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Kenta Oshima
Kenta Oshima
Hiroshima Institute of Technology
在 cc.it-hiroshima.ac.jp 的电子邮件经过验证
标题
引用次数
引用次数
年份
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
732020
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
452019
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
402019
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
282015
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
272019
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
262017
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
232017
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
192017
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
182017
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
162019
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
142014
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
132022
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
102018
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
102017
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
102017
Regularizing fuel-optimal multi-impulse trajectories
K Oshima
Astrodynamics 8 (1), 97-119, 2024
82024
Capture and escape analyses on planar retrograde periodic orbit around the Earth
K Oshima
Advances in Space Research 68 (9), 3891-3902, 2021
82021
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
62023
Continuation and stationkeeping analyses on planar retrograde periodic orbits around the Earth
K Oshima
Advances in Space Research 69 (5), 2210-2222, 2022
52022
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
52019
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