研究者業績

小野田 淳次郎

オノダ ジュンジロウ  (Junjiro Onoda)

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

論文

 105
  • Junjiro Onoda, Kenji Minesugi, Seong-Cheol Kwon, Hyun-Ung Oh
    Smart Materials and Structures 30(6) 065014-065014 2021年6月1日  
    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.
  • Seong-Cheol Kwon, Junjiro Onoda, Hyun-Ung Oh
    Sensors and Actuators A: Physical 281 55-66 2018年10月  査読有り
  • Seong-Cheol Kwon, Junjiro Onoda, Hyun-Ung Oh
    Mechanical Systems and Signal Processing 2018年8月  査読有り
  • Junjiro Onoda, Shigeru Shimose, Kenji Minesugi
    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.
  • Shigeru Shimose, Kanjuro Makihara, Junjiro Onoda
    Smart Materials Research 2013(Article No. 736487) 2013年1月  査読有り

MISC

 51
  • 小野田淳次郎, 峯杉賢治, KWON Seong-Cheol, OH Hyun-Ung
    構造強度に関する講演会講演集 62nd 2020年  
  • 小野田淳次郎, 峯杉賢治, KWON Seong-Cheol, OH Hyun-Ung
    構造強度に関する講演会講演集 61st 2019年  
  • 小野田淳次郎, 峯杉賢治, 下瀬滋
    構造強度に関する講演会講演集 60th 2018年  
  • 小野田淳次郎
    日本法科学技術学会誌 20(Supplement) 1-2 2015年10月26日  
  • 小野田 淳次郎
    Explosion 22(1) 1-1 2012年4月30日  
  • 槙原 幹十朗, 下瀬 滋, 竹内 伸介, 小野田 淳次郎
    機械力学・計測制御講演論文集 2011 18-18 2011年9月4日  
  • 槙原 幹十朗, 小野田 淳次郎, 養父 拓也
    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.
  • 槙原幹十朗, 小野田淳次郎, 峯杉賢治
    自動制御連合講演会(CD-ROM) 49th ROMBUNNO.SU2-3-3 2006年  
  • 槙原幹十朗, 小野田淳次郎, 峯杉賢治
    自動制御連合講演会(CD-ROM) 48th H1-26 2005年11月25日  
  • 槙原 幹十朗, 小野田 淳次郎, 峯杉 賢治
    「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.
  • 槙原 幹十朗, 小野田 淳次郎, 峯杉 賢治
    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.
  • 金田英宏, 中川貴雄, 村上浩, 小野田淳次郎, 佐藤英一, 名取通弘, 八田博志, 峯杉賢治, 奥泉信克, 塩谷圭吾, 尾中敬, 山城亮治
    日本天文学会年会講演予稿集 2004 2004年  
  • 小野田淳次郎
    ミノル記念講演会講演録 10th 29P 2003年12月16日  
  • 小野田淳次郎
    宇宙科学研究所報告 特集 (47) 5-11 2003年3月  
  • 小野田淳次郎, 峯杉賢治
    宇宙科学研究所報告 特集 (47) 25-84 2003年3月  
  • 安野拓也, 栗林一彦, 峯杉賢治, 小野田淳次郎
    いわき明星大学理工学部研究紀要 (13) 55-64 2000年3月20日  
  • 小野田淳次郎
    日本航空宇宙学会誌 46(538) 585-593 1998年11月  
  • 竹内伸介, 小野田淳次郎, 峯杉賢治, 橋元保雄, 富沢利夫, 下瀬滋
    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。
  • 小野田 淳次郎, 長島 隆一
    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  
  • 森昌彦, 西田稔夫, 久利修平, 名山理介, 小野田淳次郎, 栗林一彦
    三菱重工技報 33(3) 186-189 1996年5月  
  • 小野田 淳次郎
    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  
  • Junjiro Onoda, Hyun Ung Oh, Kenji Minesugi
    37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference 1569-1577 1996年1月1日  
    © 1996, American Institute of Aeronautics and Astronautics, Inc. To 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.
  • 小野田淳次郎
    システム/制御/情報 39(3) 136-141 1995年3月  
  • 横田俊昭, 佐々木進, 田中真, 遠山文雄, 太田正広, 小野田淳次郎, 戸田勧, 鈴木良昭, 八坂哲雄
    宇宙基地利用基礎実験費研究成果報告書 平成6年度 国際宇宙観測共同事業費(IML-2計画参加) 22-45 1995年  
  • Kenji Minesugi, Junjiro Onoda, Yoji Hanawa
    Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 1 200-206 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.
  • Junjiro Onoda, Dan Ying Fu, Kenji Minesugi
    Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2 1060-1067 1995年1月1日  
    A two-dimensionally deployable truss structure is newly proposed for space application, whose most significant feature is its small number of mechanisms to be locked when it is deployed. Its packaging efficiency is shown to be better than many known deployable trusses. Several versions of the truss are also proposed. To confirm that the new deployable truss has enough design flexibility, a paraboloidal truss platform is designed for trial. Furthermore, a numerical investigation shows that the platform is actually deployable/foldable from the practical point of view.
  • Junjiro Onoda, Tetsuji Sano, Kenji Minesugi
    Collection of Technical Papers - AIAA/ASME Structures, Structural Dynamics and Materials Conference 2095-2100 1993年1月1日  
    A new approach to the passive vibration suppression of truss structures has been proposed and investigated. The approach is to take advantage of the preloaded backlashes introduced at the joints of truss structures. Because of the preload, the structure keeps its high stiffness and high static shape accuracy when the external load and the vibration level are low enough. When the response of the structure exceeds a certain level, e.g. allowable level, the backlashes at the joints start slipping, introducing the frictional damping and a nonlinearity. This nonlinearity transfers energy from a vibration mode to another. Because the vibration of higher modes usually damp sooner, this nonlinearity transfers energy from the lower modes to the higher modes, resulting in a quick damping of entire vibration. Numerical simulations show that the energy transfer between the modes drastically enhances the inherent damping capability of the structure. Resulting damping can be as large as that due to the frictional force at the backlashes even when the inherent damping ratio of each mode is as low as 0.1-0.2%. The simulation results demonstrate that both the frictional force and the enhanced inherent damping, especially the combination of them, suppress the vibration nicely.
  • 小野田淳次郎, 渡辺直行, 市田和夫, 橋元保雄, 中田篤
    宇宙科学研究所報告 特集 29(29) 87-113 1991年6月  
  • 小野田淳次郎, 渡辺直行
    CAS研究報告 (31) 129-132 1988年3月  
  • 小野田淳次郎
    CAS研究報告 (31) 125-128 1988年3月  
  • 小野田淳次郎, HAFTKA R T
    CAS研究報告 (30) 9-12 1987年3月  
  • 森大吉郎, 小野田淳次郎, 橋本保雄, 中田篤, 名取通弘, 市田和夫
    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。
  • 小野田淳次郎, 富沢利夫, 中田篤, 橋元保雄, 今沢茂夫, 市田和夫, 森大吉郎
    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.
  • 小野田淳次郎
    CAS研究報告 (28) 125-134 1985年3月  
  • 小野田淳次郎
    CAS研究報告 (27(A)) 35-46 1984年3月  
  • 小野田淳次郎, 名島憲治, 岡崎洋
    宇宙科学研究所報告 特集 (6) 155-166 1983年3月  
  • 三浦公亮, 酒巻正守, 小野田淳次郎, 名取通弘
    CAS研究報告 (26) 61-66 1983年3月  
  • 森大吉郎, 小野田淳次郎, 細村建夫, 白銀博
    CAS研究報告 (26) 67-71 1983年3月  
  • 小野田淳次郎, 森大吉郎
    CAS研究報告 (25) 33-44 1982年3月  
  • 森大吉郎, 小野田淳次郎
    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.
  • 森大吉郎, 小野田淳次郎, 今政とし郎, 下山仁一, さい藤一雄, 岡崎洋
    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。
  • 小野田淳次郎, 森大吉郎
    CAS研究報告 (24) 77-84 1981年3月  
  • 森大吉郎, 小野田淳次郎, 橋元保雄, 村上卓司, 白銀博, 小野島昇
    東京大学宇宙航空研究所報告 16(4A) 1207-1221 1980年11月  
  • 森大吉郎, 小野田淳次郎, 今政惇郎, 下山仁一, 斉藤一雄, 岡崎洋
    三菱重工技報 17(5) 120-129 1980年9月  
  • 小野田淳次郎, 森大吉郎
    CAS研究報告 (23) 121-126 1980年3月  
  • 今沢茂夫, 小野田淳次郎, 中田篤, 富沢利夫
    東京大学宇宙航空研究所報告 16(1 (B)) 355-367 1980年2月  
  • 森大吉郎, 小野田淳次郎, 橋元保雄, 細村健夫
    東京大学宇宙航空研究所報告 16(1 (B)) 215-231 1980年2月  
  • 小野田淳次郎, 今沢茂夫, 森大吉郎, 砂川恵, 秋葉鐐二郎, 棚次亘弘
    東京大学宇宙航空研究所報告 15(1 (B)) 177-185 1979年3月  
  • 今沢茂夫, 小野田淳次郎, 中田篤
    東京大学宇宙航空研究所報告 14(1 (B)) 311-321 1978年3月  
  • 橋元保雄, 八坂哲雄, 小野田淳次郎
    東京大学宇宙航空研究所報告 14(1B) 53-76 1978年3月  

講演・口頭発表等

 241

共同研究・競争的資金等の研究課題

 12