| Project/Area Number |
23360104
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| Research Category |
Grant-in-Aid for Scientific Research (B)
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| Allocation Type | Single-year Grants |
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| Section | 一般 |
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| Research Field |
Dynamics/Control
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| Research Institution | Nagoya University |
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Principal Investigator |
HARA Susumu 名古屋大学, 工学(系)研究科(研究院), 准教授 (40329850)
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| Co-Investigator(Kenkyū-buntansha) |
OTSUKI Masatsugu 独立行政法人宇宙航空研究開発機構, 宇宙科学研究所, 助教 (50348827)
YAMADA Yoji 名古屋大学, 大学院・工学研究科, 教授 (90166744)
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| Co-Investigator(Renkei-kenkyūsha) |
KUBOTA Kubota 独立行政法人宇宙航空研究開発機構, 宇宙科学研究所, 教授 (90211888)
HASHIMOTO Tatsuaki 独立行政法人宇宙航空研究開発機構, 宇宙科学研究所, 教授 (70228419)
MATSUHISA Hiroshi 京都大学, 大学院・工学研究科, 名誉教授 (00109034)
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| Project Period (FY) |
2011-04-01 – 2014-03-31
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| Project Status |
Completed (Fiscal Year 2013)
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| Budget Amount *help |
¥19,240,000 (Direct Cost: ¥14,800,000、Indirect Cost: ¥4,440,000)
Fiscal Year 2013: ¥3,380,000 (Direct Cost: ¥2,600,000、Indirect Cost: ¥780,000)
Fiscal Year 2012: ¥2,210,000 (Direct Cost: ¥1,700,000、Indirect Cost: ¥510,000)
Fiscal Year 2011: ¥13,650,000 (Direct Cost: ¥10,500,000、Indirect Cost: ¥3,150,000)
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| Keywords | 惑星探査 / 機械力学・制御 / 制御工学 / 航空宇宙工学 / 衝撃 / 制御光学 |
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| Research Abstract |
In order to control shock response of mechanical structures, this study proposes mechanisms and control methods by means of the momentum exchange principle and the energy exchange principle and aims for their applications to shock response control of next generation planetary exploration spacecraft. Simulation and experimental investigation shows that the plural mechanisms and methods proposed by this study enable us to reduce rebound motion and prevent tumbling at lunar/planetary landing and realize robust and high reliable landing.
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