Curriculum Vitaes
Profile Information
- Affiliation
- Senior Researcher, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
- Degree
- 博士（工学）(Mar, 2005, 東京大学)
- Researcher number
- 60443280
- J-GLOBAL ID
- 202001000370405138
- researchmap Member ID
- R000014112
Research History
3-
Apr, 2006 - Present
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Apr, 2005 - Mar, 2006
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Apr, 1999 - Mar, 2002
Education
4-
Apr, 1997 - Mar, 1999
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Apr, 1993 - Mar, 1995
Committee Memberships
4-
Apr, 2019 - Mar, 2021
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Nov, 2014 - Aug, 2017
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Nov, 2009 - Jul, 2014
Awards
9-
Mar, 2019
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May, 2013
-
Jan, 2011
Papers
104-
The 13th SICE Multi-Symposium on Control Systems, Mar, 2026 Lead author
Misc.
63-
宇宙科学技術連合講演会講演集(CD-ROM), 67th, Jan 15, 2025DESTINY+ is a planned JAXA medium-class Epsilon mission from Earth to deep space using a low-thrust, many-revolution orbit. Such a trajectory design is a challenging problem not only for trajectory design but also for flight operations, and in particular, it is essential to evaluate the impact of operational uncertainties to ensure mission success. In this study, we design the low-thrust trajectory from Earth orbit to a lunar transfer orbit by differential dynamic programming using the Sundman transformation. The results of Monte Carlo simulations with operational uncertainties confirm that the spacecraft can be successfully guided to the lunar transfer orbit by using the feedback control law of differential dynamic programming in the angular domain.
