Zobrazeno 1 - 10
of 111
pro vyhledávání: '"Picosatellite"'
Publikováno v:
Aerospace, Vol 11, Iss 7, p 557 (2024)
This research presents the design and development of a near-space picosatellite platform intended to operate at high altitudes between 20–40 km above sea level. These picosatellites function similarly to orbital satellites but float and travel with
Externí odkaz:
https://doaj.org/article/d5e1148c436648ff9bba5d179031c2dc
Akademický článek
Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.
K zobrazení výsledku je třeba se přihlásit.
Akademický článek
Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.
K zobrazení výsledku je třeba se přihlásit.
Autor:
Herencia Ruiz, Daniel
We have recently been able to witness how large companies have set themselves the goal of launching fleets of hundreds or even thousands of satellites to offer different services. This new generation of satellites is marking a clear trend to reduce t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______3484::6cf1cdca44ae64e11ab48807614c576e
https://hdl.handle.net/2117/381090
https://hdl.handle.net/2117/381090
Publikováno v:
Radioengineering, Vol 22, Iss 1, Pp 389-393 (2013)
Conventional CubeSat radio systems typically use one of several basic modulations, such as AFSK, GMSK, BPSK, QPSK and OOK or switch between them on demand if possible. These modulations represent a bal¬anced trade-off between good energy efficiency
Externí odkaz:
https://doaj.org/article/fc863c2bef7f4de0b4b8651368af68da
Publikováno v:
Journal of Astronomy and Space Sciences, Vol 29, Iss 1, Pp 23-31 (2012)
Thermal analysis and control design are prerequisite essential to design the satellite. In the space environment, it makes satellite survive from extreme hot and cold conditions. In recent years CubeSat mission is developed for many kinds of purpos
Externí odkaz:
https://doaj.org/article/610952974c6541158d68183b821f3b71
Autor:
Shiroma Wayne, Martin Larry, Akagi Justin, Akagi Jason, Wolfe Byron, Fewell Bryan, Ohta Aaron
Publikováno v:
Open Engineering, Vol 1, Iss 1, Pp 9-15 (2011)
Externí odkaz:
https://doaj.org/article/aae594dededc4b65946af1ed75738c30
Publikováno v:
2021 IEEE International Symposium on Antennas and Propagation and USNC-URSI Radio Science Meeting (APS/URSI).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a8b5b10f64fbabd9fd5c797d040a9beb
https://doi.org/10.1109/aps/ursi47566.2021.9704477
https://doi.org/10.1109/aps/ursi47566.2021.9704477
Publikováno v:
Small Satellite Conference
The nascent field of fractionated satellite architectures provides an opportunity to improve spacecraft modularity and afford greater flexibility, adaptability, and upgradeability to spacecraft constellations. Satellite modules within a coherent form
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1459::7d57ca9d22ff7979ff3e91a803a60220
https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=4973&context=smallsat
https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=4973&context=smallsat
Publikováno v:
Revista Facultad de Ingeniería Universidad de Antioquia, Iss 70 (2014)
The purpose of this document is to describe the design and simulation of an attitude determination system (ADS) for the CubeSat Colombia I picosatellite, based on an extended Kalman filter EKF [1,2]. In this development the propagation of the State o
Externí odkaz:
https://doaj.org/article/70cdda3a35b74c2a8c2a81fded22729a