Modeling and stability analysis of hybrid power systems for the more electric aircraft

Electric Power Systems Research

Volumn 82, Issue 1, 2012, Pages 59-67

  Griffo, Antonio ^a   Wang, Jiabin ^b  

^a UNIVERSITY OF BRISTOL   (United Kingdom)

^b UNIVERSITY OF SHEFFIELD   (United Kingdom)

Author keywords

Linearization; More electric aircraft; Power system stability; Vehicular power systems

Indexed keywords

18-PULSE; AC-DC CONVERSIONS; COMPREHENSIVE ASSESSMENT; DESIGN PARAMETERS; DETAILED MODELING; FUNCTIONAL MODEL; HYBRID POWER SYSTEMS; LINEARIZED EQUATIONS; MORE ELECTRIC AIRCRAFT; POWER SYSTEM COMPONENTS; POWER SYSTEM STABILITY; SMALL SIGNAL STABILITY; SMALL SIGNAL STABILITY ANALYSIS; STABILITY ANALYSIS;

AC GENERATOR MOTORS; AIRCRAFT MODELS; DC POWER TRANSMISSION; ELECTRIC AUTOTRANSFORMERS; ELECTRIC SIGNAL SYSTEMS; LINEARIZATION; POWER TRANSMISSION; SYSTEM STABILITY;

ELECTRIC RECTIFIERS;

EID: 80053356145     PISSN: 03787796     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.epsr.2011.08.017     Document Type: Article

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