Curriculum Vitaes
Profile Information
- Affiliation
- 特任教授 (シニアフェロー), 宇宙科学研究所 宇宙飛翔工学研究系, 国立研究開発法人宇宙航空研究開発機構
- Degree
- 工学博士
- J-GLOBAL ID
- 200901015159678275
- researchmap Member ID
- 0000023634
Education
1Papers
279-
Acta Astronautica, Sep, 2023
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Journal of Guidance, Control, and Dynamics, 45(7) 1299-1309, 2022 Peer-reviewed
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Acta Astronautica, 179 172-185, Feb, 2021
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AIAA Scitech 2021 Forum, Jan 11, 2021
Misc.
218-
Proceedings of 27th International Symposium on Space Technology and Science (ISTS 2009), 2009-k-21, Jul, 2009 Peer-reviewed
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Planetary People, 18(2) 66-68, Jun 25, 2009
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Proceedings of 1st IAA Planetary Defense Conference, Apr, 2009 Peer-reviewed
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Digests of 10th Planetary Science Symposium, Mar, 2009(in Japanese)
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Journal of the Japan Society of Mechanical Engineers, 112(1082) 3-3, Jan 5, 2009
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アストロダイナミクスシンポジウム講演後刷り集(Web), 18th, 2009
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Digests of 9th Space Science Symposium, P2-85, Jan, 2009(in Japanese)
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2008 Symposium on Flight Mechanics and Astrodynamics, Dec, 2008
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International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008, 3 1512-1519, Dec 1, 2008
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A Collection of Technical Papers of The 18th Workshop on Astrodynamics and Flight Mechanics, 155-160, Jul, 2008
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JOURNAL OF POWER SOURCES, 181(1) 149-154, Jun, 2008
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The proceedings of the JSME annual meeting, 2008 379-380, 2008 Peer-reviewedThis paper describes the attitude dynamics of spacecraft with large flexible structure, such as huge antenna or membrane of solar sail. The coupled motion of the rigid spacecrafts with the flexible structure is complicated, and it is important to predict the motion for the design of configuration or operation planning. It requires a lot of time to calculate the motion of the flexible structure by numerical simulation, and the analysis using simple model is important for exhaustive validation. In this study, a simplified model of the attitude dynamics considering the first vibration mode of flexible structure is introduced. Using this model, the vibration mode of the attitude motion of spacecraft is analyzed. The result of the analysis is confirmed with numerical simulation and compared with the result obtained by use of proven model.
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ELECTROCHEMISTRY, 75(12) 950-957, Dec, 2007
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ELECTROCHEMISTRY, 75(7) 518-522, Jul, 2007
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(6) 121-127, Mar 30, 2007Hayabusa is a spacecraft to explore the asteroid (25143) Itokawa. The spacecraft was launched on May 9, 2003 from Uchinoura Space Center using M-V launch vehicle, and arrived at (25143) Itokawa on September 12, 2005. Hayabusa adopts an Ion Engine System (IES) for its main propulsion. From the viewpoint of navigation, an error in acceleration modeling of low thrust has a great influence on accuracy of orbit determination and prediction.
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Advanced Robotics, 21(14), 2007
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宇宙科学技術連合講演会講演集(CD-ROM), 51st 3J05, 2007
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Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006, 2 1403-1414, Dec 1, 2006
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AIAA 57th International Astronautical Congress, IAC 2006, 6 4204-4213, Dec 1, 2006
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Journal of plasma and fusion research, 82(4) 215-225, Apr 25, 2006
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Proceedings of the IEICE General Conference, 2006(1) "SE-20"-"SE-21", Mar 8, 2006
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Proceedings of the IEICE General Conference, 2006(1) "SS-22"-"SS-27", Mar 8, 2006
Research Projects
8-
Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2018 - Mar, 2023
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2015 - Mar, 2017
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2012 - Mar, 2017
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2014 - Mar, 2016
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, 2007 - 2010
