This paper describes the Hardware-In-the-Loop (HIL) simulation methodology used for the verification of functional requirements of e-st@r-I CubeSat. The satellite’s behavior has been investigated via HIL simulation, and the results obtained are consistent with the expected values in any operative conditions. It is proven that HIL simulation is a valuable means for supporting the verification process of small satellites and may help reduce time and cost of the development phase and increase mission reliability.
Verification of a CubeSat via Hardware-in-the-loop Simulation / Corpino, Sabrina; Stesina, Fabrizio. - In: IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS. - ISSN 0018-9251. - ELETTRONICO. - 50:4(2014). [10.1109/TAES.2014.130370]
Verification of a CubeSat via Hardware-in-the-loop Simulation
CORPINO, Sabrina;STESINA, FABRIZIO
2014
Abstract
This paper describes the Hardware-In-the-Loop (HIL) simulation methodology used for the verification of functional requirements of e-st@r-I CubeSat. The satellite’s behavior has been investigated via HIL simulation, and the results obtained are consistent with the expected values in any operative conditions. It is proven that HIL simulation is a valuable means for supporting the verification process of small satellites and may help reduce time and cost of the development phase and increase mission reliability.File | Dimensione | Formato | |
---|---|---|---|
Manuscript_Verification of a cubesat via HIL simulation_post print_PORTO.pdf
accesso aperto
Tipologia:
2. Post-print / Author's Accepted Manuscript
Licenza:
Pubblico - Tutti i diritti riservati
Dimensione
1.53 MB
Formato
Adobe PDF
|
1.53 MB | Adobe PDF | Visualizza/Apri |
Pubblicazioni consigliate
I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
https://hdl.handle.net/11583/2535907
Attenzione
Attenzione! I dati visualizzati non sono stati sottoposti a validazione da parte dell'ateneo