Zobrazeno 1 - 10
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pro vyhledávání: '"Nanosatellit"'
Akademický článek
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Propulsion systems allow satellites to perform many functionalities in space, such as orbital station keeping, reentry control, attitude control, orbital transferring, rendezvous operation, and even more thrilling, interplanetary travel. Indeed, prop
Externí odkaz:
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-288714
Autor:
Larsson, Jesper
The purpose of this paper was to implement Kalman filtering in the form of pre-existing Simulink blocks into a CubeSat attitude determination and control system simulation and to evaluate their performance. In recent versions of Simulink, the block l
Externí odkaz:
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-285762
Autor:
Larsson, Jesper
The purpose of this paper was to implement Kalman filtering in the form of pre-existing Simulink blocks into a CubeSat attitude determination and control system simulation and to evaluate their performance. In recent versions of Simulink, the block l
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::a2073fc0b7eb6f0d72f9be2658a3d042
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-285762
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-285762
Propulsion systems allow satellites to perform many functionalities in space, such as orbital station keeping, reentry control, attitude control, orbital transferring, rendezvous operation, and even more thrilling, interplanetary travel. Indeed, prop
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::ba4d26c7ed85a8ba7257d20ca2fcc571
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-288714
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-288714
Autor:
Nermark, Clara
When developing products for space, including nanosatellites, the verification and validation process is a mandatory part of any project conducted within the European space industry. Within such a process, testing is a method for verification and val
Externí odkaz:
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-325791
Autor:
Surivet, Anthony
With the increasing number of satellites operating in orbit and the development of nanosatelliteconstellations, it has become more and more arduous for operators to keep track of every satellitestate, and perform corrective or avoidance manoeuvres. T
Externí odkaz:
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-299420
Autor:
Järmyr Eriksson, Carl
A finite element model of the CubeSat MIST was created, in order to assess the stresses that occur in the satellite in response to loads during its launch. Due to size limits of thesoftware used, simplifications had to be made to the geometry of the
Externí odkaz:
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-309956
Autor:
Järmyr Eriksson, Carl
A finite element model of the CubeSat MIST was created, in order to assess the stresses that occur in the satellite in response to loads during its launch. Due to size limits of thesoftware used, simplifications had to be made to the geometry of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::12035612a09ff0f04213e0824902d0fb
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-309956
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-309956
Autor:
Surivet, Anthony
With the increasing number of satellites operating in orbit and the development of nanosatelliteconstellations, it has become more and more arduous for operators to keep track of every satellitestate, and perform corrective or avoidance manoeuvres. T
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::5ae71b50c11e957f3a934da8681c667d
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-299420
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-299420