Tesi etd-02112014-231543 |
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Tipo di tesi
Tesi di laurea magistrale
Autore
NOCERA, GIUSEPPE
URN
etd-02112014-231543
Titolo
Integration of Multi-physic models of All Electric Aircraft on board systems
Dipartimento
INGEGNERIA CIVILE E INDUSTRIALE
Corso di studi
INGEGNERIA AEROSPAZIALE
Relatori
relatore Prof. Denti, Eugenio
Parole chiave
- AEA
- clean sky
- on board systems
Data inizio appello
04/03/2014
Consultabilità
Completa
Riassunto
My thesis illustrates the integration and the update of the following systems in the Shared Simulation Environment prototype (SSE):
- Cabin Thermal (CT)
- Environmental Control System (ECS)
- Electrical Power Distribution System & Energy Management System (EPDS/EMS)
- Ice Protection System (IPS)
All the models were developed by the partners involved in the GRA WP 3.2. The integration platform used for the SSE is Matlab/Simulink and all the models have been developed in this simulation environment, except for the EPDS/EMS,IPS models and CT model, developed in Dymola and AMESim, respectively.
The CT model, has been integrated in Matlab/Simulink via S-function, the EPDS/EMS model via co-simulation.
- Cabin Thermal (CT)
- Environmental Control System (ECS)
- Electrical Power Distribution System & Energy Management System (EPDS/EMS)
- Ice Protection System (IPS)
All the models were developed by the partners involved in the GRA WP 3.2. The integration platform used for the SSE is Matlab/Simulink and all the models have been developed in this simulation environment, except for the EPDS/EMS,IPS models and CT model, developed in Dymola and AMESim, respectively.
The CT model, has been integrated in Matlab/Simulink via S-function, the EPDS/EMS model via co-simulation.
File
| Nome file | Dimensione |
|---|---|
| SUMMARY.pdf | 83.06 Kb |
| TESI.pdf | 2.43 Mb |
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