DocumentCode :
2051587
Title :
Improved method for real-time transient stability assessment of power systems
Author :
Echeverria, D.E. ; Rueda, J.L. ; Colome, D.G. ; Erlich, I.
Author_Institution :
Inst. de Energia Electr., Univ. Nac. de San Juan (IEE-UNSJ), San Juan, Argentina
fYear :
2012
fDate :
22-26 July 2012
Firstpage :
1
Lastpage :
8
Abstract :
This paper presents a new approach to predict the time evolution of rotor angles of synchronous machines based on a modification of the Taylor series expansion in order to assess the transient stability of power systems in real time. To demonstrate the benefits of the proposed approach, a comparative analysis is made with other approaches which have been used for predicting the rotor angles, namely regression and interpolation algorithms and an approach based on original Taylor series expansion. The different prediction approaches are applied to the New England benchmark power system to predict the time evolution of the rotor angles in terms of stability and instability of first and second swing. The obtained results highlight the prediction accuracy of the proposed approach and the fulfilment of computational time requirements concerning real time applications.
Keywords :
interpolation; power system transient stability; regression analysis; synchronous machines; New England benchmark power system; Taylor series expansion; interpolation algorithms; power system transient stability; prediction approach; real-time transient stability assessment; regression algorithms; rotor angles; synchronous machines; Generators; Mathematical model; Phasor measurement units; Polynomials; Power system stability; Rotors; Taylor series; PMU; Rotor angle prediction; Taylor series; WAMS; real time assessment; transient stability;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Power and Energy Society General Meeting, 2012 IEEE
Conference_Location :
San Diego, CA
ISSN :
1944-9925
Print_ISBN :
978-1-4673-2727-5
Electronic_ISBN :
1944-9925
Type :
conf
DOI :
10.1109/PESGM.2012.6345036
Filename :
6345036
Link To Document :
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