Function Demonstration Study of Variable-Shape Space Systems Utilizing Microsatellite System Technology
Project/Area Number |
26289329
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Research Category |
Grant-in-Aid for Scientific Research (B)
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Allocation Type | Partial Multi-year Fund |
Section | 一般 |
Research Field |
Aerospace engineering
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Research Institution | Tokyo Institute of Technology (2015-2016) Japan Aerospace Exploration Agency (2014) |
Principal Investigator |
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Project Period (FY) |
2014-04-01 – 2017-03-31
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Project Status |
Completed (Fiscal Year 2016)
|
Budget Amount *help |
¥15,990,000 (Direct Cost: ¥12,300,000、Indirect Cost: ¥3,690,000)
Fiscal Year 2016: ¥2,860,000 (Direct Cost: ¥2,200,000、Indirect Cost: ¥660,000)
Fiscal Year 2015: ¥6,110,000 (Direct Cost: ¥4,700,000、Indirect Cost: ¥1,410,000)
Fiscal Year 2014: ¥7,020,000 (Direct Cost: ¥5,400,000、Indirect Cost: ¥1,620,000)
|
Keywords | 宇宙システム / 超小型衛星 / 再構成システム / 航空宇宙工学 / 超小型衛星システム |
Outline of Final Research Achievements |
In order to meet advanced requirements in near future microsatellite missions, research and development of microsatellite system technology were conducted for enhancement of its functionality. In particular, flight model of 50kg micarosatellite TSUBAME was finished, launched and operated to gain valuable lessoned learned. Next, concept of variable-shape space system was focused which has configuration change function in order to make itself adaptive for task requirement in mission operations. In the study, variable-shape attitude control was proposed and its fundamental research was conducted: extraction of element technology, analysis, development and experiment. In particular, concept design of 50kg micarosatellite Hibari was reviewed using variable-shape attitude control to conduct a new scientific observation.
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Report
(4 results)
Research Products
(58 results)
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[Presentation] Wrinkling of a Membrane with a Curved Small Thin Film2017
Author(s)
Masanori Matsushita, Osamu Mori, Nobukatsu Okuizumi, Yasutaka Satou, Takashi Iwasa, and Saburo Matunaga
Organizer
31th International Symposium on Space Technology and Science
Place of Presentation
Ehime Prefectural Cultural Hall
Year and Date
2017-06-03
Related Report
Int'l Joint Research
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[Presentation] 深層学習を用いた新しい衛星姿勢決定方法の開発2017
Author(s)
吉井健敏, 太田佳, 松下将典, 菊谷侑平, 林雄希, 小池毅彦, 新谷勇介, 針田聖平, 小澤俊貴, 下川辺隆史, 谷津陽一, 河合誠之, 松永三郎
Organizer
第17回宇宙科学シンポジウム
Place of Presentation
ISAS, 神奈川
Year and Date
2017-01-05
Related Report
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[Presentation] Flight Model Development of the Micro-satellite TSUBAME2015
Author(s)
Masanori Matsushita, Shota Kawajiri, Takashi Nagasu, Eugene Kim, Kazuyoshi Miyasato, Souta Suzuki, Kyosuke Tawara, Kei Ohta, Masaya Koga, Hao Ting, Shin Kurita, Nagahisa Moriyama, Makoto Arimoto, Yoichi Yatsu, Shinichi Kimura, Saburo Matunaga
Organizer
10th IAA Symposium on Small Satellites for Earth Observation
Place of Presentation
Berlin, Germany
Year and Date
2015-04-20
Related Report
Int'l Joint Research
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[Presentation] 超小型衛星TSUBAMEのフライトモデル開発とクリティカルフェーズ運用2014
Author(s)
松下将典,河尻翔太,長洲 孝,宮里知良, 鈴木聡太,俵 京佑,キム・ユージン,太田 佳,古賀将哉,下中淳史,カク・テイ,栗田 真, 森山長久,有元 誠,谷津陽一,木村真一,松永三郎
Organizer
5th UNISEC Space Takumi Conference for Practical Study of Problem Finding and Solving in Space Systems
Place of Presentation
ISAS
Year and Date
2014-12-26
Related Report
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