Curriculum Vitaes
Profile Information
- Affiliation
- Professor, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
- Degree
- Ph.D.(The University of Tokyo)
- researchmap Member ID
- 1000144488
Research Interests
2Education
4Committee Memberships
2-
Jun, 2008 - Jun, 2010
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Apr, 2005 - Mar, 2006
Papers
122-
Smart Materials and Structures, Aug 1, 2024 Peer-reviewed
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Smart Materials and Structures, 30(6) 065014-065014, Jun 1, 2021 Peer-reviewedAbstract 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, Oct, 2018 Peer-reviewed
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Mechanical Systems and Signal Processing, 117, Aug, 2018 Peer-reviewed
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JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 28(7) 888-906, Apr, 2017 Peer-reviewed
Misc.
42-
日本航空宇宙学会誌 = Journal of the Japan Society for Aeronautical and Space Sciences, 54(628) 126-126, May 5, 2006
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宇宙科学研究所報告, 100(100) 36P-34, Mar, 1998In this paper, the trajectory dispersion of the Viper rocket caused by the elastic vibration of the vehicle and rocket launcher is investigated. In order to estimate the trajectory dispersion, a three dimensional numerical simulation of the launch was carried out considering the elastical effect of the vehicle and rocket launcher. The accuracy of the numerical simulation was validated first by the comparison with the vibration data measured on actual launch, and after that the trajectory dispersion was estimated by the simulation. As the result, it is confirmed that the trajectory dispersion caused by th elastic vibration is no matter on actual launch mission.
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システム/制御/情報, 39(3) 136-141, Mar, 1995
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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
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CAS研究報告, (31) 129-132, Mar, 1988
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CAS研究報告, (31) 125-128, Mar, 1988
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CAS研究報告, (30) 9-12, Mar, 1987
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宇宙科学研究所報告, 40(40) 22P-21, Oct, 1986This 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, Mar, 1983A 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, Mar, 1982Development 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, Sep, 1981This paper presents the development of the motor case of the newly developed single stage sounding rocket"S-520". This rocket being a single stage rocket, in compariosn with the previously developed K-9M and K-10 versions which are two stage, has the advantage of simplicity in operation and handling, and also of better range safety. In the development of this sounding rocket of high performance, extreme weight saving, precise alignment and high reliability of the motor case were required. Using the improved material, design technique using FEM structural analysis and new fabrication techniques such as EBW, the motor case which satisfies all the requirements has been developed and the burst test by hydropressure showed its high reliability.
Presentations
247-
JSASS/JSME/JAXA Structures Conference, Aug 7, 2020
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JSASS/JSME/JAXA/SURCAS Structures Conference, Aug 9, 2019
Professional Memberships
4Works
2Research Projects
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科学研究費助成事業 基盤研究(C), 日本学術振興会, Apr, 2020 - Mar, 2023
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科研費, Apr, 2014 - Mar, 2017
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科研費, Apr, 2008 - Mar, 2010
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科研費, 2007 - 2008
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科研費, 2006 - 2007