024衛星システム設計学特論 (公立大学法人大阪)
Research Projects
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科学研究費助成事業, 日本学術振興会, Apr, 2023 - Mar, 2027
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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 Grant-in-Aid for Scientific Research (C), Japan Society for the Promotion of Science, Apr, 2014 - Mar, 2018
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Grants-in-Aid for Scientific Research Grant-in-Aid for Scientific Research (B), Japan Society for the Promotion of Science, 2008 - 2010
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Grants-in-Aid for Scientific Research Grant-in-Aid for Scientific Research (B), Japan Society for the Promotion of Science, 2007 - 2008