Modeling Free Acceleration of a Salient Synchronous Machine Using Two-Axis Theory

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1 Modeling ree Acceleration of a Salient Synchronous Machine Using Two-Axis Theory Abdullah H. Akca and Lingling an, Senior Member, IEEE Abstract This paper investigates a nonlinear simulation model of a synchronous machine derived from space vector. The model is built to show acceleration from zero speed to nominal speed while its stator is connected to a three-phase voltage source. The two-axis modeling approach is adopted to emulate the threephase stator circuits as dq circuits on the rotor. The entire model is based on the rotor reference frame. or swing dynamics, torque/speed dynamic equation is adopted without any approximation. A machine started by a three-phase voltage source at its stator is simulated via MATLAB/Simulink. The simulation results demonstrate how to start a synchronous machine: without excitation voltage and with increased resistance in the excitation circuit. Index Terms Space Vector SV), Synchronous Machine SM), Magnetomotive orce MM), Electromotive orce EM), dq fictitious circuit I. INTRODUCTION Instead of using Park s transformation, we show in this article that Park s transformation can be viewed to use two fictitious circuits on rotor to represent the three-phase stator circuit. or synchronous generator analysis, this approach is easy to be understood and provides great insights. The key concept here is space vector. When a standing still three-phase synchronous machine connected to a three-phase voltage source at its stator, three-phase balanced stator currents create rotating magnetomotive force MM) Ampers law) in the air gap. This MM generates a rotating flux armature flux) in the air gap. This flux induces sinusoidal EM in the rotor windings. So a current starts to flow through the rotor circuit which forms a rotating MM and further a rotor flux. Interaction of the armature flux and rotor flux stator MM or rotor MM) leads to electromagnetic torque and the machine may start rotate. This procedure is same as the induction effect of an induction motor. The difference of a salient synchronous machine and an induction machine resides in the salience of the synchronous machine rotor. Unlike an induction machine where the rotor is round and the airgap is uniform, a salient synchronous machine has a nonsymmetric rotor and an nonuniform airgap. Modeling of a synchronous machine is easier using two-axis theory. Basically speaking, two-axis theory decomposes MM into d and q axes, where d-axis is aligned with the rotor flux generated by the excitation current) direction, q-axis lags d- axis by 9 degree. See ig. 1. That way, for d-axis MM, the airgap path is fixed and for q-axis MM, the airgap path is also fixed. This in turn results in fixed inductances of dq-axis L d and L q ). It is also easy to see that L d should be greater than L q since the airgap path in d-axis direction is much shorter than that in the q-axis direction. d-axis q d Reference θ d q q-axis ig. 1: Synchronous machine dq axes positions, excitation winding, and two fictitious windings dd qq. The effect of the three-phase stator circuits on forming an MM is similar as two fictitious circuits on the rotor on forming a d-axis MM and a q-axis MM. Therefore, the two windings dd and qq in ig. 1 are used to represent the stator circuits. To start a synchronous machine, induction effect is key. Therefore, the excitation voltage source is short cut. In the rest of the paper, Section II presents machine modeling based on space vector concept. Section III presents the simulation model and case study results. Section IV concludes the paper. II. SPACE VECTOR-BASED SYNCHRONOUS MACHINE MODELING A. Space vector and Park s transformation The concept of space vector aligns with the physics of Ampere s Law: three-phase balanced stator currents form a rotating MM. The rotating speed is the electric frequency. The MMs due to each phase stator current are expressed as follow. f a α, t) = NI a t) cosα) f b α, t) = NI b t) cos α π ) f c α, t) = NI c t) cos α π ) 1)

where N is the number of windings, α is a position in the airgap and the three-phase balanced currents are expressed as follows. i a t) = I m cosω s t θ a ) i b t) = I m cos ω s t θ a π ) i c t) = I m cos ω s t θ a π ) where θ a is the initial phase angle of the phase-a current. Therefore the total MM due to the stator currents is: f s α) = N i a cosα) i b cos α π ) i c cos α π = 1.5I m cosα θ a ) ) Writing it in the form of a space vector to indicate the magnitude and the position of the maximum MM, we have f s = 1.5NI m e jθa = Ni a Ni b e jπ/ Ni c e jπ/ 4) It can be found that the space vector of the MM is proportional to the analytic form of i a t). In turn, space vector representation of a variable follows all rules of the original variable. On zero sequence i a = i b = i c, so related space vector value will be zero. This means, there will not be any MM or torque generation for zero sequence. rom the equations above, space vector notation of the stator MM for a balanced set can be shown as ) fs t) = NI ae jωstθ). 5) This vector will be decomposed into d-axis and q-axis components aligned with the rotor reference frame. Assume that the rotor rotating speed is ω m, then we have: where θ is the initial rotor angle position. Or i dq = e jθ ) i = e jθ i a i b e j π ic e j π 11) where θ = ω m t θ is the rotor position. This transformation aligns with the Park s transformation defined in Kraus book [1], where i i d = 1 1 1 cosθ) cos ) θ π cos ) i a θ π i q sinθ) sin ) θ π sin ) i b θ π i c If we use the above space vector notation, for three-phase )) power p = v a i a v b i b v c i c, assume balanced operation, we will end up with p = v di d v q i q ) 1) To avoid using, we can scale up space vectors by k =. This type of scaling up is used in the Park s transformation of Bergen s book []. Note the Park s transformation in [] is defined as follows. i 1 1 1 i d = cosθ) cos ) θ π cos ) i a θ π i q sinθ) sin ) θ π sin ) i b θ π i c where θ is the angle the dq reference frame is ahead of the static reference frame. The relationship of flux linkages, dq currents and excitation current i is as follows. Notations of this paper follows the classic text []. = L d i d km i 1) = km i L i 14) = L q i q 15) f sdq = NI me jωs ωm)t 6) f sd = NI m cosω s ω m )t 7) f sq = NI m sinω s ω m )t 8) The dq-axis MMs produces dq fluxes in the airgap. The d- axis flux will link with the rotor circuit and generates flux linkage for. Based on araday s law, if this flux linkage is varying, will have induced EM and in turn current i. i in turn will generate an MM and flux. Therefore, the total d-axis air gap flux is due to both i d and i while the q-axis flux is due to i q only. rom the forming of rotating magnetic field, we introduce the space vector definition as: i = i a i b e jπ/ i c e jπ/ ) 9) is introduced as a scaling factor so that the magnitude of the space vector is the same as that of the per-phase signals. If we view this space vector from the rotor reference frame as i dq, then i dq e jωmtθ) = i = I m e jωsθa) 1) B. araday s Law In this subsection, we will express stator and rotor voltage/current relationship applying araday s Law. or the stator voltage, considering the stator resistance r s, its relationship with the stator current and stator flux linkage is as follow. vs t) = r s is t) d λ t) 16) The space vectors will be viewed based on the rotor frame, then the rotating speed of the space vectors will be reduced by ω m since the rotor speed is ω m. v dq = v s e jωmtθ) 17) v dq = r s i dq dq jω m q 18) where f dq = f d jf q. The dq stator circuits voltage, current an flux linkage relationship is expressed as v d = r s i d d ω m 19) v q = r s i q d ω m. )

or the EM induced in the rotor windings, the related equation is = r i d t) 1) In term of fluxes, rotor and stator circuit voltages can be shown as v sd v sq = L d r km r s km r L r s λ d ω m ω m r s L q The machine speed is related to the net torque. J dω m ) = T m ) where is the electromagnetic torque and T m is the mechanical torque. In this study, T m =. The electromagnetic torque is expressed by flux linkages only as follow. = P [ λd L q km L d L km ) where P is the number of pole pairs. ] L L d L km ) 4) A. Case Study I TABLE I: Parameters Nominal voltage 1 ω s 14 rad/sec r s. r.1 L d.98 L q.45 L.65 km.8 J.9 P poles) N 1 Machine acceleration is analyzed while there is no exterior excitation effect on it. Electrical torque and angular speed relation is given in ig. 5 and,, fluxes are presented ig. 4. 1 x 1 7 1 4 5 6 7 8 5 x 1 6 III. SIMULATION or a synchronous machine that operates as an induction machine, free acceleration simulation is made. or this operation, parameters from Table I are used. Equations ) and 4) are modelled via MATLAB/Simulink. ig. is the block diagram of the simulated system and ig. is the Simulnk screen copy. Related to this simulation, three different case studies are analysed. In the first case, there is no exterior resistances connected to machine for excitation. In the second case, the excitation circuit resistance is 81 times of the original one. In the last case, the resistance is 8 times of the original one. 1 4 5 6 7 8 5 x 1 1 4 5 6 7 8 ig. 4:,,. vsd vsq - dλ/ lux Electrical Torque Te - 1/J m ω rad/s) 1 Cosθ) Sinθ) lux s Tm 1 4 5 6 7 8 x 1 ig. : Block Model of the synchronous machine. As it is seen, v d, v q are input variables of the synchronous machine. v d, v q are computed based on the following equations. v d = V m cosω s ω m )t 5) v q = V m sinω s ω m )t 6) N.m) 1 4 5 6 7 8 ig. 5: iltered and the angular speed. where V m is the voltage magnitude. or this case, angular speed can only reach half of the full.

4 ig. : Block Model of the synchronous machine. B. Case Study II It is seen that in the previous case, the machine could not be accelerated to a full speed. In this case, exterior resistance is used which is 81 times of r. It can be observed that the angular speed ω m saturates at 5 rad/sec as shown in ig. 7. 1 x 1 ω rad/s) 1 1 4 5 6 7 8 x 1 1 4 5 6 7 8 x 1 N.m) 1 4 5 6 7 8 5 x 1 1 4 5 6 7 8 ig. 6:,,. 1 4 5 6 7 8 ig. 7: Speed and filtered. to 77 rad/s. After a dip at 5- seconds, the electrical torque saturates and its average value becomes zero. The flux distribution is shown in ig. 8. In this case, angular speed saturates at 77 rad/sec while has stable distribution. ig. 6 presents flux linkages. It is observed that the average flux values are zero at steady-state. C. Case Study III or acceleration of the synchronous machine, in this case an exterior resistance is connected to the machine whose value is larger than the previous cases and 8 times of the original rotor resistance. In this way, the machine can accelerate to a full speed as shown in ig. 9. After a steady speed at about 5 rad/s from 1-5 seconds, the speed quickly accelerates IV. CONCLUSION Space vector and two-axis theory are applied to model a three-phase synchronous machine modeling for free acceleration. The dynamic model is derived and built in MAT- LAB/Simulink. Case studies demonstrate that the model can reasonably represents the free acceleration for a synchronous generator. In lab experiments, external rotor windings are applied while the excitation voltage is short cut for a synchronous machine to start up. This simulation model can accurately model the phenomenon.

5 5 x 1 1 4 5 6 7 8 1 x 1 1 4 5 6 7 8 5 x 1 1 4 5 6 7 8 ig. 8:,,. 4 ω rad/s) 1 4 5 6 7 8 x 1 N.m) 1 4 5 6 7 8 ig. 9: Speed and filtered. REERENCES [1] P. C. Krause, O. Wasynczuk, S. D. Sudhoff, and S. Pekarek, Analysis of electric machinery and drive systems. John Wiley & Sons, 1, vol. 75. [] A. R. Bergen and V. Vittal, Power systems analysis. Prentice Hall, 1999.