Modelling and stability analysis of aircraft power systems

The more-electric aircraft concept is a major trend in aircraft electrical power system engineering and results in an increase in electrical loads based on power electronic converters and motor drive systems. Unfortunately, power electronic driven loads often behave as constant power loads having th...

Full description

Bibliographic Details
Main Author: Areerak, Kongpan
Format: Thesis (University of Nottingham only)
Language:English
Published: 2009
Subjects:
Online Access:https://eprints.nottingham.ac.uk/12944/

Similar Items