Naoya Ozaki
Naoya Ozaki
Japan Aerospace Exploration Agency
No verified email
Title
Cited by
Cited by
Year
Initial operation results of a 50kg-class deep space exploration micro-spacecraft PROCYON
R Funase, T Inamori, S Ikari, N Ozaki, H Koizumi
282015
Low-thrust trajectory design and operations of PROCYON, the first deep-space micro-spacecraft
S Campagnola, N Ozaki, Y Sugimoto, CH Yam, H Chen, Y Kawabata, ...
25th International Symposium on Space Flight Dynamics 7, 2015
272015
One-year deep space flight result of the world's first full-scale 50kg-class deep space probe PROCYON and its future perspective
R Funase, T Inamori, S Ikari, N Ozaki, S Nakajima, H Koizumi, A Tomiki, ...
202016
Stochastic differential dynamic programming with unscented transform for low-thrust trajectory design
N Ozaki, S Campagnola, R Funase, CH Yam
Journal of Guidance, Control, and Dynamics 41 (2), 377-387, 2018
182018
Mission to Earth–Moon Lagrange point by a 6U CubeSat: EQUULEUS
R Funase, S Ikari, K Miyoshi, Y Kawabata, S Nakajima, S Nomura, ...
IEEE Aerospace and Electronic Systems Magazine 35 (3), 30-44, 2020
152020
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
142017
Differential dynamic programming approach for robust-optimal low-thrust trajectory design considering uncertainty
N Ozaki, S Campagnola, CH Yam, R Funase
25th International Symposium on Space Flight Dynamics, Munich, Germany, 19-23, 2015
122015
Mission Design of Martian Moons eXploration (MMX)
Y Kawakatsu, K Kuramoto, T Usui, H Ikeda, N Ozaki, N Baresi, G Ono, ...
69th International Astronautical Congress (IAC), 1-12, 2018
92018
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
82019
Flight Model Design and Development Status of the Earth-Moon Lagrange Point Exploration CubeSat EQUULEUS Onboard SLS EM-1
R Funase, S Ikari, Y Kawabata, S Nakajima, S Nomura, K Kakihara, ...
82018
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
82016
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
72017
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
72017
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
62020
Tube Stochastic Optimal Control for Nonlinear Constrained Trajectory Optimization Problems
N Ozaki, S Campagnola, R Funase
Journal of Guidance, Control, and Dynamics 43 (4), 645-655, 2020
62020
Preliminary mission design of PROCYON: A micro spacecraft to asteroid
N Ozaki, R Funase, S Nakajima, CH Yam, S Campagnola, B Sarli, ...
24th International Symposium on Space Flight Dynamics, 1-4, 2014
62014
Thermal Design and Analysis for a 6U Deep Space CubeSat EQUULEUS under Tightly-Coupled Spacecraft Resource Constraints
Y Koshiro, N Ozaki, S Matsushita, A Ishikawa, R Funase
Proceedings of the 31st International Symposium on Space Technology and Science, 2017
52017
Flyby navigation and guidance experiment for interplanetary micro-spacecraft PROCYON
N Ozaki, Y Kawabata, H Takeuchi, T Ichikawa, S Taniguchi, T Yagami, ...
2016 55th Annual Conference of the Society of Instrument and Control …, 2016
42016
Tube Stochastic Differential Dynamic Programming for Robust Low-Thrust Trajectory Optimization Problems
N Ozaki, R Funase
2018 AIAA Guidance, Navigation, and Control Conference, 0861, 2018
32018
GTOC8: results and methods of ESA advanced concepts team and JAXA-ISAS
D Izzo, D Hennes, M Märtens, I Getzner, K Nowak, A Heffernan, ...
arXiv preprint arXiv:1602.00849, 2016
32016
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