RESEARCH

Spacecraft Orbit Control & Trajectory Design

Mission Analysis for “Dismantling Rubble Pile Asteroids with AoES”: Active orbital control using SRP
(CU Boulder, 2017-present) PI: Prof. Jay McMahon

Funded by NASA Innovative Advanced Concepts (NIAC) program.

I am currently working on mission analysis for the new concept of asteroid exploration, “Dismantling Rubble Pile Asteroids with AoES.” This mission concept is to explore and mine small asteroids using a light-weight soft robot. This spacecraft also takes advantage of its high area-to-mass ratio to control the orbit around asteroids exploiting Solar Radiation Pressure (SRP), which is a dominant force around small bodies.

My current work is to develop orbital control strategies and show the feasibility of the mission concept. Some of the results are presented and published at some technical conferences and their proceedings (see publication).

Mission Analysis for the First Cis-Lunar Exploration CubeSat EQUULEUS
(UTokyo & ISAS/JAXA, 2016-present)

Funded by ISAS/JAXA.

I worked on design of the science orbits for EQUilibriUm Lunar-Earth point 6U Spacecraft (EQUULEUS) mission, as a member of the Mission analysis team led by Dr. S. Campagnola. (see here about EQUULEUS mission)

Our work leverages the circular restricted three-body problem (CR3BP) and nonlinear programming (NLP) in order to systematically and efficiently design quasi-halo orbits in the ephemeris model and perform stationkeeping analysis. The systematic approach enabled us to design over 13,000 of quasi-halo orbits and perform Monte-Carlo stationkeeping simulation for each, which has contributed to the complex mission design in the multi-body regime with constrained launch conditions.

Quasi-halo orbits designed in the ephemeris model

Attitude & Orbit Control of Solar Sailing Spacecraft
(UTokyo, 2014-2017)

The first solar sail IKAROS. © JAXA

Funded by Grant-in-Aid for scientific research #17J09626 as a JSPS DC1 fellow (2017-), which is one of the most prestigious fellowships for Ph.D. students in Japan.

TBW

Micro Spacecraft Development
– System Design, Trajectory Design & Attitude Control

The First Cis-Lunar Exploration CubeSat EQUULEUS
(UTokyo & ISAS/JAXA, 2016-present) PI: Prof. T. Hashimoto & Prof. R. Funase

Funded by ISAS/JAXA.

For EQUULEUS mission, in addition to its mission analysis, I worked on the system design as a system manager.

EQUULEUS is a 6U CubeSat scheduled to be launched in 2019 by NASA’s Space Launch System (SLS) Exploration Mission 1 (EM-1) (visit here for more detail). The CubeSat aims to reach the 2nd Earth-Moon Lagrange point (EML2) by using low-energy transfer technique in order to conduct scientific observation as well as to demonstrate the low-energy orbit control technique via CubeSat.

After the mission was officially selected by NASA in 2016 spring-summer, as a system manager, I led a small team consisting of master/undergrad students for the preliminary mission design and analysis. Given the CubeSat’s limited capability and high-level mission objectives, we searched an “optimal” solution to “what the spacecraft system should be like?”.

The first cis-lunar exploration CubeSat EQUULEUS. © The Univ. of Tokyo & JAXA

The First Deep-Space Micro Spacecraft PROCYON
(UTokyo & ISAS/JAXA, 2014-2017) PI: Prof. R. Funase & Prof. Y. Kawakatsu

The first deep-space micro spacecraft PROCYON. © The Univ. of Tokyo & JAXA

Funded by ISAS/JAXA.

TBW

Group award:

  • Japanese government MEXT Commendation for Science and Technology “Prize for Science and Technology (Research Category)” (2017).
  • The University of Tokyo President’s Award for Students (2015).

-Acknowledgment-

Funding

2017-present

  • Graduate research assistantship, Department of Aerospace Engineering Sciences, CU Boulder
  • Masason foundation fellowship, from Masason foundation, Japan. (tuition, monthly stipend, and research grant as needed for five years; selection ratio ∼8.7%)

2017-2019

  • Scholarship for study abroad, Nakajima Foundation, Japan. (tuition cover and monthly stipend for 2 years, selection ratio: ∼14%)

2017

  • Departmental fellowship, Department of Aerospace Engineering Sciences, CU Boulder
  • Tuition fee half exemption for outstanding students, the University of Tokyo, Japan
  • JSPS DC1 research fellowship for young scientists, Japan Society for the Promotion of Science (JSPS), Japan (monthly stipend and research grant for 3 years, selection ratio: ∼20%)

2015-2016

  • Japanese Government MEXT Scholarship, the Ministry of Education, Culture, Sports, Science, and Technology (MEXT), Japan (monthly stipend)

2016

  • Support for international technological interaction, Tokyo Electric Power Company Holdings (TEPCO) Memorial Foundation, Japan
  • Grant for short overseas research, Murata Foundation, Japan
  • Short-term international travel support, Ministry of Education, Culture, Sports, Science, and Technology (MEXT), Japan

If you can dream it, you can do it.
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