| Project/Area Number |
23560960
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| Research Category |
Grant-in-Aid for Scientific Research (C)
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| Allocation Type | Multi-year Fund |
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| Section | 一般 |
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| Research Field |
Aerospace engineering
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| Research Institution | Nanzan University |
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Principal Investigator |
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| Research Collaborator |
BANDO Mai 九州大学, 大学院工学研究科, 助教 (40512041)
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| Project Period (FY) |
2011 – 2013
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| Project Status |
Completed (Fiscal Year 2013)
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| Budget Amount *help |
¥3,510,000 (Direct Cost: ¥2,700,000、Indirect Cost: ¥810,000)
Fiscal Year 2013: ¥910,000 (Direct Cost: ¥700,000、Indirect Cost: ¥210,000)
Fiscal Year 2012: ¥1,040,000 (Direct Cost: ¥800,000、Indirect Cost: ¥240,000)
Fiscal Year 2011: ¥1,560,000 (Direct Cost: ¥1,200,000、Indirect Cost: ¥360,000)
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| Keywords | 制限3体問題 / ラグランジュ点 / ハロー軌道 / 楕円軌道 / フォーメーションフライト / パルス制御 / インパルス制御 / フィードバック制御 / 楕円制限３体問題 / アクティブフォーメーション / 楕円制限3体問題 / フォーメーション / 総速度変化 |
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| Research Abstract |
In this work, we have proposed a design method of feedback control systems for the generation and maintenance of small halo orbits near a Lagrangian point and for formation flying in the vicinity of a halo orbit in the Earth-moon-satellite three-body system. We have also shown how to design feedback controls with low fuel consumption for formation flying along an eccentric orbit in the cases of continuous control, impulse control and pulse control. To allow for the flexibility of the reference orbit, we have proposed active formation flying where the reference orbit is generated by an exogenous system and is maintained by feedback controls.
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