| 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 | 88 | 2017 |
| EQUULEUS Trajectory Design K Oguri, K Oshima, S Campagnola, K Kakihara, N Ozaki, N Baresi, ... The Journal of the Astronautical Sciences 67 (3), 950-976, 2020 | 75 | 2020 |
| Robust Spacecraft Guidance Around Small Bodies Under Uncertainty: Stochastic Optimal Control Approach K Oguri, JW McMahon Journal of Guidance, Control, and Dynamics 44 (7), 1295-1313, 2021 | 56 | 2021 |
| Mission analysis for the EM-1 CubeSats EQUULEUS and OMOTENASHI S Campagnola, J Hernando-Ayuso, K Kakihara, Y Kawabata, ... IEEE Aerospace and Electronic Systems Magazine 34 (4), 38-44, 2019 | 40 | 2019 |
| 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 | 33 | 2019 |
| Stochastic Primer Vector for Robust Low-Thrust Trajectory Design Under Uncertainty K Oguri, JW McMahon Journal of Guidance, Control, and Dynamics 45 (1), 84-102, 2022 | 27 | 2022 |
| 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 | 26 | 2017 |
| Stochastic Sequential Convex Programming for Robust Low-thrust Trajectory Design under Uncertainty K Oguri, G Lantoine AAS/AIAA Astrodynamics Specialist Conference, 2022 | 25 | 2022 |
| 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 | 25 | 2017 |
| Risk-aware Trajectory Design with Impulsive Maneuvers: Convex Optimization Approach K Oguri, JW McMahon AAS/AIAA Astrodynamics Specialist Conference, Portland, Maine, 2019 | 24 | 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 | 20 | 2019 |
| Risk-aware Trajectory Design with Continuous Thrust: Primer Vector Theory Approach K Oguri, JW McMahon AAS/AIAA Astrodynamics Specialist Conference, Portland, Maine, 2019 | 19 | 2019 |
| 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 | 19 | 2017 |
| 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 | 16 | 2020 |
| Indirect Forward–Backward Shooting for Low-Thrust Trajectory Optimization in Complex Dynamics Y Sidhoum, K Oguri Journal of Guidance, Control, and Dynamics 47 (10), 2164-2172, 2024 | 15 | 2024 |
| Successive convexification with feasibility guarantee via augmented lagrangian for non-convex optimal control problems K Oguri 2023 62nd IEEE Conference on Decision and Control (CDC), 3296-3302, 2023 | 14 | 2023 |
| On the performance of different smoothing methods for indirect low-thrust trajectory optimization Y Sidhoum, K Oguri The Journal of the Astronautical Sciences 33, 2023 | 12 | 2023 |
| Robust Solar Sail Trajectory Design under Uncertainty with Application to NEA Scout Mission K Oguri, G Lantoine, TH Sweetser AIAA SCITECH 2022 Forum, 1627, 2022 | 12 | 2022 |
| 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 | 12 | 2016 |
| Solar Sailing Primer Vector Theory: Indirect Trajectory Optimization with Practical Mission Considerations K Oguri, G Lantoine, JW McMahon Journal of Guidance, Control, and Dynamics 45 (1), 153-161, 2022 | 11 | 2022 |
Jay McMahonUniversity of ColoradoE-mail confirmado em colorado.edu
