Zobrazeno 1 - 10
of 21
pro vyhledávání: '"Gabriella Gaias"'
Publikováno v:
Aerospace, Vol 11, Iss 3, p 224 (2024)
In recent years, the interest in proximity operations to uncooperative and non-collaborative objects has been growing and and demanding for specific technology advances to tackle these challenging cases of in-orbit servicing and removal missions. Ind
Externí odkaz:
https://doaj.org/article/af0b8076f55b4877b6af4bd0d2ac1f8f
Publikováno v:
Aerospace, Vol 10, Iss 11, p 959 (2023)
In this paper, the problem of autonomous optimal absolute orbit keeping for a satellite mission in Low Earth Orbit using electric propulsion is considered. The main peculiarity of the approach is to support small satellite missions in which the platf
Externí odkaz:
https://doaj.org/article/09b33bb29a0e4b919e6a828e06016f6b
Publikováno v:
Acta Astronautica. 205:33-46
This paper presents a strategy for optimal manoeuvre design of multi-satellite formation flying in low Earth orbit environment, with the aim of providing a tool for mission operation design. The proposed methodology for formation flying manoeuvres fo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::affc2f0ab576fde80d9f641afb288c21
http://hdl.handle.net/11311/1188459
http://hdl.handle.net/11311/1188459
A practical and effective numerical method is presented, aiming at solving the problem of initial relative orbit determination using solely line-of-sight measurements. The proposed approach exploits the small discrepancies which can be observed betwe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bbe849cf6f93312a013687aa38d46c2d
http://hdl.handle.net/11311/1139190
http://hdl.handle.net/11311/1139190
Publikováno v:
Advances in Space Research
This work presents a precise analytical model to reconstruct the line-of-sight vector to a target satellite over time, as required by angles-only relative navigation systems for application to rendezvous missions. The model includes the effects of th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::15621e0da7e9669838549bd6bf35a65a
http://hdl.handle.net/11311/1099115
http://hdl.handle.net/11311/1099115
Publikováno v:
Acta Astronautica. 123:409-419
AVANTI is a formation-flight experiment involving two noncooperative satellites. After a brief overview of the challenges that experiment design and scenario induce, this paper presents the safety concept retained to guarantee the safety of the forma
The paper provides an overview of the angles-only relative orbit determination activities conducted to support the Autonomous Vision Approach Navigation and Target Identification (AVANTI) experiment. This in-orbit endeavor was carried out by the Germ
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::83183945ff76bdeaeccf77a57db6f9f9
https://elib.dlr.de/114308/
https://elib.dlr.de/114308/
The paper describes the onboard vision-based navigation software employed during the DLR's AVANTI experiment and presents its flight performance. The navigation task relies on a dedicated target detection module in charge of extracting the line-of-si
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7a4088865adfcd091b5027cc8a9d4f29
http://hdl.handle.net/11311/1139191
http://hdl.handle.net/11311/1139191
This paper presents ultimate design, implementation, and in-flight performance of the spaceborne guidance navigation and control system which enabled the Autonomous Vision Approach Navigation and Target Identification (AVANTI) experiment; a flight de
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4992e9176a6e65b27a8dce866ab57cf2
https://elib.dlr.de/115566/
https://elib.dlr.de/115566/