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Mathematically, L / ss = ω ss [L 2 mm /L rr ] and T rr = L rr /r rr, where L rr and r rr are the rotor self-inductance and resistance, respectively, and L mm is the mutual inductance between the stator and the rotor terminals of the DFIG.
As depicted from this figure, the DFIG stator terminals are directly connected to the low voltage side of the utility transformer (LVSUT), whereas, the DFIG rotor terminals are connected to the same LVSUT via a back to back, voltage source converter (VSC) based power electronic circuit.
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The series R-L circuit is inserted between the rotor-winding terminals and the ac-side of rotor-side power converter (RSPC) when the rotor overcurrent exceeds its threshold value during faults.
ISC implements synergetic control of terminal voltage, rotor speed, mechanical input power and guide vane opening.
During a short-circuit fault, a very high current flows through both stator and rotor windings, and the terminal voltage of the DFIG becomes very low [4].
According to the control objectives, a manifold, which is a linear combination of the deviation of generator terminal voltage, rotor speed and active power, is chosen for the design of ISEC.
The proposed control law will be shown to optimally and exponentially regulate the terminal voltage, the rotor angle, and the rotor speed to the reference values.
It will decrease the terminal voltage amplitude drop, terminal voltage phase angle, maximum rotor current, and increase reactive power output.
The design includes rotor speed estimation from measured stator terminal voltages and currents.
The aim is to obtain high performance for the terminal voltage and the rotor speed simultaneously under a large sudden fault and a wide range of operating conditions.
The aim is to obtain high performance for the terminal voltage and the rotor speed simultaneously under a sudden fault and a wide range of operating conditions.
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