Publications

See Google Scholar for complete and current information

Journal Articles

*Dr. Oguri and his advisees are indicated in bold.

Under review

  1. Y. Sidhoum and K. Oguri. On the Performance of Different Smoothing Methods for Indirect Low-Thrust Trajectory Optimization.
  2. D. C. Qi and K. Oguri. Analysis of Autonomous Orbit Determination in Various Near-Moon Periodic Orbits.

Published / Accepted

  1. O. F. Awad, M. R. Stoeckle, and K. Oguri. An Autonomous Planetary Navigation System Independent of GNSS and Ground Station Tracking, in press
  2. K. Oguri and G. Lantoine. Indirect trajectory optimization via solar sailing primer vector theory: Minimum solar-angle transfers. Acta Astronautica, 211:405–415, Oct. 2023. doi: 10.1016/j.actaastro.2023.06.032. 
  3. K. Oguri, G. Lantoine, A. E. Petropoulos, and J. W. McMahon. Solar Sailing Q-law for Planetocentric, Many-Revolution Sail Orbit Transfers, Journal of Guidance, Control, and Dynamics, in press
  4. N. Ozaki, K. Oguri, and R. Funase. PROCYON Mission Reanalysis: Low-Thrust Asteroid Flyby Trajectory Design leveraging Convex Programming. The Journal of the Astronautical Sciences, Feb. 2022
  5. K. Oguri and J. W. McMahon. Stochastic Primer Vector for Robust Low-thrust Trajectory Design under Uncertainty. Journal of Guidance, Control, and Dynamics, Jan. 2022
  6. K. Oguri, G. Lantoine, and J. W. McMahon. Solar Sailing Primer Vector Theory: Indirect Trajectory Optimization with Practical Mission Considerations. Journal of Guidance, Control, and Dynamics, Jan. 2022
  7. K. Oguri and J. W. McMahon. Robust Spacecraft Guidance around Small Bodies under Uncertainty: Stochastic Optimal Control Approach. Journal of Guidance, Control, and Dynamics. July 2021
  8. K. Oguri, G. Lantoine, W. Hart, and J. McMahon. Science orbit design with a quasi-frozen beta angle: Effects of body obliquity on J2-perturbed dynamics. Celestial Mechanics and Dynamical Astronomy, Oct. 2020.
  9. K. Oguri, J. W. McMahon, Solar Radiation Pressure--Based Orbit Control with Application to Small-Body Landing. Journal of Guidance, Control, and Dynamics, 43(2):195-211, Feb. 2020.
  10. 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, Jan 2020.
  11. S.Ikari, T.Ito, K.Oguri, T.Inamori, S.Sakai, Y.Kawakatsu, A.Tomiki, and R.Funase. In Orbit Demonstration of a FDIR Algorithm for the Attitude Control System of Micro Interplanetary Spacecraft PROCYON. Journal of the Japan Society for Aeronautical and Space Sciences, 68 (2):89–95, 2020. (in Japanese)
  12. 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, Apr. 2019.
  13. 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, 2017.

Conference Proceedings

*Dr. Oguri and his advisees are indicated in bold.

Under review

  • N/A at the time

Published / Accepted

  1. K. Oguri. Successive Convexification with Feasibility Guarantee via Augmented Lagrangian for Non-Convex Optimal Control Problems. In IEEE Conference on Decision and Control (CDC), Accepted (Also in arXiv. http://arxiv.org/abs/2304.14564), 2023
  2. K. Oguri. Smooth Indirect Solution Method for State-constrained Optimal Control Problems with Nonlinear Control-affine Systems. In IEEE Conference on Decision and Control (CDC), Accepted (Also in arXiv. http://arxiv.org/abs/2304.14587), 2023
  3. N. Kumagai and K. Oguri. Adaptive-Mesh Sequential Convex Programming for Space Trajectory Optimization. In AAS/AIAA Astrodynamics Specialist Conference, 2023
  4. Y. Sidhoum and K. Oguri. Low-thrust Trajectory Optimization for Enceladus Exploration Using Indirect Forward-Backward Shooting. In AAS/AIAA Astrodynamics Specialist Conference, 2023
  5. S. Shrivastava, K. Oguri. Fault-Tolerant Feedback Control for Spacecraft Rendezvous using Markov Jump Model. In AAS/AIAA Astrodynamics Specialist Conference, 2023
  6. D. Aleti, K. Oguri, and N. Kumagai. Chance-Constrained Output-Feedback Control without History Feedback: Application to NRHO Stationkeeping. In AAS/AIAA Astrodynamics Specialist Conference, 2023
  7. N. Kumagai and K. Oguri. Robust NRHO Station-keeping Planning with Maneuver Location Optimization under Operational Uncertainties. In AAS/AIAA Astrodynamics Specialist Conference, 2023
  8. O. F. Awad, M. R. Stoeckle, and K. Oguri. Gravity Model Error Compensation for Accurate Earth Orbit Determination of Two Satellites using Relative Position Measurements Only. In AAS Guidance, Navigation, and Control conference, 2023
  9. Y. Sidhoum and K. Oguri. Indirect Forward-Backward Shooting for Low-thrust Trajectory Optimization in Complex Dynamics. In AAS/AIAA Space Flight Mechanics Meeting, 2023
  10. Y. Sidhoum and K. Oguri. On the Performance of Different Smoothing Methods for Indirect Low-thrust Trajectory Optimization. In AAS/AIAA Space Flight Mechanics Meeting, 2023
  11. D.C.Qi and K.Oguri. Investigation on Autonomous Orbit Determination in Cislunar Space via GNSS and Horizon-based Measurements. In AAS/AIAA Space Flight Mechanics Meeting, 2023
  12. T. Ishizuka, S. Lizy-Destrez, N. Ozaki, and K.Oguri. Robust Trajectory Optimization for Autonomous Asteroid Rendezvous. In 73rd International Astronautical Congress, Paris, France, 2022
  13. K. Oguri and G. Lantoine. Stochastic Sequential Convex Programming for Robust Low-thrust Trajectory Design under Uncertainty. In AAS/AIAA Astrodynamics Specialist Conference, 2022
  14. K. Oguri, G. Lantoine, and T. H. Sweetser. Robust Solar Sail Trajectory Design under Uncertainty with Application to NEA Scout Mission. In AIAA SCITECH 2022 Forum, Jan. doi:10.2514/6.2022-1627
  15. K. Oguri and J. W. McMahon. Risk-aware Mission Design for In situ Asteroid Exploration under Uncertainty. In IEEE Aerospace Conference, Big Sky, MT (Virtual), Mar. 2021
  16. K. Oguri and J. W. McMahon. Stochastic Primer Vector for Robust Impulsive Trajectory Design Under Uncertainty. In AAS/AIAA Astrodynamics Specialist Conference, South Lake Tahoe, CA (Virtual), Aug. 2020
  17. K. Oguri and J. W. McMahon. Autonomous Guidance for Robust Achievement of Science Observations around Small Bodies. In AAS Guidance, Navigation, and Control, Breckenridge, Colorado, 2020. (Student Paper Competition 2nd Place)
  18. 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, Nice, France, 2019
  19. 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
  20. 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
  21. 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
  22. 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)
  23. 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,
  24. 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)
  25. 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
  26. 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
  27. 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
  28. 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
  29. 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
  30. 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
  31. 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
  32. 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
  33. 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
  34. 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
  35. 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)
  36. 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
  37. 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
  38. 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)
  39. 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

Preprints

*Dr. Oguri and his advisees are indicated in bold.

Theses

  1. O. AwadAn Autonomous Small Satellite Navigation System for Earth, Cislunar Space, and Beyond, Ph.D. Thesis, School of Aeronautics and Astronautics, Purdue University, May 2023
  2. K. Oguri, Risk-aware Mission Design around Small Celestial Bodies, Ph.D. Thesis, Department of Aerospace Engineering Sciences, University of Colorado Boulder, May 2021