研究者業績

峯杉 賢治

Minesugi Kenji

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 教授
学位
工学博士(1991年3月 東京大学)

J-GLOBAL ID
201801002275500853
researchmap会員ID
B000340311

論文

 43
  • 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.
  • ISHIMURA Kosei, ISHIDA Manabu, KAWANO Taro, MINESUGI Kenji, ABE Kazuhisa, SASAKI Takashi, IIZUKA Ryo, BANDO Nobutaka
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 16(2) 181-187 2018年  
    <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>
  • Yoh Takei, Susumu Yasuda, Kosei Ishimura, Naoko Iwata, Atsushi Okamoto, Yoichi Sato, Mina Ogawa, Makoto Sawada, Taro Kawano, Shingo Obara, Chikara Natsukari, Atsushi Wada, Shinya Yamada, Ryuichi Fujimoto, Motohide Kokubun, Noriko Y. Yamasaki, Hiroyuki Sugita, Kenji Minesugi, Yasuo Nakamura, Kazuhisa Mitsuda, Tadayuki Takahashi, Seiji Yoshida, Shoji Tsunematsu, Kenichi Kanao, Katsuhiro Narasaki, Kiyomi Otsuka, F. Scott Porter, Caroline A. Kilbourne, Meng P. Chiao, Megan E. Eckart, Gary A. Sneiderman, James T. Pontius, Dan McCammon, Paul Wilke, John Basile
    Journal of Astronomical Telescopes, Instruments, and Systems 4(1) 2018年1月1日  査読有り
    © The Authors 2018. Published by SPIE under a Creative Commons Attribution 3.0 Unported License. Distribution or reproduction of this work in whole or in part requires full attribution of the original publication, including its DOI. The soft x-ray spectrometer (SXS) onboard ASTRO-H (named Hitomi after launch) is a microcalorimeter-type spectrometer, installed in a dewar to be cooled at 50 mK. The energy resolution of the SXS engineering model suffered from microvibration from cryocoolers mounted on the dewar. This is mitigated for the flight model (FM) by introducing vibration isolation systems between the cryocoolers and the dewar. The detector performance of the FM was verified before launch of the spacecraft in both ambient condition and thermal-vacuum condition, showing no detectable degradation in energy resolution. The in-orbit detector spectral performance and cryocooler cooling performance were also consistent with that on ground, indicating that the cryocoolers were not damaged by launch environment. The design and performance of the vibration isolation system along with the mechanism of how the microvibration could degrade the cryogenic detector is shown. Lessons learned from the development to mitigate unexpected issues are also described.
  • 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.
  • Maeda Yoshitomo, Ishida Manabu, Iizuka Ryo, Iwata Naoko, Minesugi Kenji, Ishimura Kosei, Kawano Taro, Ogawa Hiroyuki, Taniguchi Shohei, Kawamoto Masamitsu, Shionome Yu, Someya Kentaro, Sato Takuro, Ichihara Kou, Tomikawa Kazuki, Sato Toshiki, Kikuchi Naomichi, Serlemitsos Peter, Soong Yang, Okajima Takashi, Olsen Larry, Robinson David, McGuinness Dan, Szymkiewicz Richard, Hahne Devin, Sytwu Joseph, Kearney John, Toomey Emory, Lozipone Larry, Brown Clif, Numata Ai, Galassi Nick, Thorpe Rosemary, Contino Dominic, Pless Paul, Schofield Mark, Chang Bill, Rice Brian, Henry Chris, Glenn Kevin, Koenecke Richard, Cottingham Christine, Mori Hideyuki, Hayashi Takayuki, Tawara Yuzuru, Tachibana Kenji, Torii Tatsuharu, Tamura Keisuke, Ishibashi Kazunori, Kunieda Hideyo, Ogasaka Yasushi, Sakurai Ikuya, Mochida Masayuki, Kawabata Eiji, Ito Toshihiro, Iwase Toshihiro, Kurebayashi Yuuki, Watanabe Tsuyoshi, Awaki Hisamitsu, Ogi Keiji, Itoh Keitaro, Izumiya Takanori, Awaya Takashi, Okada Gohta, Minami Sari, Sugita Satoshi, Miyazawa Takuya, Furuzawa Akihiro
    日本物理学会講演概要集 71 369-369 2016年  
    <p>X線天文衛星「ひとみ」には、軟X線望遠鏡(Soft X-ray Telescope: SXT)が二台搭載された。米国のGSFC/NASAが主体で開発されている。SXT-S、SXT-Iと呼ばれ、それぞれの焦点面検出器はX線カロリメーター検出器 SXS、X線CCDカメラ SXI に対応する。どちらの検出器にも天体の像が結ばれていることが確認できた。また、スペクトル中には地上のキャリブレーションで予想していた反射鏡表面に金のMやLの吸収端が見えていた。当講演では、機上で得られた性能及び、地上との予測の比較を報告する。</p>

MISC

 91
  • 塩谷圭吾, 中川貴雄, 村上浩, 金田英宏, 佐藤栄一, 峯杉賢治, 八田博, 尾中敬
    日本金属学会講演概要 136th 2005年  
  • 槙原幹十朗, 小野田淳次郎, 峯杉賢治
    構造強度に関する講演会講演集 47th 54-56 2005年  
  • 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 271-276 2005年  
    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  
    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.
  • 竹内 伸介, 峯杉 賢治, 津田 雄一
    宇宙科学シンポジウム 4 187-190 2004年1月8日  
  • 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 272 2004年  
  • 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  
  • 峯杉 賢治, 下瀬 滋
    宇宙科学研究所報告. 特集 47 467-482 2003年3月  
  • 峯杉 賢治, 小野田 淳次郎
    宇宙科学研究所報告 特集 (47) 25-84 2003年3月  
  • 下瀬 滋, 峯杉 賢治
    宇宙科学研究所報告 特集 (47) 467-481 2003年3月  
  • 大久保洋志, 渡辺直行, 峯杉賢治, 小野田淳次郎, 高橋巧
    構造強度に関する講演会講演集 44th 134-136 2002年7月24日  
  • OH H‐U, 小野田淳次郎, 峯杉賢治
    構造強度に関する講演会講演集 43rd 181-184 2001年8月1日  
  • H. U. Oh, J. Onoda, K. Minesugi
    Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2 986-991 2001年1月1日  
    This paper shows the effectiveness of a semiactive vibration isolator filled with liquid-crystal type electro-rheological (ER) fluid for disturbances generated by momentum-wheels. The principal characteristics of an ER isolator was measured in dynamic tests, and a mathematical model of the isolator was proposed. Two control laws for semiactive approach were proposed. Numerical simulation results indicated that the proposed semiactive control produced much better isolation performance than a passive system.
  • 安野 拓也, 栗林 一彦, 峯杉 賢治
    いわき明星大学理工学部研究紀要 (13) 55-64 2000年3月  
  • 清水さやか, 大久保洋志, 渡辺直行, 峯杉賢治, 小野田淳次郎
    構造強度に関する講演会講演集 41st 241-244 1999年7月14日  
  • 安野拓也, 安孫子紀子, 長谷川正, 栗林一彦, 峯杉賢治, 小野田淳次郎
    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年  
  • 東海林和典, 菊池忠彦, 竹井秀樹, 梅里真弘, 峯杉賢治, 小野田淳次郎
    宇宙科学技術連合講演会講演集 42nd 1093-1098 1998年10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 1-34 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。
  • Junjiro Onoda, Hyun Ung Oh, Kenji Minesugi
    Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 3 1813-1821 1998年1月1日  
    This paper proposes and investigates a method to enhance ER-fluid variable dampers for semiactive vibration suppression. The ER-fluid dampers studied in this paper can be modeled as a variable friction damper. The friction in the damper is an increasing function of the absolute value of the voltage applied to the electrode of the damper. Generally, the friction is not zero even when no voltage is applied. Semiactive vibration suppression is to control the friction such that vibrations damp quickly. Therefore, to suppress large amplitude vibrations to small amplitude, the friction needs to be varied through a large range. In other word, the ratio of the maximum and minimum values of the frictional force needs to be large. To increase the ratio by decreasing the minimum frictional force, this paper proposes to excite a high-frequency vibration of the electrode. The effectiveness of the electrode vibration for the reduction of the minimum frictional force is demonstrated in this paper by both static experiments and semiactive vibration suppression experiments. The results of semiactive vibration suppression experiments indicate that the minimum frictional force is reduced by the electrode vibration by factor of 1/3-1/2.
  • 小野田淳次郎, 峯杉賢治, 中村正俊, 柳沢昇
    構造強度に関する講演会講演集 40th 241-244 1998年  
  • 小野田淳次郎, 峯杉賢治, 大塚秀和
    構造強度に関する講演会講演集 39th 241-244 1997年  
  • 小野田淳次郎, 峯杉賢治, 中村正俊, 柳沢昇
    構造強度に関する講演会講演集 39th 237-240 1997年  
  • 小野田淳次郎, 峯杉賢治
    構造強度に関する講演会講演集 39th 229-232 1997年  
  • 小野田淳次郎, 栗林一彦, 峯杉賢治, 西田稔夫
    構造強度に関する講演会講演集 39th 233-236 1997年  
  • 小野田淳次郎, 峯杉賢治, 竹内伸介
    構造強度に関する講演会講演集 39th 337-340 1997年  
  • 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.
  • Kenji Minesugi, Junjiro Onoda, Hiroshi Ohkubot, Yoji Hanawa
    37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference 1016-1023 1996年1月1日  
    © 1996, American Institute of Aeronautics and Astronautics, Inc. All rights reserved. Passive 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.
  • 小野田淳次郎, 峯杉賢治, OH H U
    構造強度に関する講演会講演集 38th 225-228 1996年  
  • 大久保洋志, 峯杉賢治, 小野田淳次郎, 渡辺直行
    構造強度に関する講演会講演集 38th 313-316 1996年  
  • 小野田淳次郎, 峯杉賢治, 竹内伸介
    構造強度に関する講演会講演集 38th 129-132 1996年  
  • 樋口健, 小野田淳次郎, 峯杉賢治, 芝山有三, 東海林和典, 菊池忠彦, 大賀弘一
    宇宙科学技術連合講演会講演集 39th 381-382 1995年10月  
  • 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.
  • 小野田淳次郎, 峯杉賢治, 中村正俊
    構造強度に関する講演会講演集 36th 81-84 1994年  
  • 小野田淳次郎, 峯杉賢治, 中村正俊, 松田豊
    構造強度に関する講演会講演集 36th 77-80 1994年  
  • 塙洋二, 小野田淳次郎, 峯杉賢治
    構造強度に関する講演会講演集 36th 101-104 1994年  
  • 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, 峯杉賢治
    構造強度に関する講演会講演集 35th 198-201 1993年  
  • 小野田淳次郎, 峯杉賢治
    構造強度に関する講演会講演集 35th 194-197 1993年  
  • 峯杉賢治, 小野田淳次郎, 平田安弘, 富沢利夫, 長谷川克也
    構造強度に関する講演会講演集 35th 62-65 1993年  
  • 佐野哲史, 小野田淳次郎, 峯杉賢治
    構造強度に関する講演会講演集 34th 114-117 1992年  

講演・口頭発表等

 13

担当経験のある科目(授業)

 2

共同研究・競争的資金等の研究課題

 12