Zobrazeno 1 - 10
of 15
pro vyhledávání: '"Kenshiro OGURI"'
Publikováno v:
The Journal of the Astronautical Sciences. 69:1-27
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::54d555cff2fedc1374b32f2f95293230
https://doi.org/10.1007/s40295-021-00299-4
https://doi.org/10.1007/s40295-021-00299-4
Publikováno v:
Journal of Guidance, Control, and Dynamics. 45:153-161
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4fe765863e77d3560dc4a21e5b49cddc
https://doi.org/10.2514/1.g006210
https://doi.org/10.2514/1.g006210
Autor:
Jay W. McMahon, Kenshiro Oguri
Publikováno v:
Journal of Guidance, Control, and Dynamics. 45:84-102
Any space trajectories are subject to state uncertainty due to imperfect state knowledge, random disturbances, and partially known dynamical environments. Ideally, such uncertainty and associated r...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cf8ccc457f49f7bea42b4253bedf6846
https://doi.org/10.2514/1.g005970
https://doi.org/10.2514/1.g005970
Autor:
Jay W. McMahon, Kenshiro Oguri
Publikováno v:
Journal of Guidance, Control, and Dynamics. 44:1295-1313
Dynamical environments around small celestial bodies are complex and uncertain, leading to highly perturbed, uncertain orbital motions in their proximity. Under such complexity and uncertainty, mis...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b95f22b3eaf0f892c3ca6d163deb3fc6
https://doi.org/10.2514/1.g005426
https://doi.org/10.2514/1.g005426
Autor:
Jay W. McMahon, Kenshiro Oguri
Publikováno v:
Journal of Guidance, Control, and Dynamics. 43:195-211
With appropriate control algorithms, solar radiation pressure (SRP) can be effectively used for orbit control around small celestial bodies. In contrast to the historical treatment of SRP as a dist...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a397dc72cd68c77ab9599bcdb8f618ce
https://doi.org/10.2514/1.g004489
https://doi.org/10.2514/1.g004489
Autor:
Nicola Baresi, Stefano Campagnola, Ryu Funase, Kenta Oshima, Yasuhiro Kawakatsu, Kenshiro Oguri, Naoya Ozaki, Kota Kakihara
Publikováno v:
The Journal of the Astronautical Sciences. 67:950-976
This paper presents the trajectory design for EQUilibriUm Lunar-Earth point 6U Spacecraft (EQUULEUS), which aims to demonstrate orbit control capability of CubeSats in the cislunar space. The mission plans to observe the far side of the Moon from an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ffc37a67d6531e58bdde0a31707b9327
https://doi.org/10.1007/s40295-019-00206-y
https://doi.org/10.1007/s40295-019-00206-y
Autor:
Takaya Inamori, Atsushi Tomiki, Kenshiro Oguri, Takahiro Ito, Ryu Funase, Shin-ichiro Sakai, Yasuhiro Kawakatsu, Satoshi Ikari
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 68:89-95
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cb80c42c9a6ebd37739c25f289a55471
https://doi.org/10.2322/jjsass.68.89
https://doi.org/10.2322/jjsass.68.89
Publikováno v:
AIAA SCITECH 2022 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::24524ec9a74f06c655cd6d041d9df43b
https://doi.org/10.2514/6.2022-1627
https://doi.org/10.2514/6.2022-1627
Autor:
Kenshiro Oguri, Jay W. McMahon
Publikováno v:
2021 IEEE Aerospace Conference (50100).
In-situ robotic asteroid exploration is integral to current and future space programs for sustainable human exploration and resupply in deep space, deflection of potentially hazardous objects, and study of the early solar system formulation. Meanwhil
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c4ab66add70ebb3d46c2d36c1f43ea66
https://doi.org/10.1109/aero50100.2021.9438479
https://doi.org/10.1109/aero50100.2021.9438479
Publikováno v:
Celestial Mechanics and Dynamical Astronomy. 132
The beta angle, an angle formed by the sunlight and a spacecraft orbital plane, is an important parameter for science orbit design of orbiter missions. This angle defines lighting conditions and eclipse occurrences, and is used for science observatio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f86f3f73bfeb566cba0cb1525127cf86
https://doi.org/10.1007/s10569-020-09987-z
https://doi.org/10.1007/s10569-020-09987-z