PUBLICATION

 

Peer-reviewed journal publications

  1. K. Oguri, K. Kakihara, S. Campagnola, K. Oshima, N. Ozaki, R. Funase, EQUULEUS Mission Analysis: Design of the Science Orbit Phase, Acta Astronautica, submitted.
  2. K. Oshima, S. Campagnola, C. H. Yam, Y. Kayama, Y. Kawakatsu, N. Ozaki, Q. Vespieren, K. Kakihara, K. Oguri, R. Funase, EQUULEUS Mission Analysis: Design of the Transfer Phase, Acta Astronautica, submitted.
  3. 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

  1. 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
  2. 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
  3. 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
  4. 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
  5. 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)
  6. 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

  1. 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
  2. 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
  3. 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
  4. 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
  5. 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
  6. 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
  7. T. Ito, S. Ikari, 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)
  8. 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

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– Isaac Newton