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
120-
Smart Materials and Structures 2024年8月1日 査読有り
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Smart Materials and Structures 30(6) 065014-065014 2021年6月1日 査読有り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This article describes the optimal configuration and combination of piezoelectric transducers and inductors for the synchronized-switch-damping-on-an-inductor technique. The technique suppresses structural vibrations by inverting the polarity of the electric voltage in a piezoelectric transducer using a switched inductive shunt circuit at each displacement extremum. The energy dissipation rate of synchronized switch damping on an inductor depends on the impedances of the transducer and the inductor in the circuit, especially the resistive component, in this inversion. For this study, mathematical models of the equivalent resistances of transducers and inductors for this inversion phenomenon were formulated based on experiments with various transducers and inductors. Using these models, the optimal ratio of the thickness-area of patch-type piezoelectric transducers and that of the length-cross-sectional area of the lead of the inductors were analytically obtained. The optimization of series-parallel connections of multiple transducers and inductors was also shown to be equivalent to this one. The optimal mass budget allocation for the transducers and inductors was also formulated. Two examples of optimization, involving an increase in energy dissipation rates by a factor of 4, were presented. The examples showed that the time taken to suppress free vibrations in a clamped beam was reduced to half through the optimization.
MISC
53-
機械力学・計測制御講演論文集 2011 18-18 2011年9月4日
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Dynamics & Design Conference 2006 "621-1"-"621-6" 2006年8月6日This paper presents a self-sensing method for semi-active vibration suppression that measures only the value of piezoelectric voltage. The method separates electrical status into two cases concerning electrical current, and characterize each of these to establish a self-sensing system. Experiments revealed that the self-sensing system suppressed vibrations by combining the state-switching control or the synchronized-switching control. We confirmed that the self-sensing method is robust against model errors through the vibration suppression experiment subject to model errors caused by intentional frequency shift.
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日本航空宇宙学会誌 = Journal of the Japan Society for Aeronautical and Space Sciences 54(628) 126-126 2006年5月5日
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「運動と振動の制御」シンポジウム講演論文集 2005(9) 271-276 2005年8月22日A 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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Dynamics & Design Conference 2005 "713-1"-"713-6" 2005年8月22日A 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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43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2002, Denver, CO. 2002年
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宇宙科学研究所報告 100(100) 36P-34 1998年3月本報告では, 発射時に生じるロケット本体及びランチャーの弾性振動に起因する Viper ロケットの軌道分散について報告する。軌道分散の推定のために, ロケット及びランチャーの弾性を考慮した発射の三次元数値シミュレーションを行なった。実際の発射時に計測された振動データとの比較によりシミュレーションの精度を確認した後に, シミュレーションを用いて軌道分散の推定を行なった。その結果, 弾性振動に起因する軌道分散は実際の打ち上げミッションにおいて問題にならない値であることが確認された。
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日本航空宇宙学会誌 = Journal of the Japan Society for Aeronautical and Space Sciences 45(517) 77-78 1997年2月
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日本航空宇宙学会誌 = Journal of the Japan Society for Aeronautical and Space Sciences 44(507) 212-213 1996年4月5日
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宇宙科学研究所報告 特集 16(16) 161-168 1986年10月M-3S型ロケットは, M-3H型ロケットの第1段に姿勢制御装置を搭載したものである。第1段すなわち大気中飛翔時から姿勢制御を行うこととしたことに伴い, 機体に作用する曲げ荷重は制御方法に大きく左右されることとなったが, 原則として過大な曲げ荷重を発生させない制御方法を採用するか, あるいは制御力の範囲を一定限以下とすることを前提として, 接手等の主な機体部分の設計変更は行なわないこととした。M-3S型ロケットの構造のM-3H型との主な相違点は, 次のとおりである。(1)尾翼筒の内外径の増大及び整備点検用開口部の設定(2)尾翼先端部へのSMRCの搭載及び尾翼全長短縮(3)衛星接手の新規設計(4)M-3Aモータケースの薄肉化(2号機より)(5)M-13ノズルまわりのTVC搭載部の設計また, 第1段制御系設計の資料を得る為に, 機体動特性の予測が従来になく精力的に行なわれたことも, 本機体開発の特徴であった。
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宇宙科学研究所報告 40(40) 22P-21 1986年10月This report presents the outline of the rocket structural testing facility constructed in Sagamihara campus of ISAS in 1984. The facility is composed of a) a 12m long, 8m tall, 6m wide testing stand, b) a 2-channel 70 MPa hydropressure loading device with a control unit, c) a 600-channel strain/displacement measureling system, and d) a data acquisition, processing and display system. Although the planning of the facility was motivated by the structural testings required in the process of development of Mu-3SII launch vehicle, it was designed so as to carry out the various structural testing of various kinds of structures as flexibly and efficiently as possible.
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宇宙科学研究所報告 特集 6(6) 155-166 1983年3月A development of a heat isolation system of tanks for LOX/LH2 rockets and its evaluation test are presented. A heat isolation system mainly made of polyurethane foam, glass cloth for reinforcement and humidity-resistant surface, is developed and applied to a run-tank. An evaluation test is carried out with LN2 and the mean value of heat conductivity over the all isolated surface at the temperature of LN2 is found to be 0.012 kcal/mhK. After the evaluation test, the run-tank is used for eight ground firing tests of rockets without any trouble related to the heat isolation system.
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宇宙科学研究所報告 3(3) 1-18 1982年3月Development of spherical cases for the solid propellant rocket motors is presented. These motor cases, made of titanium alloy, have been designed for upper stages of satellite launchers for scientific satellites. In past twenty years, many type of motor cases have been developed corresponding to the ever increasing mission requirement of the Japanese scientific satellites, thereby, overcoming the shortage of budget. In this report, research work carried out to produce more efficient and more large motor cases are outlined, emphasizing the improvement both in material property and manufacturing process.
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宇宙科学研究所報告 1(1) 1-24 1981年9月本報告は新型の単段式観測ロケット「S-520」用モータケース開発研究の概要を述べたものである。 S-520は単段式であるので, 2段式に比べて組立, 発射の作業性が良く, また射場保安の上でも有理である。単段式でありながら, 2段式の K-9M, K-10 の効率的な代替機としてのねらいをももって開発された S-520 では, その高い性能を達成する為に, モータケースにも極度の軽量化, 高い寸法精度及び高い信頼性が要求されたが, 材料の改良と, 最新の構造解析技術及び製造技術の適用により, 要求を満すモータケースを開発することができた。
講演・口頭発表等
243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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科研費 2014年4月 - 2017年3月
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科研費 2008年4月 - 2010年3月
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科研費 2007年 - 2008年
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科研費 2006年 - 2007年