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
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Smart Materials Research 2013(Article No. 736487) 2013年1月 査読有り
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Journal of System Design and Dynamics 6(5) 583-596 2012年12月 査読有りWe report herein our innovative self-powered digital autonomous system for vibration control using a digital micro-processor. Our unit is a completely self-powered control system that does not require an external power-supply. Because this digital, self-directive, self-powered system is programmable and can be used to implement versatile control schemes. Our digital-autonomous controller is much more advanced and progressive than conventional analog-autonomous controllers. Moreover, our digital system can be implemented in multiple-input multiple-output systems (MIMO) to suppress even complicated structural vibrations. This is quite useful for energy-saving or energy-shortage systems, such as large space structures, artificial satellites, and isolated lunar bases, which are vulnerable to long night-time exposures without solar power. Experiments demonstrate that displacement is reduced to as much as 35%. Energy dissipation in experiments is measured using various methodologies. Finally, we investigate the influence of the voltage offset of the AD port of the microprocessor on both estimation error and suppression performance.
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AIAA JOURNAL 50(9) 2004-2011 2012年9月 査読有り
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JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME 134(2) 2012年4月 査読有り最終著者
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Journal of System Design and Dynamics, Vol. 6, No. 5, (2012), pp. 583-596. 6(5) 583-596 2012年 査読有り
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Trans. JSASS Aerospace Tech. Japan 10(28) Pc_13-Pc_18 2012年 査読有りWe propose a digital autonomous power scavenger with a microprocessor. The proposed system is a completely self-powered one that does not require any external power supply at all, and can thus be used portably at any site. Nevertheless, the digital approach enables the power scavenger to be programmable and thus, it affords some versatility with regard to control schemes. The proposed digitalautonomous system is much more advanced and progressive than clumsy analog-autonomous ones. It can be implemented in multiple-input multiple-output systems to scavenge electrical power from even complicated structural vibrations. We determined the value of the storage capacitance that gives the best balance between scavenging power and consumed power.
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Smart Materials Research 2012 2012年 査読有り
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Smart Materials Research 2011 1-8 2011年5月 査読有りWe conduct comprehensive investigation of a semiactive vibration suppression method using piezoelectric transducers attached to structures. In our system, piezoelectric transducers are connected to an electric circuit composed of the diodes, an inductance, and a selective switch. Our method (SSDI) makes better use of counterelectromotive force to suppress the vibration, instead of simple dissipation of vibration energy. We use an actual artificial satellite to verify their high performance compared to conventional semi-active methods. As a consequence, we demonstrate that our semi-active switching method can suppress the vibration of the real artificial satellite to as much as 50% amplitude reduction. In our experiment, we reveal that the suppression performance depends on how multiple piezoelectric transducers are connected, namely, their series or parallel connection. We draw two major conclusions from theoretical analysis and experiment, for constructing effective semi-active controller using piezoelectric transducers. This paper clearly proves that the performance of the method is the connection (series or parallel) of multiple piezoelectric transducers and the their resistances dependent on frequency.
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日本航空宇宙学会論文集 59(686) 55-60 2011年 査読有り最終著者Passive damping augmentation is one of attractive methods for vibration suppression to various kinds of structures because it is definitely stable and generally simple. Using viscous adhesive indicated a remarkable effect to the vibration suppression in the practical application to a satellite. In this paper, mathematical model of thin viscous adhesive layer using non-linear elements has been proposed. In this model, the characteristics of elements are correlated with non-linear internal phenomena of polymer. The simulation results using this proposal model are good agreement with experimental ones.
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SMART MATERIALS & STRUCTURES 19(8) 1-10 2010年8月 査読有り
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AIAA JOURNAL 47(7) 1601-1607 2009年7月 査読有り最終著者
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 52(175) 36-46 2009年5月 査読有り
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EMBODING INTELLIGENCE IN STRUCTURES AND INTEGRATED SYSTEMS 56 345-354 2009年 査読有り筆頭著者責任著者
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JOURNAL OF VIBRATION AND CONTROL 14(3) 417-436 2008年3月 査読有り筆頭著者責任著者
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日本航空宇宙学会論文集 56(651) 169-178 (J-STAGE)-178 2008年 査読有りAdhesive bonding structure around a metalic mouthpiece of a cryogenic composite tank was analyzed based on fracture mechanics. Energy release rate was analytically formulated considering difference in strain energies in tension and bending between before and after the crack growth based on a simplified mathematical model. The analytical results were compared with the calculated results by finite element method for five example tanks; they revealed fairly good match. This analysis gives a guideline of the initial optimal design of a cryogenic composite tank based on fracture mechanics.
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SMART MATERIALS & STRUCTURES 16(2) 455-461 2007年4月 査読有り
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 49(166) 203-210 2007年2月 査読有り
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AIAA JOURNAL 45(2) 497-504 2007年2月 査読有り
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JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME 129(1) 84-93 2007年2月 査読有り
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AIAA JOURNAL 45(1) 306-308 2007年1月 査読有り
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KSAS, International Journal of Aeronautical and Space Sciences 7(1) 70-85 2006年11月 査読有り
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SMART MATERIALS & STRUCTURES 15(5) 1493-1498 2006年10月 査読有り
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AIAA JOURNAL 44(7) 1445-1453 2006年7月 査読有り
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ACTA ASTRONAUTICA 58(10) 506-514 2006年5月 査読有り
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SMART MATERIALS & STRUCTURES 15(2) 342-350 2006年4月 査読有り
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AIAA JOURNAL 44(2) 411-413 2006年2月 査読有り
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日本航空宇宙学会論文集 53(619) 343-350 2005年8月5日 査読有りA novel control law based on the sliding-mode control is proposed for energy-recycling vibration suppression of a structure with piezoelectric transducers. The performance of vibration suppression with the proposed control law is investigated and compared with that of the previously proposed control law based on LQR control theory. Numerical simulations of vibration suppression with a 10-bay truss structure show that the proposed control law is effective in suppressing vibration. Through experiments of vibration suppression with a truss structure, the proposed control law is shown to suppress single-mode and multiple-mode vibrations of actual structure. Although the proposed control law is derived in a different way from the previous control law, the two methods are found to have similar coefficients of modal velocities in the control index.
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AIAA JOURNAL 43(8) 1706-1715 2005年8月 査読有り
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日本航空宇宙学会論文集 53(613) 43-50 2005年2月5日 査読有りPassive 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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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 47(157) 167-174 2004年11月 査読有り
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JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME 126(2) 272-277 2004年4月 査読有り
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International Astronautical Federation - 55th International Astronautical Congress 2004 3 2018-2026 2004年
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AIAA JOURNAL 41(4) 711-719 2003年4月 査読有り筆頭著者責任著者
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 45(150) 255-260 2003年2月 査読有り最終著者
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 45(147) 53-60 2002年5月 査読有り最終著者
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Simultaneous optimization of piezoelectric actuator placement and feedback for vibration suppressionACTA ASTRONAUTICA 50(6) 335-341 2002年3月 査読有り
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SMART MATERIALS & STRUCTURES 11(1) 156-162 2002年2月 査読有り
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Simultaneous optimization of intelligent structure and feedback gains for flexible structure controlAUTOMATIC CONTROL IN AEROSPACE 2001 471-476 2002年 査読有り
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JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME 122(4) 412-419 2000年10月 査読有り
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AIAA JOURNAL 38(9) 1736-1741 2000年9月 査読有り筆頭著者責任著者
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COMPUTERS & STRUCTURES 70(1) 119-128 1999年1月 査読有り
MISC
44講演・口頭発表等
413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