A guidance and control system design for reliability improvement of the next space transportation system
| Project/Area Number |
20760549
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| Research Category |
Grant-in-Aid for Young Scientists (B)
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| Allocation Type | Single-year Grants |
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| Research Field |
Aerospace engineering
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| Research Institution | Nihon University |
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Principal Investigator |
ABE Akio Nihon University, 理工学部, 助教 (60434114)
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| Project Period (FY) |
2008 – 2009
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| Project Status |
Completed (Fiscal Year 2009)
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| Budget Amount *help |
¥2,340,000 (Direct Cost: ¥1,800,000、Indirect Cost: ¥540,000)
Fiscal Year 2009: ¥1,430,000 (Direct Cost: ¥1,100,000、Indirect Cost: ¥330,000)
Fiscal Year 2008: ¥910,000 (Direct Cost: ¥700,000、Indirect Cost: ¥210,000)
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| Keywords | 再使用型宇宙輸送機 / 航空宇宙工学 / 機械力学・制御 / モデル化 / 輸送機器 / Space Transportation / Re-entry / Guidance and Control / Adaptive Control / Trajectory Generation / Collision Avoidance / Onboard Generation |
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| Research Abstract |
In this study, a new guidance and control system for a space transportation system in the next generation is presented. Additionally, the effectiveness and reliability of the proposed guidance and control system are verified. Especially, in 2008 and 2009, the authors attempted to design the guidance system for generating the reference trajectory an adaptive control system which can treat the variations of the vehicle dynamics. The effectiveness of the proposed guidance and control system is verified by the numerical simulation of the onboard computer.
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Report
(3 results)
Research Products
(8 results)
