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Modeling, Analysis and Simulation of a DC Distributed Power Architecture for an Airborne Application
Citation
Vesti, Sanna Kaarina, Alou Cervera, Pedro 
ORCID: https://orcid.org/0000-0002-2985-1330, Oliver Ramírez, Jesús Angel ORCID: https://orcid.org/0000-0002-5286-5378, García Suárez, Oscar ORCID: https://orcid.org/0000-0001-6042-3855, Prieto López, Roberto ORCID: https://orcid.org/0000-0001-7361-6816 and Cobos Márquez, José Antonio ORCID: https://orcid.org/0000-0003-4542-2656
(2010).
Modeling, Analysis and Simulation of a DC Distributed Power Architecture for an Airborne Application.
In: "Seminario Anual de Automática, Electrónica Industrial e Instrumentación (SAAEI)", 07/07/2010 - 09/07/2010, Bilbao, España.
Description
| Title: | Modeling, Analysis and Simulation of a DC Distributed Power Architecture for an Airborne Application |
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| Author/s: |
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| Item Type: | Presentation at Congress or Conference (Article) |
| Event Title: | Seminario Anual de Automática, Electrónica Industrial e Instrumentación (SAAEI) |
| Event Dates: | 07/07/2010 - 09/07/2010 |
| Event Location: | Bilbao, España |
| Title of Book: | Actas del Seminario Anual de Automática, Electrónica Industrial e Instrumentación (SAAEI) |
| Date: | 2010 |
| Subjects: | |
| Faculty: | E.T.S.I. Industriales (UPM) |
| Department: | Automática, Ingeniería Electrónica e Informática Industrial [hasta 2014] |
| Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
Abstract
This paper describes a design and analysis method for a DC distributed power architecture design in Airborne Application, utilizing simulation. Typically the used system components are commercial off-the-shelf components (COTS) thus complicating the system level analysis and simulation. Within this paper, it is shown how these systems can be designed utilizing simulation results, based on behavioural models of dc/dc converters. Additionally, models for commercial EMI filters are developed. This enables system level simulations and important information from efficiency, transient response, failures and stability is obtained assisting the designer to reach an optimum power system solution with minimum time and effort. Complex systems in avionics require high reliability. Therefore, the system level simulation is an essential tool for reaching the feasible solution complying with all the requirements
More information
| Item ID: | 7814 |
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| DC Identifier: | https://oa.upm.es/7814/ |
| OAI Identifier: | oai:oa.upm.es:7814 |
| Official URL: | http://www.saaei.org/ |
| Deposited by: | Memoria Investigacion |
| Deposited on: | 03 Aug 2011 08:25 |
| Last Modified: | 20 Apr 2016 16:50 |
