This post follows the method proposed in “Power System Stability and Control” by Prabha S. Kundur and Om P. Malik.

In p.u. We are looking for a representation :

\[\Delta \dot{x}_i = A_i \Delta x_i + B_i \Delta v\] \[\Delta i_i = C_i \Delta x_i + D_i \Delta v\]

Where :

\[\Delta v = \begin{bmatrix}\Delta v_{d} \\\Delta v_{q} \end{bmatrix}\] \[\Delta i_i = \begin{bmatrix}\Delta i_{d} \\\Delta i_{q} \end{bmatrix}\]

In order to obtain the state-space representation matrices \(A_i\) , \(B_i\) , \(C_i\) and \(D_i\) , we consider the stator voltage equations and the equations of motion.

The rotor circuit equations

\[p \psi_{fd} = \frac{\omega_0 R_{fd}}{X_{ad}} E_{fd} - \omega_0 R_{fd} i_{fd}\] \[p \psi_{1d} = -\omega_0 R_{1d} i_{1d}\] \[p \psi_{1q} = -\omega_0 R_{1q} i_{1q}\] \[p \psi_{2q} = -\omega_0 R_{2q} i_{2q}\]

The rotor currents are given by :

\[i_{fd} = \frac{1}{X_{fd}}(\psi_{fd} - \psi_{ad})\] \[i_{1d} = \frac{1}{X_{1d}}(\psi_{1d} - \psi_{ad})\] \[i_{1q} = \frac{1}{X_{1q}}(\psi_{1q} - \psi_{aq})\] \[i_{2q} = \frac{1}{X_{2q}}(\psi_{2q} - \psi_{aq})\]

The d- and q-axis mutual flux linkages are given by:

\[\psi_{ad} = -X_{ad}i_d + X_{ad}i_{fd}+X_{ad}i_{1d} = xaux_d (-i_d + \frac{\psi_{fd}}{X_{fd}}+\frac{\psi_{1d}}{X_{1d}})\] \[\psi_{aq} = -X_{aq}i_q + X_{aq}i_{1q}+X_{aq}i_{2q} = xaux_q (-i_q + \frac{\psi_{1q}}{X_{1q}}+\frac{\psi_{2q}}{X_{2q}})\] \[xaux_d = \frac{1}{\frac{1}{X_{ad}} + \frac{1}{X_{fd}}+ \frac{1}{X_{1d}}}\] \[xaux_q = \frac{1}{\frac{1}{X_{aq}} + \frac{1}{X_{1q}}+ \frac{1}{X_{2q}}}\]

Linearizing the previous equations and considering \(\Delta E_{fd} = 0\) :

\[\Delta \psi_{ad} = xaux_d (-\Delta i_d + \frac{\Delta \psi_{fd}}{X_{fd}}+\frac{\Delta \psi_{1d}}{X_{1d}})\] \[\Delta \psi_{aq} = xaux_q (-\Delta i_q + \frac{\Delta \psi_{1q}}{X_{1q}}+\frac{\Delta \psi_{2q}}{X_{2q}})\] \[\Delta i_{fd} = \frac{1}{X_{fd}}(\Delta \psi_{fd} - \Delta \psi_{ad}) = \frac{1}{X_{fd}}(\Delta \psi_{fd} - xaux_d (-\Delta i_d + \frac{\Delta \psi_{fd}}{X_{fd}}+\frac{\Delta \psi_{1d}}{X_{1d}}))\] \[\Delta i_{1d} = \frac{1}{X_{1d}}(\Delta \psi_{1d} - \Delta \psi_{ad}) = \frac{1}{X_{1d}}(\Delta \psi_ {1d} - xaux_d (-\Delta i_d + \frac{\Delta \psi_{fd}}{X_{fd}}+\frac{\Delta \psi_{1d}}{X_{1d}}))\] \[\Delta i_{1q} = \frac{1}{X_{1q}}(\Delta \psi_{1q} - \Delta \psi_{aq}) = \frac{1}{X_{1q}}(\Delta \psi_{1q} - xaux_q (-\Delta i_q + \frac{\Delta \psi_{1q}}{X_{1q}}+\frac{\Delta \psi_{2q}}{X_{2q}}))\] \[\Delta i_{2q} = \frac{1}{X_{2q}}(\Delta \psi_{2q} - \Delta \psi_{aq}) = \frac{1}{X_{2q}}(\Delta \psi_{2q} - xaux_q (-\Delta i_q + \frac{\Delta \psi_{1q}}{X_{1q}}+\frac{\Delta \psi_{2q}}{X_{2q}}))\] \[\Delta \dot \psi_{fd} = \frac{\omega_0 R_{fd}}{X_{ad}} \Delta E_{fd} - \omega_0 R_{fd} \Delta i_{fd} = -\omega_0 R_{fd} \frac{1}{X_{fd}}(\Delta \psi_{fd} - xaux_d (-\Delta i_d + \frac{\Delta \psi_{fd}}{X_{fd}}+\frac{\Delta \psi_{1d}}{X_{1d}}))\] \[\Delta \dot \psi_{1d} = -\omega_0 R_{1d} \Delta i_{1d} = -\omega_0 R_{1d} \frac{1}{X_{1d}}(\Delta \psi_{1d} - xaux_d (-\Delta i_d + \frac{\Delta \psi_{fd}}{X_{fd}}+\frac{\Delta \psi_{1d}}{X_{1d}}))\] \[\Delta \dot \psi_{1q} = -\omega_0 R_{1q} \Delta i_{1q} = -\omega_0 R_{1q} \frac{1}{X_{1q}}(\Delta \psi_{1q} - xaux_q (-\Delta i_q + \frac{\Delta \psi_{1q}}{X_{1q}}+\frac{\Delta \psi_{2q}}{X_{2q}}))\] \[\Delta \dot \psi_{2q} = -\omega_0 R_{2q} \Delta i_{2q} = -\omega_0 R_{2q}\frac{1}{X_{2q}}(\Delta \psi_{2q} - xaux_q (-\Delta i_q + \frac{\Delta \psi_{1q}}{X_{1q}}+\frac{\Delta \psi_{2q}}{X_{2q}}))\]

The stator voltage equations

\[v_d = -R_a i_d + X_l i_q - \psi_{ad}\] \[v_q = -R_a i_q - X_l i_d + \psi_{aq}\]

Linearizing the previous equations:

\[\Delta v_d = -R_a \Delta i_d + X_l \Delta i_q - \Delta \psi_{aq} = -R_a \Delta i_d + X_l \Delta i_q - xaux_q (-\Delta i_q + \frac{\Delta \psi_{1q}}{X_{1q}}+\frac{\Delta \psi_{2q}}{X_{2q}})\] \[\Delta v_q = -R_a \Delta i_q - X_l \Delta i_d + \Delta \psi_{ad} = -R_a \Delta i_q - X_l \Delta i_d + xaux_d (-\Delta i_d + \frac{\Delta \psi_{fd}}{X_{fd}}+\frac{\Delta \psi_{1d}}{X_{1d}})\]

The swing equation

\[p \omega_r = \frac{1}{2H}(T_m - T_e)\] \[T_e = \psi_d i_q - \psi_q i_d = \psi_{ad} i_q - \psi_{aq} i_d\]

Linearizing the previous equations and adding a term to account for the damping:

\[\Delta T_e = i_{q0} \Delta \psi_{ad} + \psi_{ad0} \Delta i_q - i_{d0} \Delta \psi_{aq} - \psi_{aq0} \Delta i_d = i_{q0}xaux_d (-\Delta i_d + \frac{\Delta \psi_{fd}}{X_{fd}}+\frac{\Delta \psi_{1d}}{X_{1d}})+ \psi_{ad0} \Delta i_q - i_{d0}xaux_q (-\Delta i_q + \frac{\Delta \psi_{1q}}{X_{1q}}+\frac{\Delta \psi_{2q}}{X_{2q}}) - \psi_{aq0} \Delta i_d\] \[\Delta \dot \omega_r = \frac{1}{2H}(\Delta T_m - \Delta T_e - K_D \Delta \omega_r)\]

Arranging the previous equations to assemble the state space equations:

\[a_{11} = -\frac{K_D}{2H}\] \[a_{12} = 0\] \[a_{13} = - \frac{1}{2H} \frac{i_{q0}xaux_d}{X_{fd}}\] \[a_{14} = -\frac{1}{2H}\frac{i_{q0}xaux_d}{X_{1d}}\] \[a_{15} = -\frac{1}{2H} \frac {-i_{d0} xaux_q}{X_{1q}}\] \[a_{16} = -\frac{1}{2H} \frac{-i_{d0}xaux_q}{X_{2q}}\] \[a_{21} = \omega_0\] \[a_{22} = 0\] \[a_{23} = 0\] \[a_{24} = 0\] \[a_{25} = 0\] \[a_{26} = 0\] \[a_{31} = 0\] \[a_{32} = 0\] \[a_{33} = -\omega_0 R_{fd} \frac{1}{X_{fd}}(1-\frac{xaux_d}{X_{fd}})\] \[a_{34} = -\omega_0 R_{fd} \frac{1}{X_{fd}}(-\frac{xaux_d}{X_{1d}})\] \[a_{35} = 0\] \[a_{36} = 0\] \[a_{41} = 0\] \[a_{42} = 0\] \[a_{43} = -\omega_0 R_{1d} \frac{1}{X_{1d}}(- \frac{xaux_d}{X_{fd}})\] \[a_{44} = -\omega_0 R_{1d} \frac{1}{X_{1d}}(1- \frac{xaux_d}{X_{1d}})\] \[a_{45} = 0\] \[a_{46} =0\] \[a_{51} =0\] \[a_{52} = 0\] \[a_{53} = 0\] \[a_{54} = 0\] \[a_{55} = -\omega_0 R_{1q} \frac{1}{X_{1q}}(1 - \frac{xaux_q}{x_{1q}})\] \[a_{56} = -\omega_0 R_{1q} \frac{1}{X_{1q}}(- \frac{xaux_q}{x_{2q}})\] \[a_{61} = 0\] \[a_{62} =0\] \[a_{63} = 0\] \[a_{64} = 0\] \[a_{65} = -\omega_0 R_{2q}\frac{1}{X_{2q}} (\frac{-xaux_q}{X_{1q}})\] \[a_{66} = -\omega_0 R_{2q}\frac{1}{X_{2q}} (1 - \frac{xaux_q}{X_{2q}})\] \[b_{11} = \frac{-1}{2H} (-\psi_{aq0} - i_{q0}xaux_d)\] \[b_{12} = \frac{-1}{2H} (\psi_{ad0} + i_{d0}xaux_q)\] \[b_{21} = 0\] \[b_{22} = 0\] \[b_{31} = -\omega_0 R_{fd} \frac{xaux_d}{X_{fd}}\] \[b_{32} = 0\] \[b_{41} = -\omega_0 R_{1d} \frac{xaux_d}{X_{1d}}\] \[b_{42} = 0\] \[b_{51} = 0\] \[b_{52} = -\omega_0 R_{1q} \frac{xaux_q}{X_{1q}}\] \[b_{61} = 0\] \[b_{62} = -\omega_0 R_{2q} \frac{xaux_q}{X_{2q}}\] \[c_{11} = 0\] \[c_{12} = 0\] \[c_{13} = 0\] \[c_{14} = 0\] \[c_{15} = \frac{- xaux_q}{x_{1q}}\] \[c_{16} = \frac{-xaux_q}{x_{2q}}\] \[c_{21} = 0\] \[c_{22} = 0\] \[c_{23} = \frac{xaux_d}{X_{fd}}\] \[c_{24} = \frac{xaux_d}{X_{1d}}\] \[c_{25} = 0\] \[c_{26} = 0\] \[d_{11} = -R_a\] \[d_{12} = X_l + xaux_q\] \[d_{21} = -X_l - xaux_d\] \[d_{22} = -R_a\]