Satellite attitude estimation by measuring the received power multi-point synchronization
| Project/Area Number |
20560363
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| Research Category |
Grant-in-Aid for Scientific Research (C)
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| Allocation Type | Single-year Grants |
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| Section | 一般 |
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| Research Field |
Communication/Network engineering
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| Research Institution | Hokkaido Institute of Technology |
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Principal Investigator |
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| Project Period (FY) |
2008 – 2011
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| Project Status |
Completed (Fiscal Year 2011)
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| Budget Amount *help |
¥4,810,000 (Direct Cost: ¥3,700,000、Indirect Cost: ¥1,110,000)
Fiscal Year 2011: ¥650,000 (Direct Cost: ¥500,000、Indirect Cost: ¥150,000)
Fiscal Year 2010: ¥650,000 (Direct Cost: ¥500,000、Indirect Cost: ¥150,000)
Fiscal Year 2009: ¥1,560,000 (Direct Cost: ¥1,200,000、Indirect Cost: ¥360,000)
Fiscal Year 2008: ¥1,950,000 (Direct Cost: ¥1,500,000、Indirect Cost: ¥450,000)
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| Keywords | 通信方法(無線、有線、衛星、光、移動) / アマチュア衛星通信 / 超小型衛星 / CubeSat / HIT-SAT / 回転速度 / 姿勢推定 / 指向性アンテナ / 多地点同期受信 / M-Vロケット / 超小型人工衛星 / Cube-Sat / スピン / 自転速度 / アンテナ / 指向特性 |
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| Research Abstract |
Antenna are mounted on nano-satellite(CubeSat satellite class), it is a dipole antenna of amateur radio band is almost. Therefore, the satellite attitude estimation is possible by using the antenna radiation pattern, measuring the change in received power at the ground receiving station. In addition, we revealed in measurement and analysis of real data that by receiving multi-point synchronization, satellite attitude estimation is possible in a short time.
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Report
(6 results)
Research Products
(76 results)
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[Journal Article] and HIT-SAT development team : "Orbital experiment of nano-satellite "HIT-SAT" as a sub-payload of M-V rocket"2008
Author(s)
T.Sato, R.Mitsuhashi, S.Satori, K.Isimura, T.Totani, A.Nakamura, K.Hori, T.Yasunaka
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Journal Title
Proc.of 26th International Symposium on Space Technology and Science, Hamamatsu, Japan, 2008-u-15
Related Report
Peer Reviewed
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