| 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 | 66 | 2020 |
| 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 | 63 | 2018 |
| 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 | 60 | 2020 |
| 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 | 52 | 2020 |
| 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 | 44 | 2015 |
| 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 | 37 | 2019 |
| Science operation plan of Phobos and Deimos from the MMX spacecraft T Nakamura, H Ikeda, T Kouyama, H Nakagawa, H Kusano, H Senshu, ... Earth, Planets and Space 73 (1), 227, 2021 | 35 | 2021 |
| Initial operation results of a 50kg-class deep space exploration micro-spacecraft PROCYON R Funase, T Inamori, S Ikari, N Ozaki, H Koizumi | 35 | 2015 |
| 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, ... | 33 | 2016 |
| Mission design of DESTINY+: Toward active asteroid (3200) Phaethon and multiple small bodies N Ozaki, T Yamamoto, F Gonzalez-Franquesa, R Gutierrez-Ramon, ... Acta Astronautica 196, 42-56, 2022 | 32 | 2022 |
| 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-18-A3. A 3, 2018 | 24 | 2018 |
| EQUULEUS mission analysys: 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 | 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 | 18 | 2017 |
| 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 | 15 | 2015 |
| 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 |
| Asteroid flyby cycler trajectory design using deep neural networks N Ozaki, K Yanagida, T Chikazawa, N Pushparaj, N Takeishi, R Hyodo Journal of Guidance, Control, and Dynamics 45 (8), 1496-1511, 2022 | 10 | 2022 |
| 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, ... | 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 |
| 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 | 9 | 2016 |
| Procyon mission reanalysis: Low-thrust asteroid flyby trajectory design leveraging convex programming N Ozaki, K Oguri, R Funase The Journal of the Astronautical Sciences 69 (1), 1-27, 2022 | 8 | 2022 |
Stefano CampagnolaResearcher at JAXAVerified email at missionanalysis.org
