研究者業績
基本情報
- 所属
- 国立研究開発法人宇宙航空研究開発機構 宇宙科学研究所 名誉教授
- 学位
- 工学博士(東京大学)
- researchmap会員ID
- 1000144488
研究キーワード
2研究分野
1学歴
4-
- 1974年
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- 1974年
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- 1969年
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- 1969年
委員歴
2-
2008年6月 - 2010年6月
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2005年4月 - 2006年3月
論文
91-
Smart Materials and Structures 2024年8月1日 査読有り筆頭著者責任著者
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Smart Materials and Structures 30(6) 065014-065014 2021年6月1日 査読有り筆頭著者責任著者Abstract 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 2018年10月 査読有り
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Mechanical Systems and Signal Processing 117 2018年8月 査読有り
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JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES 28(7) 888-906 2017年4月 査読有り筆頭著者責任著者
MISC
44講演・口頭発表等
418-
20th International Symposium on Space Technology and Science (ISTS) 1996年5月
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37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference 1996年4月 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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37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference 1996年 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年 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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46th International Astronautical Congress 1995年10月
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46th International Astronautical Congress 1995年10月
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AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 1995年4月
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Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 1995年1月1日Vibration 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 1994年10月
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19th International Symposium on Space Technology and Science 1994年5月
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19th International Symposium on Space Technology and Science 1994年5月
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19th International Symposium on Space Technology and Science 1994年5月
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19th International Symposium on Space Technology and Science 1994年5月
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AIAA/ASME Adaptive Structures Forum 1994年4月
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AIAA/ASME Adaptive Structures Forum 1994年4月
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AIAA Dynamic Specialist Conference 1994年4月
所属学協会
4Works(作品等)
2共同研究・競争的資金等の研究課題
12-
日本学術振興会 科学研究費助成事業 基盤研究(C) 2020年4月 - 2023年3月
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日本学術振興会 科研費 2014年4月 - 2017年3月
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日本学術振興会 科研費 2008年4月 - 2010年3月
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日本学術振興会 科研費 2007年 - 2008年
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日本学術振興会 科研費 2006年 - 2007年