Publications

See Google Scholar for complete and current information

Journal Articles

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

Under review

  • K. Oguri and G. Lantoine. Lossless Control-Affine Formulation for Solar-Sail Trajectory Optimization via Sequential Convex Programming. under review

Published / Accepted

  1. Y. Sidhoum and K. Oguri. Indirect Forward-Backward Shooting for Low-thrust Trajectory Optimization in Complex Dynamics. Journal of Guidance, Control, and Dynamics, in press
  2. N. Kumagai and K. Oguri. Adaptive-Mesh Sequential Convex Programming for Space Trajectory Optimization. Journal of Guidance, Control, and Dynamics, in press
  3. O. F. Awad, M. R. Stoeckle, and K. Oguri. An Autonomous Planetary Navigation System Independent of GNSS and Ground Station Tracking, The Journal of the Astronautical Sciences, 2024, doi: 10.1007/s40295-023-00397-5
  4. Y. Sidhoum and K. Oguri. On the Performance of Different Smoothing Methods for Indirect Low-Thrust Trajectory Optimization, The Journal of the Astronautical Sciences, 2023. doi: 10.1007/s40295-023-00417-4.
  5. D. C. Qi and K. Oguri. Analysis of Autonomous Orbit Determination in Various Near-Moon Periodic Orbits, The Journal of the Astronautical Sciences, 2023. doi: 10. 1007/s40295-023-00415-6
  6. 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. 
  7. 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, doi: 10.2514/1.G007103
  8. 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
  9. 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
  10. 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
  11. 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
  12. 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.
  13. 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.
  14. 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.
  15. 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)
  16. 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.
  17. 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. Kumagai and K. Oguri. Chance-Constrained Gaussian Mixture Steering to a Terminal Gaussian Distribution, under review (arXiv: https://arxiv.org/abs/2403.16302)

Published / Accepted

  1. A. A. Anibha and K. Oguri. Autonomous Horizon-based Asteroid Navigation with Observability Enhancing Maneuvers. In 4th Space Imaging Workshop, Atlanta, GA, 2024
  2. Y. Sidhoum and K. Oguri. Robust Low-thrust Trajectory Correction Planning under Uncertainty: Primer Vector Theory Approach, In AAS/AIAA Astrodynamics Specialist Conference, Broomfield, CO, 2024
  3. N. Kumagai and K. Oguri. Sequential Chance-Constrained Covariance Steering for Robust Cislunar Trajectory Design under Uncertainties, In AAS/AIAA Astrodynamics Specialist Conference, Broomfield, CO, 2024
  4. M. A. P. Ra and K. Oguri. Chance-Constrained Sensing-Optimal Path Planning for Safe Angles-only Autonomous Navigation, In AAS/AIAA Astrodynamics Specialist Conference, Broomfield, CO, 2024
  5. A. Liao and K. Oguri. Shape Model-Independent Autonomous Asteroid Navigation: Analysis on Observability and Feasibility, In AAS/AIAA Astrodynamics Specialist Conference, Broomfield, CO, 2024
  6. A. K. Alkhenani, K. Oguri, and M. J. Mueterthies. Optimal Trajectories of Electrodynamic Tethers in the Jovian System using Indirect Method, In AAS/AIAA Astrodynamics Specialist Conference, Broomfield, CO, 2024
  7. P. Lealiiee Jr, N. Kumagai, M. Akella, and K. Oguri. Learning-aided Chance-Constrained Control: Safety-assured Control & Learning for Spacecraft Mission Uncertainties, In AAS/AIAA Astrodynamics Specialist Conference, Broomfield, CO, 2024
  8. H. Sekine, Y. Kawabata, K. Oguri, and R.Funase. Guidance and Control of Formation Flying Reconfiguration Considering Collision Avoidance in the CRTBP, In AAS/AIAA Astrodynamics Specialist Conference, Broomfield, CO, 2024
  9. K. Oguri. Regularization of the Circular Restricted Three-body Problem for Trajectory Optimization, In AAS/AIAA Astrodynamics Specialist Conference, Broomfield, CO, 2024
  10. K. Oguri. Chance-Constrained Control for Safe Spacecraft Autonomy: Convex Programming Approach. In IEEE American Control Conference (ACC), to appear, Toronto, ON, Canada, 2024 (arXiv: https://arxiv.org/abs/2403.04062)
  11. R. Mishra, K. Oguri, T. Griffith, and A. Sizemore. Path Planning for Single-Agent and Multi-Agent Satellite Inspection Problem: Low Thrust Formulation. In AAS Guidance, Navigation, and Control Conference, Breckenridge, CO, 2024. (Student Paper Competition 2nd Place)
  12. O. F. Awad, M. R. Stoeckle, and K. Oguri. Autonomous Cislunar Orbit Determination via Two-Satellite Formation using Relative Position Measurements Only. In AAS Guidance, Navigation, and Control Conference, Breckenridge, CO, 2024
  13. E. M. Jarrett-Izzi, K. Oguri, M. Carpenter, and J. Danis. Investigation on Moon-based Sensor Placement for Cislunar Orbit Determination with Exclusion Zones. In AAS Guidance, Navigation, and Control Conference, Breckenridge, CO, 2024.
  16. N. Kumagai and K. Oguri. Adaptive-Mesh Sequential Convex Programming for Space Trajectory Optimization. In AAS/AIAA Astrodynamics Specialist Conference, 2023
  17. Y. Sidhoum and K. Oguri. Low-thrust Trajectory Optimization for Enceladus Exploration Using Indirect Forward-Backward Shooting. In AAS/AIAA Astrodynamics Specialist Conference, 2023 (John V. Breakwell student award)
  18. S. Shrivastava, K. Oguri. Fault-Tolerant Feedback Control for Spacecraft Rendezvous using Markov Jump Model. In AAS/AIAA Astrodynamics Specialist Conference, 2023
  19. 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
  20. N. Kumagai and K. Oguri. Robust NRHO Station-keeping Planning with Maneuver Location Optimization under Operational Uncertainties. In AAS/AIAA Astrodynamics Specialist Conference, 2023
  21. 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
  22. 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
  23. 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
  24. 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
  25. 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
  26. K. Oguri and G. Lantoine. Stochastic Sequential Convex Programming for Robust Low-thrust Trajectory Design under Uncertainty. In AAS/AIAA Astrodynamics Specialist Conference, 2022
  27. 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
  28. 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
  29. 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
  30. 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)
  31. 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
  32. 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
  33. 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
  34. 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
  35. 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)
  36. 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,
  37. 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)
  38. 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
  39. 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
  40. 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
  41. 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
  42. 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
  43. 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
  44. 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
  45. 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
  46. 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
  47. 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
  48. 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)
  49. 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
  50. 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
  51. 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)
  52. 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

Theses

  1. R. Mishra. Multi-Agent Path Planning for On-Orbit Servicing Applications. MS thesis, School of Aeronautics and Astronautics, Purdue University, May 2024
  2. E. Jarrett-Izzi. Moon-Based Non-Gaussian Multi-Object Tracking for Cislunar Space Domain Awareness. MS thesis, School of Aeronautics and Astronautics, Purdue University, May 2024
  3. D. Qi, Autonomous Guidance and Navigation for Rendezvous under Uncertainty in Cislunar Space, M.S. Thesis, School of Aeronautics and Astronautics, Purdue University, Dec 2023
  4. O. Awad, An Autonomous Small Satellite Navigation System for Earth, Cislunar Space, and Beyond, Ph.D. Thesis, School of Aeronautics and Astronautics, Purdue University, May 2023
  5. K. Oguri, Risk-aware Mission Design around Small Celestial Bodies, Ph.D. Thesis, Department of Aerospace Engineering Sciences, University of Colorado Boulder, May 2021