In this paper, the design of a fully magnetic attitude control subsystem for a picosat platform is discussed. The developed control law is based on a simple and reliable architecture, which can be easily implemented on small spacecrafts for de-tumbling and three-axis stabilization purposes. The subsystem design follows a practical engineering approach, exploiting global optimization methods, which lead to an integral actuation compliant with typical pointing accuracy requirements for picosat missions. Performance of the proposed attitude control subsystem is demonstrated by numerical simulations.
Titolo: | Fully magnetic attitude control subsystem for picosat platforms | |
Autori: | ||
Data di pubblicazione: | 2018 | |
Rivista: | ||
Handle: | http://hdl.handle.net/11311/1043407 | |
Appare nelle tipologie: | 01.1 Articolo in Rivista |
File in questo prodotto:
File | Descrizione | Tipologia | Licenza | |
---|---|---|---|---|
COLAA_OA_01-18.pdf | Paper open access | Post-Print (DRAFT o Author’s Accepted Manuscript-AAM) | Accesso apertoVisualizza/Apri | |
COLAA01-18.pdf | Paper | Publisher’s version | Accesso riservato |
I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.