DocumentCode :
2402590
Title :
AC Impedance Measurement Techniques
Author :
Familiant, Y.L. ; Corzine, K.A. ; Huang, J. ; Belkhayat, M.
Author_Institution :
Missouri Univ., Rolla, MO
fYear :
2005
fDate :
15-15 May 2005
Firstpage :
1850
Lastpage :
1857
Abstract :
Naval ship as well as aerospace power systems are incorporating a greater degree of power electronic switching sources and loads. Although these power electronics based components provide exceptional performance, they are prone to instability due to their high efficiency and constant power characteristics which lead to negative impedance. When designing these systems, integrators must consider the impedance versus frequency at a system interface (which designates source and load). Stability criterions have been developed in terms of source and load impedance for both DC and AC systems and it is often helpful to have techniques for impedance measurement. For DC systems, the measurement techniques have been well established. This paper suggests several methods for measuring AC impedance including utilization of power converters, induction machines and chopper circuits. Simulation results on an example AC system demonstrate the effectiveness of the proposed methods
Keywords :
asynchronous machines; choppers (circuits); electric impedance measurement; power convertors; AC impedance measurement techniques; aerospace power systems; chopper circuits; induction machines; load impedance; naval ship; power converters; power electronic switching sources; stability criterions; system interface; Aerospace electronics; Frequency; Impedance measurement; Marine vehicles; Measurement techniques; Power electronics; Power measurement; Power system measurements; Power system stability; Stability criteria;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electric Machines and Drives, 2005 IEEE International Conference on
Conference_Location :
San Antonio, TX
Print_ISBN :
0-7803-8987-5
Electronic_ISBN :
0-7803-8988-3
Type :
conf
DOI :
10.1109/IEMDC.2005.195972
Filename :
1531590
Link To Document :
بازگشت