| Project/Area Number |
23246148
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| Research Category |
Grant-in-Aid for Scientific Research (A)
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| Allocation Type | Single-year Grants |
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| Section | 一般 |
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| Research Field |
Aerospace engineering
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| Research Institution | Japan Aerospace Exploration Agency |
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Principal Investigator |
KAWASAKI Shigeo 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 (40266367)
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| Co-Investigator(Kenkyū-buntansha) |
INATANI Yoshifumi 宇宙航空研究開発機構, 宇宙科学研究所, 教授 (10168403)
NARUO Yoshihiro 宇宙航空研究開発機構, 宇宙科学研究所, 助教 (70150050)
MITA Makoto 宇宙航空研究開発機構, 宇宙科学研究所, 助教 (40370100)
MARU Yusuke 宇宙航空研究開発機構, 宇宙科学研究所, 助教 (20524101)
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| Co-Investigator(Renkei-kenkyūsha) |
YOSHIDA Satoshi 宇宙航空研究開発機構, 宇宙科学研究所, 宇宙航空プロジェクト研究員 (50751830)
MIYAJI Akihira 宇宙航空研究開発機構, 宇宙科学研究所, 招聘研究員 (40734091)
NISHIKAWA Kenjiro 鹿児島大学, 工学部電気電子工学科, 教授 (80610245)
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| Research Collaborator |
ITOH Tatsuo カリフォルニア大学, ロサンゼルス校, 教授
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| Project Period (FY) |
2011-04-01 – 2015-03-31
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| Project Status |
Completed (Fiscal Year 2014)
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| Budget Amount *help |
¥30,420,000 (Direct Cost: ¥23,400,000、Indirect Cost: ¥7,020,000)
Fiscal Year 2014: ¥4,680,000 (Direct Cost: ¥3,600,000、Indirect Cost: ¥1,080,000)
Fiscal Year 2013: ¥13,260,000 (Direct Cost: ¥10,200,000、Indirect Cost: ¥3,060,000)
Fiscal Year 2012: ¥12,480,000 (Direct Cost: ¥9,600,000、Indirect Cost: ¥2,880,000)
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| Keywords | ヘルスモニタリング / ワイヤレスセンサネットワーク / 無線電力伝送 / Fly-by-Wireless / ワイヤレスセンサーネットワーク |
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| Outline of Final Research Achievements |
In this study, the wireless safety monitoring sensor system by a IC sensor-tag applying the wireless communication/sensor and power transmission technology was demonstrated. This system consists of RF-ICs and the IC sensor-tag by a hybrid integrated circuit, a compact base station and firmware to control data sending, sequence, and wireless powering.
We obtained the official experiment license to realize the system and proved the compatibility of sensor information and date sending by the Zigbee operating at 2.45 GHz with microwave power transmission at 5.8 GHz in the reusable spacecraft prototype model. From this study, we are confirmed that the wireless safety monitoring sensor system for the complete harness-free reusable spacecraft is feasible using the wireless information/communication and power transmission technology.
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