(RMS(I(ROTOR1A))+RMS(I(ROTOR1B)))*RMS(V(ROTOR1A))*RMS(I(STATOR1))*RMS(V(STATOR1))

(RMS(I(ROTOR1A))+RMS(I(ROTOR1B)))*RMS(V(ROTOR1A))

RMS(I(ROTOR1A))+RMS(I(ROTOR1B))

RMS(V(ROTOR1A))

I(ROTOR1A)+I(ROTOR1B)

V(ROTOR1A)

V(ROTOR1A)/I(ROTOR1A)

RMS(I(STATOR1))*RMS(V(STATOR1))

RMS(I(STATOR1))

RMS(V(STATOR1))

I(STATOR1)

V(STATOR1)

RMS(I(ROTOR1A))*RMS(V(ROTOR1A))*RMS(I(ROTOR1B))*RMS(V(ROTOR1B))*RMS(I(STATOR1))*RMS(V(STATOR1))

V(STATOR1)/I(STATOR1)

RMS(V(BALLAST))*RMS(I(BALLAST))

RMS(V(LOAD))*RMS(I(LOAD))