Ozaki, Naoya
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1

PROCYON Mission Reanalysis: Low-Thrust Asteroid Flyby Traje..:

Ozaki, Naoya ; Oguri, Kenshiro ; Funase, Ryu
The Journal of the Astronautical Sciences.  69 (2022)  1 - p. 1-27 , 2022
 
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Asteroid Flyby Cycler Trajectory Design Using Deep Neural N..:

Ozaki, Naoya ; Yanagida, Kanta ; Chikazawa, Takuya...
Journal of Guidance, Control, and Dynamics.  45 (2022)  8 - p. 1496-1511 , 2022
 
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Modelling internal structure of differentiated asteroids vi..:

Liang, Yuying ; Ozaki, Naoya ; Kawakatsu, Yasuhiro.
Monthly Notices of the Royal Astronomical Society.  519 (2022)  2 - p. 2349-2365 , 2022
 
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EQUULEUS Trajectory Design:

Oguri, Kenshiro ; Oshima, Kenta ; Campagnola, Stefano...
The Journal of the Astronautical Sciences.  67 (2020)  3 - p. 950-976 , 2020
 
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Extended Robust Planetary Orbit Insertion Method Under Prob..:

Ozaki, Naoya ; Chikazawa, Takuya ; Kakihara, Kota..
Journal of Spacecraft and Rockets.  57 (2020)  6 - p. 1153-1164 , 2020
 
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Mission Analysis for the EM-1 CubeSats EQUULEUS and OMOTENA..:

Campagnola, Stefano ; Hernando-Ayuso, Javier ; Kakihara, Kota...
IEEE Aerospace and Electronic Systems Magazine.  34 (2019)  4 - p. 38-44 , 2019
 
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