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Output details

15 - General Engineering

University of Nottingham

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Output 55 of 524 in the submission

Article title

Aircraft power system stability study including effect of voltage control and actuators dynamic

Type

D - Journal article

DOI

10.1109/TAES.2011.6034652

Title of journal

IEEE Transactions on Aerospace and Electronic Systems

Article number

Volume number

Issue number

First page of article

2574

ISSN of journal

0018-9251

Year of publication

2011

URL

Number of additional authors

Additional information

Output adopted by GE Aviation as part of their suite of analysis tools for the design of electrical power systems for future commercial aircraft systems (mike.bailey4@ge.com)

Interdisciplinary

Cross-referral requested

Research group

None

Proposed double-weighted

Double-weighted statement

Reserve for a double-weighted output

Non-English

English abstract