The constant growth of air traffic, the demand for performance optimization, and the need for
decreasing both operating and maintenance costs have encouraged the aircraft industry to …

The structure and control strategy of a novel two-phase brushless main exciter (ME) are
proposed in this paper to solve the excitation problem of the main generator (MG) when the …

Purpose More electric aircraft (MEA) is defined as the extensive usage of electric power in
aircraft. The demand for electric power in new generation aircraft rises due to environmental …

Accurate information about the field current of the wound-rotor synchronous starter
generator (WRSSG) is prerequisite for optimal start control research for WRSSG in the …

With the penetration of power electronics in more electric aircraft (MEA) power systems, the
number of constant power loads continues increasing and the characteristics of negative …

This study proposes a novel mathematical model based on excitation system output
equations (ESOEs) to evaluate the steady‐state performance of the three‐phase brushless …

This study focuses on the identification of the rotating diode failures of an aircraft wound‐
field synchronous starter–generator system. Owing to the difference in topography between …

An integrated starter/generator based on the wound-rotor synchronous machine is
becoming increasingly popular in modern aircraft due to the advantages of high safety and …

In this paper, a rotating rectifier fault detection method is proposed and tested, by using the
differences between the total harmonic distortion (THD) and polarity of asynchronous exciter …

This paper reports a brushless induction excited synchronous generator. An induction
machine (IM) and a synchronous machine (SM) are embedded in the same machine frame …