Mission to Earth-Moon Lagrange Point by a 6U CubeSat: EQUULEUS R Funase, N Ozaki, S Nakajima, K Oguri, K Miyoshi, S Campagnola, ... 8th Nano-Satellite Symposium,(Ehime, Japan), 2017 | 15 | 2017 |

EQUULEUS mission analysis: Design of the science orbit phase K Oguri, K Kakihara, S Campagnola, N Ozaki, K Oshima, T Yamaguchi, ... 26th International Symposium on Space Flight Dynamics, 1-7, 2017 | 14 | 2017 |

Attitude Determination and Control System for the PROCYON Micro-Spacecraft S Ikari, T Inamori, T Ito, K Ariu, K Oguri, M Fujimoto, S Sakai, Y Kawakatsu, ... TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 60 (3 …, 2017 | 12 | 2017 |

Mission analysis for the EM-1 CubeSats EQUULEUS and OMOTENASHI S Campagnola, J Hernando-Ayuso, K Kakihara, Y Kawabata, ... IEEE AES Mag. 34 (4), 38-44, 2019 | 8 | 2019 |

Mission Analysis for EQUULEUS, JAXA’s Earth-Moon Libration Orbit Cubesat S Campagnola, N Ozaki, K Oguri, Q Verspieren, K Kakihara, K Yanagida, ... 67th International Astronautical Congress, 2016 | 8 | 2016 |

EQUULEUS mission analysis: Design of the transfer phase K Oshima, S Campagnola, CH Yam, Y Kayama, Y Kawakatsu, N Ozaki, ... International Symposium on Space Technology and Science, ISTS-2017-d-159 …, 2017 | 7 | 2017 |

Mission Analysis for EQUULEUS and OMOTENASHI S Campagnola, N Ozaki, J Hernando-Ayuso, K Oshima, T Yamaguchi, ... 31th International Symposium on Space Technology and Science, Ehime, Japan, 2017 | 7 | 2017 |

EQUULEUS Trajectory Design K Oguri, K Oshima, S Campagnola, K Kakihara, N Ozaki, N Baresi, ... The Journal of the Astronautical Sciences, 1-27, 2020 | 5 | 2020 |

Convex Optimization over Sequential Linear Feedback Policies with Continuous-time Chance Constraints K Oguri, M Ono, JW McMahon 2019 IEEE 58th Conference on Decision and Control (CDC), 6325-6331, 2019 | 5 | 2019 |

Area-of-Effect Softbots (AoES) for Asteroid Proximity Operations J McMahon, SK Mitchell, K Oguri, N Kellaris, D Kuettel, C Keplinger, ... 2019 IEEE Aerospace Conference, 1-16, 2019 | 5 | 2019 |

SRP-based orbit control with application to small body landing K Oguri, JW McMahon AAS/AIAA Astrodynamics Specialist Conference, 1-19, 2018 | 4 | 2018 |

Risk-aware Trajectory Design with Continuous Thrust: Primer Vector Theory Approach K Oguri, JW McMahon AAS/AIAA Astrodynamics Specialist Conference, Portland, ME, 2019 | 3 | 2019 |

Risk-aware Trajectory Design with Impulsive Maneuvers: Convex Optimization Approach K Oguri, JW McMahon AAS/AIAA Astrodynamics Specialist Conference, Portland, ME, 2019 | 3 | 2019 |

Design Criteria of Reflectivity Control System Under Uncertainty in Sail Property for Maneuverability Requirement of Spinning Solar Sail K Oguri, T Kudo, R Funase AIAA/AAS Astrodynamics Specialist Conference, 5674, 2016 | 3 | 2016 |

Time-Optimal Attitude Control Law with a Strategy of Applying to Orbital Control for Spinning Solar Sail Driven by Reflectivity Control K Oguri, R Funase Advances in the Astronautical Sciences 158, 933-951, 2016 | 2 | 2016 |

Reliable and robust implementation of attitude determination and control subsystem and initial flight operation results of 50-kg-class interplanetary spacecraft PROCYON T Ito, S Ikari, T Nakatani, M Fujimoto, K Ariu, K Oguri, T Inamori, R Funase, ... International Symposium on Space Flight Dynamics (ISSFD) 2015, 2015 | 2 | 2015 |

SRP-Based Orbit Control with Application to Orbit Stationkeeping at Small Bodies K Oguri, JW McMahon Advances in the Astronautical Sciences 168 (2), 2077-2093, 2019 | 1 | 2019 |

EQUULEUS: Mission to Earth-Moon Lagrange Point by a 6U Deep Space CubeSat S Ikari, N Ozaki, S Nakajima, K Oguri, K Miyoshi, S Campagnola, ... | 1 | 2017 |

Science orbit design with a quasi-frozen beta angle: effects of body obliquity on J2-perturbed dynamics K Oguri, G Lantoine, W Hart, J McMahon Celestial Mechanics and Dynamical Astronomy 132 (10), 1-33, 2020 | | 2020 |

Solar Radiation Pressure–Based Orbit Control with Application to Small-Body Landing K Oguri, JW McMahon Journal of Guidance, Control, and Dynamics 43 (2), 195-211, 2020 | | 2020 |