Title :
Stability of aircraft D-C systems
Author_Institution :
Wright Air Development Center, Wright-Patterson Air Force Base, Ohio
Abstract :
IT IS IMPORTANT that the aircraft electric power system designer be provided with techniques for evaluating the effects of inverter loads on the stability of d-c systems. Inverter-induced instability has been a problem for a number of years. In the past, the problem has been resolved by arbitrarily changing the time response of some element of the system. Stability criteria have now been developed on the basis of measurable properties of the system.
Keywords :
Frequency response; Inverters; Mathematical model; Power system stability; Resonant frequency; Stability criteria;
Journal_Title :
Electrical Engineering
DOI :
10.1109/EE.1957.6442751
