I(ROTOR)

RMS(v(ROTOR))

RMS(I(ROTOR))

I(SINEWAVEGEN)

RMS(I(SINEWAVEGEN))*RMS(V(SINEWAVEGEN))

RMS(I(SINEWAVEGEN))

RMS(V(VC1)+V(VC2)+V(CC1)+V(CC2)+V(ROTOR))*RMS(I(VC1)+I(VC2)+I(CC1)+I(CC2)+I(ROTOR))