2009 IEEE International Electric Machines and Drives Conference 2009
DOI: 10.1109/iemdc.2009.5075450
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A DFT-based phase locked loop for phase and amplitude tracking in aircraft electrical systems

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Cited by 3 publications
(3 citation statements)
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“…Measuring and analyzing the PCC voltage permits then to calculate the reference current which the active filter has to compensate for. First of all, real-time implementation of the Discrete Fourier Transform (DFT) is utilized in order to estimate the fundamental phase angle and the amplitudes and phases of all the harmonic components of interest [10]. The work presented in this paper has been performed for 5 th , 7 th , 11 th and 13 th harmonics but it can be extended in the same way to any other component.…”
Section: Description Of the Techniquementioning
confidence: 99%
“…Measuring and analyzing the PCC voltage permits then to calculate the reference current which the active filter has to compensate for. First of all, real-time implementation of the Discrete Fourier Transform (DFT) is utilized in order to estimate the fundamental phase angle and the amplitudes and phases of all the harmonic components of interest [10]. The work presented in this paper has been performed for 5 th , 7 th , 11 th and 13 th harmonics but it can be extended in the same way to any other component.…”
Section: Description Of the Techniquementioning
confidence: 99%
“…Different from the phase-locked loop is that it is an open-loop system and without transient process. The phase-locked frequency multiplication measurement methods are actually hardware synchronous measurement method, it uses the frequency of phase-locked frequency multiplication to synchronize the sampling frequency and moment of A/D, once the digital frequency multiplying signal sends a rising edge of pulse ,the sampling circuit will conduct once data sampling [6,7]. The function of auto-adapted compensatory of the high precision frequency tracking technology may reduce the frequency multiplication error effectively; eliminate the calculation error caused by base wave fluctuations [8,9].…”
Section: Related Workmentioning
confidence: 99%
“…Literature contains several examples of control solutions for constant frequency electric aircraft power system networks [6] [7]. The most prominent control algorithms are phase-locked loops (PLLs) [8] and frequency-locked loops (FLLs) [9].…”
Section: Introductionmentioning
confidence: 99%