2017
DOI: 10.1109/tste.2016.2597306
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A Sliding Mode Based Damping Control of DFIG for Interarea Power Oscillations

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Cited by 99 publications
(51 citation statements)
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“…The advantages of using the Lagrange multiplier method is as follows. First the constraints can be Algorithm 1 ADMM-Algorithm 1: Each local processor (q) initializes a q 0 , b q 0 using (12) and (13). z 0 and w q 0 are also initialized 2: At iteration j: 3: Local processors updates a q as a q j+1 = argmin a q L ρ 4: Local processor transmits a q j+1 to the global processor 5: Global processor calculates z j+1 = 1 2 2 q=1 a q j+1 6: Global processor transmits z j+1 to all local processors.…”
Section: Generatormentioning
confidence: 99%
“…The advantages of using the Lagrange multiplier method is as follows. First the constraints can be Algorithm 1 ADMM-Algorithm 1: Each local processor (q) initializes a q 0 , b q 0 using (12) and (13). z 0 and w q 0 are also initialized 2: At iteration j: 3: Local processors updates a q as a q j+1 = argmin a q L ρ 4: Local processor transmits a q j+1 to the global processor 5: Global processor calculates z j+1 = 1 2 2 q=1 a q j+1 6: Global processor transmits z j+1 to all local processors.…”
Section: Generatormentioning
confidence: 99%
“…Performance and assessment of WT depends on rotor thrust, torque, and power. The mechanical power extracted from wind speed is given by Pm=12ρπR2Vw3CPfalse(λ,βfalse),1em where ρ is the air density; typical value is ρ = 1.22 kg / m 3 ; R is the length of the blade; V w is the wind velocity in m/s; C p is the power coefficient,which is function of tip speed ratio that is λ = Rω r / V w and β position of blade angle; and ω r is rotating speed of rotor. The analytical expression of C p defined in terms of λ , β , and turbine coefficients by arrayCP(λ,β)=0.5176116λi0.4β5e21λi+0.0038λarray1λi=1λ+0.08β0.0351+β3.1em …”
Section: Mathematical Modelling Of Dfig_wesmentioning
confidence: 99%
“…Performance and assessment of WT depends on rotor thrust, torque, and power. The mechanical power extracted from wind speed is given by 16,17…”
Section: Wt Modellingmentioning
confidence: 99%
“…Here, f is obtained from (1), (5), (6), (8), (11), (17), and (18). Further, g is obtained from (2)-(4), (7), (9), (10), (12)- (16), and (19).…”
Section: Linearized Dynamic Model Of Overall Systemmentioning
confidence: 99%
“…Here, Y(s) = Δ(I + I e ), Δ(P + P e ), and Δs m are used, and U(s) = V * s . With input V * s , Equation 33 can be written in the state space, with a small change based on state equation (11), as follows:…”
Section: Design Of Output Feedback Damping Controllermentioning
confidence: 99%