### Peer-Reviewed Journal Publications

**K. Oguri**, J. W. McMahon, Solar Radiation Pressure based Orbit Control with Application to Small Body Landing. Journal of Guidance, Control, and Dynamics, under review.**K. Oguri**, K. Oshima, S. Campagnola, K. Kakihara, N. Ozaki, N. Baresi, Y. Kawakatsu, R. Funase, EQUULEUS Trajectory Design, The Journal of the Astronautical Sciences, under review.- S. Campagnola, J. Hernando-ayuso, K. Kakihara, Y. Kawabata, T. Chikazawa, R. Funase, N. Ozaki, N. Baresi, T. Hashimoto, Y. Kawakatsu, T. Ikenaga,
**K. Oguri**, and K. Oshima. Mission Analysis for the EM-1 CubeSats EQUULEUS and OMOTENASHI. IEEE Aerospace and Electronic Systems Magazine, 34(10):38–44, 2019 - S. Ikari, T. Inamori, T. Ito, K. Ariu,
**K. Oguri**, et.al, Attitude Determination and Control System for the Micro Spacecraft PROCYON, Transactions of the Japan Society for Aeronautical and Space Sciences.

### Conference Proceedings (selected)

#### First author

**K. Oguri**, M. Ono, and J. W. McMahon. Convex Optimization over Sequential Linear Feedback Policies with Continuous-time Chance Constraints. In 2019 IEEE Conference on Decision and Control, accepted, Nice, France, 2019**K. Oguri**and J. W. McMahon. Risk-aware Trajectory Design with Continuous Thrust: Primer Vector Theory Approach. In AAS/AIAA Astrodynamics Specialist Conference, Portland, ME, 2019**K. Oguri**and J. W. McMahon. Risk-aware Trajectory Design with Impulsive Maneuvers: Convex Optimization Approach. In AAS/AIAA Astrodynamics Specialist Conference, Portland, ME, 2019**K. Oguri**and J. W. McMahon. SRP-based Orbit Control for Asteroid Exploration. In 32nd International Symposium on Space Technology and Science, Fukui, Japan, 2019**K. Oguri**, G. Lantoine, B. Hart, and J. W. Mcmahon. Science Orbit Design with Frozen Beta angle: Theory and Application to Psyche mission. In AAS/AIAA Space Flight Mechanics Meeting, pages 1–15, Ka’anapali, HI, 2019.**(Bahls Endowed Funds Travel Award)****K. Oguri**and J. W. McMahon. SRP-based Orbit Control with Application to Orbit Stationkeeping at Small Bodies. In AAS/AIAA Space Flight Mechanics Meeting, pages 1–17, Ka’anapali, HI, 2019,**K. Oguri**and J. W. McMahon. SRP-based Orbit Control with Application to Small Body Landing. In AAS/AIAA Astrodynamics Specialist Conference, pages 1–19, Snowbird, UT, 2018.**(John V. Breakwell student award)****K. Oguri**, K. Kakihara, S. Campagnola, N. Ozaki, K. Oshima, T. Yamaguchi, and R. Funase. EQUULEUS Mission Analysis: Design of the Science Orbit Phase. In 26th International Symposium on Space Flight Dynamics, Ehime, Japan, 2017**K. Oguri**, A. Ishikawa, S. Ikari, T. Kudo, and R. Funase. Precision Evaluation of Reduced Dynamics Model for Non-uniform Spinning Solar Sail Driven by Reflectivity Control. In 4th International Symposium on Solar Sailing, 17045, Kyoto, Japan, 2017**K. Oguri**, T. Kudo, and R. Funase. Design Criteria of Reflectivity Control System Under Uncertainty in Sail Property for Maneuverability Requirement of Spinning Solar Sail. In AIAA/AAS Astrodynamics Specialist Conference, AIAA2016-5674, Long beach, CA, 2016**K. Oguri**and R. Funase. Time-optimal Attitude Control Law with a Strategy of Applying to Orbital Control for Spinning Solar Sail Driven by Reflectivity Control. Advances in the Astronautical Sciences (also paper of 26th AAS/AIAA Space Flight Mechanics Meetings, AAS 16-329), 158:933–951, 2016**K. Oguri**, T. Kudo, and R. Funase. Time-Optimal Attitude Control and its Application to Orbital Control of Spinning Solar Sail Driven by Reflectivity Control. In 60th Space Sciences and Technology Conference, 2016-P34, Hokkaido, Japan, 2016**(Outstanding Student Presentation Award)****K. Oguri**, T. Furumoto, and R. Funase. Optimal Attitude Control of Spinning Solar Sail with Reflectivity Control. In 30th International Symposium on Space Technology and Science, 2015-d-26, Kobe, Japan, 2015

#### Co-author

- S. Campagnola, J. Hernando-ayuso, N. Ozaki, N. Baresi, T. Hashimoto, Y. Kawakatsu, K. Kakihara, Y. Kawabata, T. Chikazawa, R. Funase, T. Ikenaga,
**K. Oguri**, and K. Oshima. Mission analysis for the EM-1 CubeSats EQUULEUS and OMOTENASHI. In International Astronautical Congress, volume 1, pages 1–7, Bremen, 2018 - S. Campagnola, N. Ozaki, J. Hernando-ayuso, K. Oshima, T. Yamaguchi,
**K. Oguri**, Y. Ozawa, T. Ikenaga, K. Kakihara, S. Taka- hashi, R. Funase, Y. Kawakatsu, and T. Hashimoto. Mission Analysis for EQUULEUS and OMOTENASHI. In 31st International Symposium on Space Technology and Science, pages 1–5, 2017 - R. Funase, N. Ozaki, S. Nakajima,
**K. Oguri**, K. Miyoshi, S. Campagnola, H. Koizumi, Y. Kobayashi, T. Ito, T. Kudo, Y. Koshiro, and S. Nomura. Mission to Earth―Moon Lagrange Point by a 6U CubeSat : EQUULEUS. In 31st International Symposium on Space Technology and Science, pages 4–7, 2017 - A. Ishikawa,
**K. Oguri**, S. Ikari, R. Funase, and S. Nakasuka. Estimation of Shape and Optical Parameters of Spinning Solar Sail Equipped with Reflectivity Control Devices. In 26th International Symposium on Space Flight Dynamics, pages 1–6, 2017 - K. Oshima, S. Campagnola, C. H. Yam, Y. Kayama, Y. Kawakatsu, N. Ozaki, Q. Verspieren, K. Kakihara,
**K. Oguri**, and R. Funase. EQUULEUS Mission Analysis: Design of the Transfer Phase. In 26th International Symposium on Space Flight Dynamics, Ehime, Japan, 2017 - S. Nomura, R. Takahashi, M. Ikura,
**K. Oguri**, T. Obata, S. Ikari, and R. Funase. Initial Design of EQUULEUS Attitude Determination and Control System : How to Design an ADCS with High Reliability for a Deep Space CubeSat. In 31st International Symposium on Space Technology and Science, pages 1–6, 2017 - S. Campagnola, N. Ozaki,
**K. Oguri**, Q. Verspieren, K. Kakihara, K. Yanagida, R. Funase, H. C. Yam, L. Ferella, T. Yamaguchi, Y. Kawakatsu, and G. D. Yarnoz. Mission Analysis for EQUULEUS , JAXA’s Earth-Moon Libration Orbit Cubesat. In 67th International Astronautical Congress, IAC-16-B4.8.1, pages 1–10, Guadalajara, Mexico, 2016 - T. Ito, S. Ikari,
**K. Oguri**, M. Fujimoto, K. Ariu, Y. Kawabata, T. Inamori, S. Sakai, Y. Kawakatsu, and R. Funase. Preliminary Study of Angular Momentum Control by Solar Radiation Pressure for 50 kg-class Spacecraft PROCYON. In 59th Space Sciences and Technology Conference, 2015-3J08, pages 1–6, Kagoshima, Japan, 2015**(Young Researcher Award)** - T. Ito, S. Ikari, T. Nakatani, M. Fujimoto, K. Ariu,
**K. Oguri**, T. Inamori, S. Sakai, Y. Kawakatsu, and R. Funase. Reliable and Robust Implementation of Attitude Determination and Control Subsystem and Initial Flight Operation Results. In 25th International Symposium on Space Flight Dynamics ISSFD, number 1, pages 1–12, Munich, Germany, 2015

If I have seen further, it is by standing on the shoulders of giants.

– Isaac Newton