Output details
15 - General Engineering
University of Nottingham
Article title
Stability study for a hybrid AC-DC more-electric aircraft power system
Type
D - Journal article
Title of journal
IEEE Transactions on Aerospace and Electronic Systems
Article number
-
Volume number
48
Issue number
1
First page of article
329
ISSN of journal
0018-9251
Year of publication
2012
Number of additional authors
4
Additional information
The modelling approach described in this paper is particularly well-suited to aerospace power systems consisting of a wide variety of interacting sources and loads. It is being applied and further developed in collaboration with Dassault Aviation (Jean-Marc.Le-Peuvedic@dassault-aviation.com) and Airbus (Guenter.Walper@airbus.com).
Interdisciplinary
-
Cross-referral requested
-
Research group
None
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-
