Induction machine

Induction machine model for detailed representation of electrical loads.

Disclaimer: This model has only been tested for the power flow problem with ACP formulation.

Parameters

Set of parameters used to model the induction machine as defined in the input data

namesymb.unittypedefaultdefinition
index$im$-Int-unique index of the induction machine
im_bus$i$-Int-unique index of the bus to which the induction machine is connected to
P_ag$P_{ag}$p.u.Real-Starting value for active power of induction machine - positive for consumption
Q_ag$Q_{ag}$p.u.Real-Starting value for active power of induction machine - positive for consumption
Pacmin$\underline{P_{im}}$p.u.Real-minimum stable operating power of the induction machine
Pacmax$\overline{P_{im}}$p.u.Real-maximum power rating of the induction machine
Pacrated$P_{im}$p.u.Real-minimum reactive power of the induction machine
status$\delta_{im}$-Int-Status indicator of the induction machine
x_m$x_{m}$p.u.Real-Magnetizing inductance of induction machine
x_sl$x_{sl}$p.u.Real-Stator leakage inductance of induction machine
x_rl$x_{rl}$p.u.Real-Rotor leakage inductance of induction machine
r_s$r_{s}$p.u.Real-Stator resistance of induction machine
r_r$r_{r}$p.u.Real-Rotor resistance of induction machine
torque----Torque model parameters of induction machine

Torque parameter

The torque model is implemented as $T(\omega) = T_0 * (A*\omega^m+B \omega + C)$. This representation includes both quadratic models (m=2) or power functions (B=C=0) (see Kundur).

NameSymbolUnitTypeDefaultDescription
T_0$T_0$p.u.Real-Per-unit torque scaling factor (base torque is approximately equal to the system base power)
A$A$$\mathrm{s}^2/\mathrm{rad}^2$Real-Quadratic coefficient of the mechanical torque characteristic (load component typical for centrifugal devices or aerodynamic drag)
B$B$$\mathrm{s}/\mathrm{rad}$Real-Linear coefficient of the mechanical torque characteristic (friction load component)
C$C$-Real-Constant coefficient of the mechanical torque characteristic (static load component)
m$m$-Real-Mechanical torque exponent describing the load type (see Kundur)

Variables

The main optimisation variables of interest are:

namesymb.unitformulationdefinition
pg$P_{g}$p.u.ACPActive power of induction machine g
qg$Q_{g}$p.u.ACPReactive power of induction machine g

Constraints

See Kundur or Van Cutsem for detailed derivation of equations.

Stator constrains

PowerModelsACDC.constraint_im_statorFunction

Im stator constraints (Based on transformer formulation)

\[p_{im,s,fr} = g v_{m,fr}^{2} - g v_{m,fr} v_{m,to}\cos\left(v_{a,fr}-v_{a,to}\right) - b v_{m,fr} v_{m,to}\sin\left(v_{a,fr}-v_{a,to}\right)\]

\[q_{im,s,fr} = - b v_{m,fr}^{2} + b v_{m,fr} v_{m,to}\cos\left(v_{a,fr}-v_{a,to}\right) - g v_{m,fr} v_{m,to}\sin\left(v_{a,fr}-v_{a,to}\right)\]

\[p_{im,s,to} = g v_{m,to}^{2} - g v_{m,to} v_{m,fr}\cos\left(v_{a,to}-v_{a,fr}\right) - b v_{m,to} v_{m,fr}\sin\left(v_{a,to}-v_{a,fr}\right)\]

\[q_{im,s,to} = - b v_{m,to}^{2} + b v_{m,to} v_{m,fr}\cos\left(v_{a,to}-v_{a,fr}\right) - g v_{m,to} v_{m,fr}\sin\left(v_{a,to}-v_{a,fr}\right)\]

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Rotor inductance constraints

PowerModelsACDC.constraint_im_rotor_inductanceFunction

IM rotor inductance constraints

\[-p_{im,ag} = g_c v_{m,ag}^{2} - g_c v_{m,ag} v_{m,m}\cos\left(v_{a,ag}-v_{a,m}\right) - b_c v_{m,ag} v_{m,m}\sin\left(v_{a,ag}-v_{a,m}\right)\]

\[-q_{im,ag} = - b_c v_{m,ag}^{2} + b_c v_{m,ag} v_{m,m}\cos\left(v_{a,ag}-v_{a,m}\right) - g_c v_{m,ag} v_{m,m}\sin\left(v_{a,ag}-v_{a,m}\right)\]

\[p_{im,ri,f} = g_c v_{m,m}^{2} - g_c v_{m,m} v_{m,ag}\cos\left(v_{a,m}-v_{a,ag}\right) - b_c v_{m,m} v_{m,ag}\sin\left(v_{a,m}-v_{a,ag}\right)\]

\[q_{im,ri,f} = - b_c v_{m,m}^{2} + b_c v_{m,m} v_{m,ag}\cos\left(v_{a,m}-v_{a,ag}\right) - g_c v_{m,m} v_{m,ag}\sin\left(v_{a,m}-v_{a,ag}\right)\]

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Magnetistation branch constraints

Slip constraints

PowerModelsACDC.constraint_im_slipFunction

IM slip constraints (slip from balance air-gap power with mechanical torque, see Van Cutsem Voltage stability)

\[T_0\left(A(1-s)^m+B(1-s)+C\right) = \frac{v_{m,ag}^{2}s}{r_r}\]

\[p_{im,ag} = \frac{v_{m,ag}^{2}s}{r_r}\]

\[q_{im,ag}=0\]

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