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 | 73 | 2020 |
Low-energy transfers to the Moon with long transfer time K Oshima, F Topputo, T Yanao Celestial Mechanics and Dynamical Astronomy 131, 1-19, 2019 | 45 | 2019 |
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 |
Jumping mechanisms of Trojan asteroids in the planar restricted three-and four-body problems K Oshima, T Yanao Celestial Mechanics and Dynamical Astronomy 122 (1), 53-74, 2015 | 28 | 2015 |
The use of vertical instability of and planar Lyapunov orbits for transfers from near rectilinear halo orbits to planar distant retrograde orbits in the Earth–Moon … K Oshima Celestial Mechanics and Dynamical Astronomy 131 (3), 14, 2019 | 27 | 2019 |
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 |
Global search for low-thrust transfers to the Moon in the planar circular restricted three-body problem K Oshima, S Campagnola, T Yanao Celestial Mechanics and Dynamical Astronomy 128, 303-322, 2017 | 23 | 2017 |
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 |
Analysis of medium-energy transfers to the Moon K Oshima, F Topputo, S Campagnola, T Yanao Celestial Mechanics and Dynamical Astronomy 127, 285-300, 2017 | 18 | 2017 |
Spatial unstable periodic quasi-satellite orbits and their applications to spacecraft trajectories K Oshima, T Yanao Celestial Mechanics and Dynamical Astronomy 131, 1-32, 2019 | 16 | 2019 |
Applications of gravity assists in the bicircular and bielliptic restricted four-body problem K Oshima, T Yanao 24th AAS/AIAA Space Flight Mechanics Meeting, 2014, 503-522, 2014 | 14 | 2014 |
Multiple families of synodic resonant periodic orbits in the bicircular restricted four–body problem K Oshima Advances in Space Research 70 (5), 1325-1335, 2022 | 13 | 2022 |
The roles of L4 and L5 axial orbits in transport among co-orbital orbits K Oshima Monthly Notices of the Royal Astronomical Society 480 (3), 2945-2952, 2018 | 10 | 2018 |
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 | 10 | 2017 |
Global search for low-energy transfers to the moon with long transfer time K Oshima, F Topputo, T Yanao 27th AAS/AIAA Space Flight Mechanics Meeting, AAS, 17-229, 2017 | 10 | 2017 |
Regularizing fuel-optimal multi-impulse trajectories K Oshima Astrodynamics 8 (1), 97-119, 2024 | 8 | 2024 |
Capture and escape analyses on planar retrograde periodic orbit around the Earth K Oshima Advances in Space Research 68 (9), 3891-3902, 2021 | 8 | 2021 |
Regularized direct method for low–thrust trajectory optimization: Minimum–fuel transfer between cislunar periodic orbits K Oshima Advances in Space Research 72 (6), 2051-2063, 2023 | 6 | 2023 |
Continuation and stationkeeping analyses on planar retrograde periodic orbits around the Earth K Oshima Advances in Space Research 69 (5), 2210-2222, 2022 | 5 | 2022 |
The role of vertical instability of Jupiter’s quasi-satellite orbits: making hazardous asteroids less detectable? K Oshima Monthly Notices of the Royal Astronomical Society 482 (4), 5441-5447, 2019 | 5 | 2019 |