Zobrazeno 1 - 10
of 15
pro vyhledávání: '"NetSat"'
Autor:
Dauner, Johannes
This thesis proposes a distributed robust control approach for low-thrust nanosatellite formation flying. The presented control approach is the further development of an already existing approach which combines robust control and distributed control
Externí odkaz:
http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-80047
Autor:
Shastri, Bhardwaj
In the scope of this master thesis work, the proposed design for NetSat was analyzed for mission and system requirements with respect to structural and thermal limitations. Different load case scenarios for structural and thermal analysis were consid
Externí odkaz:
http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-76336
Autor:
Reinthal, Eric
For the upcoming formation flying technology demonstration mission NetSat a relative orbit propagator as well as a relative orbit controller were developed. The formation will consist of four equal nano-satellites with an electric propulsion system f
Externí odkaz:
http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61664
Autor:
Mammadov, Ilham
Recently, formation flying missions emerge because of their reliability, robustness and scalability in operation over single large spacecraft. Depending on the mission requirements satellites in a formation have to reconfigure themselves into new for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::08259b3e3cce416b4686b048f55484f1
http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-46169
http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-46169
Akademický článek
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Autor:
Cosper, Amy C.
Publikováno v:
Satellite Broadband. Jun2001, Vol. 2 Issue 6, p6. 1p.
Autor:
D.S., Sciannamea, Mike
Publikováno v:
Electronic Design. 2/17/97, Vol. 45 Issue 4, p176D. 1/2p. 1 Color Photograph.
Autor:
Martinez, Matthew
Publikováno v:
Mergers & Acquisitions Report. 01/25/99, Vol. 12 Issue 4, p4. 1/4p.
Autor:
Johannes Dauner
Publikováno v:
Johannes Dauner
This thesis proposes a distributed robust control approach for low-thrust nanosatellite formation flying. The presented control approach is the further development of an already existing approach which combines robust control and distributed control
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::e87ef9d5e6ffb22a4fd1432405bcb9b9
http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-80047
http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-80047
Publikováno v:
Technical University of Denmark Orbit
Nogueira, T, Scharnagl, J, Kotsiaros, S & Schilling, K 2015, NetSat-4G A four nano-satellite formation for global geomagnetic gradiometry . in Proceedings of 10th IAA Symposium on Small Satellites for Earth Observation . 10th IAA Symposium on Small Satellites for Earth Observation, Berlin, Germany, 20/04/2015 .
Nogueira, T, Scharnagl, J, Kotsiaros, S & Schilling, K 2015, NetSat-4G A four nano-satellite formation for global geomagnetic gradiometry . in Proceedings of 10th IAA Symposium on Small Satellites for Earth Observation . 10th IAA Symposium on Small Satellites for Earth Observation, Berlin, Germany, 20/04/2015 .
This paper proposes a concept for a Global GeomaGnetic Gradiometry (4G) nano-satellite mission. The proposed concept makes use of a formation of four nano-satellites carrying vector magnetometers and flying in a Cartwheel-Helix formation at low altit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::a2351edcbd08fc23f2b2998a47c340ba
https://orbit.dtu.dk/en/publications/bd24dada-4e47-4cf9-a161-368b953ef859
https://orbit.dtu.dk/en/publications/bd24dada-4e47-4cf9-a161-368b953ef859