SLIM Project Team
Profile Information
- Affiliation
- Associate Professor, Institute of Space and Astronautical Science, Japan Aerospace Exploration AgencyAssociate Professor, Space and Astronautical Science, Department of Advanced Studies, The Graduate University for Advanced Studies, SOKENDAI
- Degree
- 博士(工学)(東京大学)
- Researcher number
- 90836222
- ORCID ID
https://orcid.org/0000-0002-8445-1575- J-GLOBAL ID
- 201801006720467786
- Researcher ID
- GXH-5604-2022
- researchmap Member ID
- B000312477
Research Interests
10Research History
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Apr, 2023 - Present
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Mar, 2019 - Mar, 2023
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Apr, 2018 - Feb, 2019
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Oct, 2016 - Dec, 2016
Education
3-
Apr, 2015 - Mar, 2018
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Apr, 2013 - Mar, 2015
Major Awards
7Major Papers
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8th IAA Planetary Defense Conference, Apr, 2023 Lead authorCorresponding author
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Acta Astronautica, 196 42-56, Jul, 2022 Peer-reviewedLead authorCorresponding author
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The Journal of the Astronautical Sciences, Feb 4, 2022 Peer-reviewedLead authorCorresponding author
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Journal of Guidance, Control, and Dynamics, 2022 Peer-reviewedLead authorCorresponding author
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Journal of Guidance, Control, and Dynamics, 43(4) 645-655, Mar, 2020 Peer-reviewedLead authorCorresponding authorRecent low-thrust space missions have highlighted the importance of designing trajectories that are robust against uncertainties. In its complete form, this process is formulated as a nonlinear constrained stochastic optimal control problem. This problem is among the most complex in control theory, and no practically applicable method to low-thrust trajectory optimization problems has been proposed to date. This paper presents a new algorithm to solve stochastic optimal control problems with nonlinear systems and constraints. The proposed algorithm uses the unscented transform to convert a stochastic optimal control problem into a deterministic problem, which is then solved by trajectory optimization methods such as differential dynamic programming. Two numerical examples, one of which applies the proposed method to low-thrust trajectory design, illustrate that it automatically introduces margins that improve robustness. Finally, Monte Carlo simulations are used to evaluate the robustness and optimality of the solution.
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Journal of Spacecraft and Rockets, 1 PartF, 2020 Peer-reviewedLead author
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JOURNAL OF THE ASTRONAUTICAL SCIENCES, 67(3) 950-976, Jan, 2020 Peer-reviewed
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IEEE Aerospace & Electro. Systems Magazine, Nov, 2019 Peer-reviewed
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IEEE AEROSPACE AND ELECTRONIC SYSTEMS MAGAZINE, 34(4) 38-44, Apr, 2019 Peer-reviewed
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JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 41(2) 377-387, Feb, 2018 Peer-reviewed
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 65(6) 219-226, 2017 Peer-reviewedEarth observation satellites can improve the flexibility of observation sites by having “maneuverability,” and low-thrust obtained by ion thruster will be a promising method for orbital change for micro-satellites. Designing low-thrust trajectories for these satellites is a multi-revolution and multi-objective (time/fuel-optimal) optimization problem, which usually requires high computational cost to solve numerically. This paper derives an analytical and approximate optimal orbit change strategy between two circular orbits with the same semi-major axis and different local time of ascending node, and proposes a graph-based method to optimize the multi-objective criteria. The optimal control problem results in a problem to search a switching point on the proposed graph, and mission designers can design an approximate switching point on this graph, by using two heuristic and reasonable assumptions that 1) the optimal thrust direction should be tangential to orbit and 2) the optimal thrust magnitude should be bang-bang control with an intermediate coast. Finally, numerical simulation with feedback control algorithm taking thrust margin demonstrates that the proposed method can be applicable in the presence of deterministic and stochastic fluctuation of aerodynamic disturbances.
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SICE Journal of Control, Measurement, and System Integration, 10(3) 192-197, 2017 Peer-reviewed
Misc.
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Apr 2, 2025DESTINY+ is an upcoming JAXA Epsilon medium-class mission to flyby multiple asteroids including Phaethon. As an asteroid flyby observation instrument, a telescope mechanically capable of single-axis rotation, named TCAP, is mounted on the spacecraft to track and observe the target asteroids during flyby. As in past flyby missions utilizing rotating telescopes, TCAP is also used as a navigation camera for autonomous optical navigation during the closest-approach phase. To mitigate the degradation of the navigation accuracy, past missions performed calibration of the navigation camera's alignment before starting optical navigation. However, such calibration requires significant operational time to complete and imposes constraints on the operation sequence. From the above background, the DESTINY+ team has studied the possibility of reducing operational costs by allowing TCAP alignment errors to remain. This paper describes an autonomous optical navigation algorithm robust to the misalignment of rotating telescopes, proposed in this context. In the proposed method, the misalignment of the telescope is estimated simultaneously with the spacecraft's orbit relative to the flyby target. To deal with the nonlinearity between the misalignment and the observation value, the proposed method utilizes the unscented Kalman filter, instead of the extended Kalman filter widely used in past studies. The proposed method was evaluated with numerical simulations on a PC and with hardware-in-the-loop simulation, taking the Phaethon flyby in the DESTINY+ mission as an example. The validation results suggest that the proposed method can mitigate the misalignment-induced degradation of the optical navigation accuracy with reasonable computational costs suited for onboard computers.
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AAS/AIAA Space Flight Mechanics Meeting, Jan, 2025
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AAS/AIAA Space Flight Mechanics Meeting, Jan, 2025 Last author
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AAS/AIAA Space Flight Mechanics Meeting, Jan, 2025 Last author
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AAS/AIAA Space Flight Mechanics Meeting, Jan, 2025 Last author
Professional Memberships
2Major Works
4Major Research Projects
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学術変革領域研究(B), 日本学術振興会, Oct, 2020 - Mar, 2023
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Grants-in-Aid for Scientific Research Grant-in-Aid for Early-Career Scientists, Japan Society for the Promotion of Science, Apr, 2019 - Mar, 2023
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Adaptable Seamless Technology Transfer Program through Target-driven R&D, Japan Science and Technology Agency, Oct, 2020 - Mar, 2022