Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Costantinos Zagaris"'
Publikováno v:
2023 IEEE Aerospace Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5e8fb033a1e968f5f65c828d72bc8072
https://doi.org/10.1109/aero55745.2023.10115819
https://doi.org/10.1109/aero55745.2023.10115819
Publikováno v:
2023 IEEE Aerospace Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3728f724a5e8694942c7403282fe4fcd
https://doi.org/10.1109/aero55745.2023.10115983
https://doi.org/10.1109/aero55745.2023.10115983
Autor:
Costantinos Zagaris, Marcello Romano
Publikováno v:
Journal of Guidance, Control, and Dynamics. 41:1416-1422
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c500c233b93dc44e613d6f15d1a1ca6d
https://doi.org/10.2514/1.g003389
https://doi.org/10.2514/1.g003389
Autor:
Andrew Bradstreet, Richard Zappulla, Josep Virgili-Llop, Marcello Romano, Costantinos Zagaris
An algorithm to guide the capture of a tumbling resident space object by a spacecraft equipped with a robotic manipulator is presented. A solution to the guidance problem is found by solving a collection of convex programming problems. As convex prog
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9683349fec4b6ccbf2b6792a649ecc49
http://hdl.handle.net/11583/2963438
http://hdl.handle.net/11583/2963438
Autor:
Virgili-Llop, Josep, Costantinos Zagaris, Zappulla, Richard II, Bradstreet, Andrew, Romano, Marcello
Preprint accepted to appear in the International Journal of Robotics Research. An algorithm to guide the capture of a tumbling resident space object by a spacecraft equipped with a robotic manipulator is presented. A solution to the guidance problem
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::d5c3449adfd7032af96b5fd3a01e44cb
https://hdl.handle.net/10945/59478
https://hdl.handle.net/10945/59478
Autor:
Costantinos Zagaris, Marcello Romano
The article of record as published may be found at http://dx.doi.org/10.2514/6.2018-2220 The objective of this research is to investigate the dynamics, and reachability characteristics of a spacecraft (commonly referred to as the deputy) conducting p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0f8a10b7adf845257703215861ef425c
https://hdl.handle.net/10945/57266
https://hdl.handle.net/10945/57266
The article of record as published may be found at http://dx.doi.org/10.2514/1.A33769 Ground-based testbeds are critical to develop and test different elements of spacecraft guidance, navigation, and control subsystems. This paper provides an in-deta
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::59a16b59e834a62bebd8b9554dfb19f3
http://hdl.handle.net/11583/2963458
http://hdl.handle.net/11583/2963458
Publikováno v:
Scopus-Elsevier
Traditional space operations are characterized by large, highly-technical, long-standing satellite systems that cost billions of dollars and take decades to develop. Many branches of the US government have recognized the problem of sustaining current
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3572da6ae64c600eb53455ede1ebbddd
https://doi.org/10.2514/1.a32263
https://doi.org/10.2514/1.a32263
Publikováno v:
AIAA/AAS Astrodynamics Specialist Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c108fc1e9eb5ba6f433ae5d991e26c11
https://doi.org/10.2514/6.2016-5268
https://doi.org/10.2514/6.2016-5268