| Project/Area Number |
21860095
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| Research Category |
Grant-in-Aid for Research Activity Start-up
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| Allocation Type | Single-year Grants |
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| Research Field |
Aerospace engineering
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| Research Institution | Japan Aerospace Exploration Agency |
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Principal Investigator |
NAKAMIYA Masaki Japan Aerospace Exploration Agency, 宇宙科学研究所, 研究員 (10548316)
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| Project Period (FY) |
2009 – 2010
|
| Project Status |
Completed (Fiscal Year 2010)
|
| Budget Amount *help |
¥1,443,000 (Direct Cost: ¥1,110,000、Indirect Cost: ¥333,000)
Fiscal Year 2010: ¥546,000 (Direct Cost: ¥420,000、Indirect Cost: ¥126,000)
Fiscal Year 2009: ¥897,000 (Direct Cost: ¥690,000、Indirect Cost: ¥207,000)
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| Keywords | 力学系理論 / ラグランジュ点 / マニフォールド / 安定マニフォールド |
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| Research Abstract |
We computed the station-keeping of the halo orbit by using the method to reduce the divergent component of the orbital disturbance obtained from the dynamical system theory. As a result, we can reduce the amount of control correction, compared to the conventional method, for the station-keeping. Moreover, we verified that we could use the stable manifold for the transfer from the Japanese launch site to the halo orbit.
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