2020 Fiscal Year Annual Research Report
Ballistic Capture Approach and its Application to Martian Moons eXploration (MMX)
Project/Area Number |
19F18371
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Research Institution | Japan Aerospace EXploration Agency |
Principal Investigator |
川勝 康弘 国立研究開発法人宇宙航空研究開発機構, 宇宙科学研究所, 教授 (80373439)
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Co-Investigator(Kenkyū-buntansha) |
DEI TOS DIOGENE ALESSAND 国立研究開発法人宇宙航空研究開発機構, 宇宙科学研究所, 外国人特別研究員
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Project Period (FY) |
2019-04-25 – 2021-03-31
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Keywords | Trajectory optimization / Nonlinear astrodynamics / Ballistic capture / Dynamical system theory / Low-thrust transfer |
Outline of Annual Research Achievements |
a) MMX: I adjusted the ballistic capture model and computed quasi-periodic orbits near Phobos. I investigated the orbit design and demonstrated that the baseline QSOs can be maintained with as low as 6.3 m/s a month. Impulsive transfers indicates budget ~100 m/s and ToF between 7 hr and 2 days.
b) DESTINY+: I optimized the GTO-to-Moon spiral ascent and the interplanetary cruise to Phaethon under strict operational constraints. High-fidelitysolutions give robustness against programmatic and operational delays.
a) EQUULEUS: I provided the end-to-end trajectory product, accounting for realistic high-fidelity models and operational constraints. I shed light to the solution structure for optimal lunar transfers, creating a database oftransfers compatible with the launch parameters.
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Research Progress Status |
令和2年度が最終年度であるため、記入しない。
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Strategy for Future Research Activity |
令和2年度が最終年度であるため、記入しない。
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[Presentation] Operations-driven low-thrust trajectory optimization with applications to DESTINY+2020
Author(s)
D. A. Dei Tos, T. Yamamoto, N. Ozaki, Y. Tanaka, F. Gonzalez-Franquesa, N. Pushparaj, O.Celik, T. Takashima, K. Nishiyama, and Y. Kawakatsu
Organizer
AIAA Scitech Forum 2020, Orlando FL US
Int'l Joint Research