Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Shamil Biktimirov"'
Decentralized Differential Aerodynamic Control of Microsatellites Formation with Sunlight Reflectors
Autor:
Kirill Chernov, Uliana Monakhova, Yaroslav Mashtakov, Shamil Biktimirov, Dmitry Pritykin, Danil Ivanov
Publikováno v:
Aerospace, Vol 10, Iss 10, p 840 (2023)
The paper presents a study of decentralized control for a satellite formation flying mission that uses differential lift and drag to enforce the relative positioning requirements. All spacecraft are equipped with large sunlight reflectors so that, gi
Externí odkaz:
https://doaj.org/article/7871601734374ca0b353c49ecd20c817
Publikováno v:
Aerospace, Vol 9, Iss 8, p 419 (2022)
The paper presents a feasibility study of satellite formation-flying missions for space advertising. To estimate a space advertising mission viability, the global population coverage model is designed and the demonstration schedule with a focus on la
Externí odkaz:
https://doaj.org/article/d501d7c76db244e4b33e0295a025e754
Publikováno v:
Aerospace; Volume 9; Issue 8; Pages: 419
The paper presents a feasibility study of satellite formation-flying missions for space advertising. To estimate a space advertising mission viability, the global population coverage model is designed and the demonstration schedule with a focus on la
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7fa680346ead470dc9441738e87eabf2
https://doi.org/10.3390/aerospace9080419
https://doi.org/10.3390/aerospace9080419
Publikováno v:
Handbook of Space Security ISBN: 9783030227869
Handbook of Space Security
Handbook of Space Security
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b3468fca1b7ce08998a78a31c9b63f10
https://doi.org/10.1007/978-3-030-22786-9_138-1
https://doi.org/10.1007/978-3-030-22786-9_138-1
Publikováno v:
XLIII ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration.
An attitude determination and control system (ADCS) model is presented, which is used for CubeSat preliminary design stages in accordance with the European Space Agency (ESA) concurrent design approach. The model is implemented in Matlab/Simulink and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a06ed15d654082aa8e11f6f10d972a70
https://doi.org/10.1063/1.5133295
https://doi.org/10.1063/1.5133295