Inter national J our nal of P o wer Electr onics and Dri v e System (IJPEDS) V ol. 11, No. 1, March 2020, pp. 64 74 ISSN: 2088-8694, DOI: 10.11591/ijpeds.v11.i1.pp64-74 r 64 T or que ripples impr o v ement of dir ect tor que contr olled v e-phase induction motor dri v e using backstepping contr ol Hamdi Echeikh 1 , Ramzi T rabelsi 2 , Hichem K esraoui 3 , Atif Iqbal 4 , Mohamed F aouzi Mimouni 5 1,5 National Engineering School,Uni v ersity Monastir , T unisia 2 High institute of Sciences and T echnologies, Uni v ersity Sousse, T unisia 3 High Institute of T echnological Studies, Mahdia, T unisia 4 Uni v ersity of Doha, Qatar Article Inf o Article history: Recei v ed Aug 10, 2019 Re vised Oct 9, 2019 Accepted Oct 14, 2019 K eyw ords: Direct-backstepping control Direct torque control Multiphase motor Rotor flux oriented control V oltage source in v erter ABSTRA CT The paper proposes Direct T orque Control (DTC) of a v e-phase induction motor dri v e with reduced torque ripple. The me thod presented here is the DTC-Backstepping based on the classic DTC w orking with a constant switching frequenc y of the in v erter . Another remarkable aspect is the comple xity of the me thod proposed, both in the control unit of the in v erter and in the number of correctors necessary for the control of the torque. The selection table and h ysteresis ha v e been eliminated. This method significantly impro v es the torque and flux oscillations and impro v es the dynamics of the dri v e by making it less s ensiti v e to load torque di sturbances. The proposed method is de v eloped and designed using Matlab/SIMULINK to sho w the ef fecti v eness and performances of the DTC-Backstepping. This is an open access article under the CC BY -SA license . Corresponding A uthor: Hamdi Echeikh, National Engineering School of Monastir , T unisia, Rue Ibn Jazar 5000, Monastir T unisia. T el: +31624644976 Email: echeikh hamdi@hotmail.com 1. INTR ODUCTION Multiphase machines of fer an interesting alternati v e to the reduction of the stresses applied to the switches as to the windings. Indeed, the multiplication of the number of phases allo ws a fractionation of the po wer and hence a reduction of the v olta g e s switched to a gi v en current. Moreo v er , these machines reduce the amplitude and increase the frequenc y of the torque ripples, thus enabling the mechanical load to filter them more easily . Finally , the multiplication of the number of phases of fers increased reliability by allo wing operation when one or more phases are open. Multiphase machines are present in the fields of marine, rail w ay traction, petrochemical industry , a vionics, automobile, etc. The rotor flux oriented control mostly emplo yed in multiphase motor dri v es is based on ef fecti v e control of the magnetic state. Ho we v er , this structure generally requires the installation of a speed/position sensor on the shaft. Moreo v er , it remains v ery sensiti v e to the v ariations of the parameters of the machine, man y resea rch ha v e de v eloped this strate gy of control applied for multiphase machines [1-6]. Direct torque control (DTC) has been initially de v eloped for induction machines in t he years 1986 and 1988 by T AKAHASHI and DEPENBR OCK. In the literature there is an e xtensi v e research on DTC applied for multiphase machines [7-14]. In [7,12] a DTC strate gy for dual three-phase induction motor dri v es is discussed. In [8] describes an in v estig ation of direct torque control for multi-phase permanent magnet synchronous motor dri v es. A DTC for v e-phase synchronous motor has J ournal homepage: http://ijpeds.iaescor e .com Evaluation Warning : The document was created with Spire.PDF for Python.
Int J Po w Elec & Dri Syst ISSN: 2088-8694 r 65 been de v eloped in [9]. Also in [11], authors established a DTC algorithms for a split-phase induction motor . Compared to v ect or control, the DTC control is much less sensiti v e to parametric v ariations and allo ws to ob- tain dynamics f aster control. A go od accurac y in measuring the position of the rotor is not necessary since only the sector in which the flux is located matters to det ermine the configuration to be used.On the other hand, the flux and torque of the machine must be estimated or observ ed using dif ferent w ays. The synthesis of such estimators is not tri vial and constit utes a dif ficulty for the implementation of this control [15]. By nature, torque oscillations e xist in DTC dri v e. The reduction of the h ysteresis bands with a gi v en sampling period does not al w ays ha v e an ef fect on the amplitude of the torque oscillations. In this case, in order to reduce torque oscillations, it is necessary to decrease the sampling period. The switching frequenc y is not controlled, it v aries according to the operating point. DTC with constant switching frequenc y using SVPWM is reported in [16,17], ho we v er , the algorithm is more comple x, ne v ertheless, torque and flux oscillations are reduced. One find in [18], the e xtended DTC, this control uses selection table of optimal v ectors and considers an additional input: the sign of the change of electromagnetic torque. In the e xtended DTC, the torque re gulator has a three- le v el output, unlik e the con v entional DTC where only tw o le v els were considered. One can observ e a reduction in torque oscillations. In [19,20], the authors present an algorithm allo wing to ha v e a constant switching frequenc y , its main feature is the remo v al of the h ysteresis re gulators and the v ector selection table, which eliminates the problems associated with them. W ith this control method, the in v erter operates at a constant frequenc y , since a PWM technique is applied. The obje cti v e of this method is to realize a direct control of the stator flux v ector in a reference frame link ed to the stator , the polar components of these tw o v ectors are obtained by their projections on the reference frame. From these components, the desired stator flux v ector at a gi v en instant is calculated. The PWM is applied to this v ector to obtain the switching states of the in v erter . Applications using fuzzy systems ha v e been de v eloped in [21,22], where the h ysteresis blocks ha v e been replaced by fuzzy controllers.vFuzzy logic is used to achie v e a compromise between torque control and flux control, and the y do not require an e xact mathematical model of the machine. Ho we v er , it dra ws strong current pulses which normally translates into higher torque ripple. The sliding mode control (SMC), due to its rob ust- ness to uncertainties and e xternal perturbations, can be applied to uncertain and disturbed nonlinear systems. It is a question of defining a so-called sliding surf ace according to the states of the system. The synthesized global command consists of tw o terms: the first allo ws to approach this surf ace, the second allo ws the reten- tion and the sliding along it [22]. The combination of SMC and DTC control reduces torque and flux ripples. Its main feature is the remo v al of the h ysteresis re gulators and the switching table, which eliminates the prob- lems associated with them. The disadv ant age of this association (DTC-SMG)is the use of the saturation func- tion that introduces a static error that persists as well as the need to ha v e a kno wledge of the dynamics of the system. In [23], authors addresse a ne w approach to adapt the concept of the Predicti v e Control Model(MPC) to Direct T orque Control (DTC) in the v e-phase induction m otor control. The proposed algorithm impro v es the performance of a DTC controller by retaining the electromagnetic torque and the stator flux modulus within predefined h ysteresis bands while minimizing switching losses. The MPC controller e xtracts the strings of switching sequences on the forecast horizon. Dynamic programming is impl emented to select the switching sequences that minimize the cost function on po wer losses. Both simulations and e xperimental are carried out on specific models and the results v erify the adv antages of the proposed DTC method in comparison with con v entional DTC. Model-based predicti v e direct control methods are adv anced control strate gies in the field of po wer electronics to control induction machines [24]. The torque control prediction (PTC) method e v aluates the electromagnetic torque and the stator flux in the cost function. The switching v ector selected for use in insu- lated g ate bipolar transistors (IGBT) which minimizes error between references and predicted v alues. System constraints can be easily understood.Beha vior and rob ustness and transient performance are e v aluated. Due to the incon v enient of the DTC control s uch as high torque and currents ripples push us to think and to design ne w control to impro v e the direct torque control technique. The idea in this paper is to use the combination between the DTC control and a non-linear control in this paper is the Backstepping control. As the authors kno w there is no study in the literature treated this approac h applied to the multiphase motor and specially v e-phase induction motor . 2. DTC-B A CKSTEPPING CONTR OL OF FIVE-PHASE INDUCTION MO T OR The induction motor dri v e system used to de v elop the proposed controller strate gy is composed m ainly of v e-phase v oltage source in v erter and a symmetrical v e-phase induction motor with phase shift of the windings equal to 2 /5. All the components of the dri v e system are schematica lly illustrated in the Figure 1. T or que ripples impr o vement of dir ect tor que ... (Hamdi Ec heikh) Evaluation Warning : The document was created with Spire.PDF for Python.
66 r ISSN: 2088-8694 Using v arious assumptions, such as ne gligible core losses, uniform air g ap, sinusoidal MMF distrib ution and symmetrical distrib uted windings, then the v e-phase induction motor model using the v ector space decom- position method presented in [25]. The model re presented in tw o orthogonal planes, where the first plane is in v olv ed in the fundamental torque production ( representing the fundamental component and contains the harmonics of order 10 n 1 ; n = 0 ; 1 ; 2 ; 3 ...). The second plane is connected to the losses in the motor ( x y represented the supply harmonics of the order 10 n 3 ; n = 0 ; 1 ; 2 ; 3 ...). Finally , the zero-sequence component is not considered due to the neutral point isolat ion isolation( z -axis representing the supply harmonics of order 5 n; n = 0 ; 1 ; 2 ; 3 ...). Using the selection of the stator currents in tw o planes and x y and the rotor flux es in the plane as state v ariables, x 1 = i s , x 2 = i s , x 3 =   r , x 4 =   r , x 5 = i sx and x 6 = i sy . The motor dri v e equations can be e xpressed in the follo wing form 8 > > > > > > > > > > < > > > > > > > > > > : _ x 1 = c 1 x 3 + c 2 ! x 4 c 3 x 1 + c 4 v 1 _ x 2 = c 1 x 4 c 2 ! x 3 c 3 x 2 + c 4 v 2 _ x 3 = c 5 x 3 ! x 4 + c 6 x 1 _ x 4 = c 5 x 4 + ! x 3 + c 6 x 2 _ x 5 = c 7 x 5 + c 8 v 3 _ x 6 = c 7 x 6 + c 8 v 4 _ ! = m 1 ( x 3 x 2 x 4 x 1 ) m 2 T l m 3 ! (1) W ith the coef ficients gi v en by c 1 = (1 ) M r ; c 2 = (1 ) M ; c 3 = ( 1 s + (1 ) r ) ; c 4 = 1 L s ; c 5 = 1 r ; c 6 = M r ; c 7 = R s L ls ; c 8 = 1 L ls = 1 M 2 L s L r ; s = L s R s ; r = L r R r ; m 1 = P 2 M J m L r ; m 2 = P J m ; m 3 = B m J m The inputs signals of system abo v e are the applied stator v oltages v 1 = v s ; v 2 = v s ; v 3 = v sx and v 1 = v sy . The equations represent the electrical speed ! and all the motor parameters, M is the mutual inductance, R s is the stator resistance, R r the rotor resistance, L r is the rotor inductance, L s is the stator inductance and L l s is the stator leakage inductance. One presented a no v el state v ariables to describe the no v el model to de v eloped the DTC-Backstepping controller , ho we v er , the separation of the model of v e- phase induction motor is released into tw o dif ferent parts, mechanical part and electrical part, the ne w state v ariables are gi v en as follo ws 8 > < > : T v =   r i s   r i s = x 3 x 2 x 4 x 1   v = 1 2 ( x 2 3 + x 2 4 ) X v = x 3 x 1 + x 4 x 2 (2) Where T v is a virtual torque, the relation between the electromagnetic torque and the virtual torque is T em = m 1 T v .   v is virtual flux, the relation between the rotor flux and the virtual flux is   v =   2 r , where   2 r =   2 r +   2 r . In practice the components   r and   r are deri v ed from the v e-phase induct ion motor v oltage model or current model gi v en by (   s = R ( v s R s i s ) dt   s = R ( v s R s i s ) dt (3) The rotor flux can be deri v ed as follo wing (   r = L r (   s L s i s )   r = L r (   s L s i s ) (4) The v e-phase induction motor model can be separated into electrical and mechanical parts using t he ne w state v ariables gi v en abo v e, the mechanical part is _ ! = m 1 T v m 2 T l m 3 ! (5) Int J Po w Elec & Dri Syst, V ol. 11, No. 1, March 2020 : 64 74 Evaluation Warning : The document was created with Spire.PDF for Python.
Int J Po w Elec & Dri Syst ISSN: 2088-8694 r 67 The deri v ati v e of the virtual torque is gi v en by _ T v = _ x 3 x 2 + x 3 _ x 2 _ x 4 x 1 x 4 _ x 1 (6) Replacing the deri v ati v e x 1 ; x 2 ; x 3 and x 4 from equation (1) one obtain: _ T v = ( c 3 + c 5 )( x 3 x 2 x 4 x 1 ) ! ( x 3 x 1 + x 4 x 2 ) c 2 ! ( x 2 3 + x 2 4 ) + c 4 ( x 3 v 2 x 4 v 1 ) (7) Using equation (2), the equation (7) can be re written as _ T v = ( c 3 + c 5 ) T v ! X v 2 c 2 !   v + c 4 u T (8) Where u T = x 3 v 2 x 4 v 1 =   r v s   r v s The deri v ati v e of the virtual rotor flux   v gi v es: _   v = _ x 3 x 3 + _ x 4 x 4 (9) Using equation (1), equation (9) can be re written as _   v = c 5 ( x 2 3 + x 2 4 ) + c 6 ( x 3 x 1 + x 4 x 2 ) (10) Using equation (2), equation (10) becomes _   v = c 5 X v + c 6   v (11) The deri v ati v e of X v gi v es as follo ws _ X v = _ x 3 x 1 + x 1 _ x 3 + _ x 4 x 2 + x 4 _ x 2 (12) Using the equation (1), equation (12) becomes: _ X v = ( c 3 + c 5 )( x 3 x 1 + x 4 x 2 ) + ! ( x 3 x 2 x 4 x 1 ) + c 6 ( x 2 1 + x 2 2 ) + c 1 ( x 2 3 + x 2 4 ) + c 4 ( x 3 v 1 + x 4 v 2 ) (13) Replacing the e xpressions of equation (2) in equation (13), one obtains: _ X v = ( c 3 + c 5 ) X v + ! T v + c 6 ( x 2 1 + x 2 2 ) + 2 c 1   v + c 4 u   (14) Where u   = x 3 v 1 + x 4 v 2 =   r v 1 +   r v 2 Indeed, for the mechanical part, the virtual torque T v is controlled with a virtual torque v oltage u T and for the electrical part, the virtual rotor flux   v is controlled by the virtual rotor flux v oltage u   . This will simplify the design of the DTC-backstepping controller in the follo wing section based on the mechanical and electrical parts. One design by ! the electrical motor speed reference, the speed error is gi v en by: z 1 = ! ! (15) The deri v ati v e of speed error can be re written as _ z 1 = _ ! _ ! = _ ! m 1 T v + m 2 T l + m 3 ! (16) Choosing the deri v ati v e of the error _ z 1 = k 1 z 1 where k 1 is a positi v e constant. One can get the reference of the virtual torque T v as T v = ( _ ! + m 2 T l + m 3 ! + k 1 z 1 ) =m 1 (17) The error of the virtual torque gi v es by z 2 = T v T v , the deri v ati v e of z 2 gi v es in equation (18). _ z 2 = _ T v _ T v = _ T v + ( c 3 + c 5 ) T v + ! X v + 2 c 2 !   v c 4 u T (18) Choosing the deri v ati v e of the error _ z 2 = k 2 z 2 , one can get the virtual torque v oltage u T as u T = ( _ T v + ( c 3 + c 5 ) T v + ! X v + 2 c 2 !   v + k 2 z 2 ) =c 4 (19) Using equation (17) the equation (19) can be re written as u T = (( ! + m 2 _ T l + m 3 _ ! k 2 1 z 1 ) =m 1 + ( c 3 + c 5 ) T v + ! X v + 2 c 2 !   v + k 2 z 2 ) =c 4 (20) T or que ripples impr o vement of dir ect tor que ... (Hamdi Ec heikh) Evaluation Warning : The document was created with Spire.PDF for Python.
68 r ISSN: 2088-8694 Finally , replacing the e xpression of _ ! from equation (1), the e xpression of the virtual v oltage u T gi v en as follo ws u T = (( ! + m 2 _ T l m 3 m 2 T l m 2 3 ! k 2 1 z 1 + m 1 ( m 3 + c 3 + c 5 ) T v ) =m 1 + ! X v + 2 c 2 !   v + k 2 z 2 ) =c 4 (21) One assume that the virtual rotor flux of the v e-phase induction motor gi v en by   v , then its error is gi v en by: z 3 =   v   v (22) The dynamic of the error of the virtual rotor flux is gi v en by the follo wing equation: _ z 3 = _   v _   v = _   v + 2 c 5   v c 6 X v (23) Choosing the dynamic of the error _ z 3 = k 3 z 3 , one obtains the virtual control X v as: X v = ( _   v + 2 c 5   v + k 3 z 3 ) =c 6 (24) Let is no w define the error of the virtual control X v as: z 4 = X v X v (25) Its dynamic error is gi v en by: _ z 4 = _ X v _ X v (26) Using equation (14), equation (26) becomes _ z 4 = _ X v + ( c 3 + c 5 ) X v ! T v c 6 ( x 2 1 + x 2 2 ) 2 c 1   v c 4 u   (27) Choosing the dynamic of the error _ z 4 = k 4 z 4 , where k 4 is a positi v e constant, then the virtual rotor flux u   obtains as u   = ( _ X v + ( c 3 + c 5 ) X v ! T v c 6 ( x 2 1 + x 2 2 ) 2 c 1   v + k 4 z 4 ) =c 4 (28) Using equation (24), one can re write the equation (28) as u   = ((   v + 2 c 5 _   v k 2 3 z 3 ) =c 6 + ( c 3 + c 5 ) X v ! T v c 6 ( x 2 1 + x 2 2 ) 2 c 1   v + k 4 z 4 ) =c 4 (29) Replacing the e xpression of _   v gi v es by equation (11) in equation (29), one obtains u   = ((   v + 2 c 5 ( 2 c 5   v + c 6 X v ) k 2 3 z 3 ) =c 6 + ( c 3 + c 5 ) X v ! T v c 6 ( x 2 1 + x 2 2 ) 2 c 1   v + k 4 z 4 ) =c 4 (30) From the tw o virtual v oltages, bot h for torque and ux, one can acquire the stator v oltages in the ( ) frame. ( v 1 = v s = ( x 3 u   x 3 u T ) = 2   v v 2 = v s = ( x 4 u   + x 3 u T ) = 2   v (31) No w , One need to determinate the control v oltages v 3 and v 4 , then one define the follo wing current errors z 5 and z 6 ( z 5 = i sx i sx = i sx x 5 z 6 = i sy i sy = i sy x 6 (32) The dynamic of the currents errors z 5 and z 6 gi v en as follo w ( _ z 5 = _ i sx _ i sx = _ i sx _ x 5 _ z 6 = _ i sy _ i sy = _ i sy _ x 6 (33) Choosing the deri v ati v e of the errors _ z 5 = k 5 z 5 and _ z 6 = k 6 z 6 , the stator v oltages in the reference ( x y ) obtained in the follo wing equation ( v 3 = v sx = ( _ i sx c 7 x 5 + k 5 z 5 ) =c 8 v 4 = v sy = ( _ i sy c 7 x 6 + k 6 z 6 ) =c 8 (34) Int J Po w Elec & Dri Syst, V ol. 11, No. 1, March 2020 : 64 74 Evaluation Warning : The document was created with Spire.PDF for Python.
Int J Po w Elec & Dri Syst ISSN: 2088-8694 r 69 3. ST ABILITY AN AL YSIS Usually it is dif ficult to find the asymptotic stability of time-v arying systems because it is v ery dif ficult to find L yapuno v functions with a ne g ati v e definite deri v ati v e. W e kno w in case of autonomous (time in v ariant) systems, if V is ne g ati v e semi-definite, then it is possible to kno w the asymptotic beha viors by in v oking in v ariant-set theorems. Ho we v er , the fle xibility is not a v ailable for time-v arying systems. This is where Babarlat’ s lemma comes into picture. 3.1. Lemma: Barbalt’ s Lemma Suppose f ( t ) 2 C 1 ( a; 1 ) and lim t !1 f ( t ) = where < 1 . If f 0 is uniformly continuous, then lim t !1 f 0 ( t ) = 0 . 3.2. Pr oof One will pro v e the result by contradiction. lim t !1 f ( t ) 6 = 0 . Then 3 > 0 and a monotone increasing sequence t n such that t n ! 1 as n ! 1 and j f 0 ( t ) j for all n 2 N . Since f 0 ( t ) is uniformly continuous, for such , 3 > 0 such that 8 n 2 N . j t t n j < )j f 0 ( t ) f 0 ( t n ) j "= 2 Hence if t 2 [ t n ; t n + ] then j f 0 ( t ) j = j f 0 ( t n ) ( f 0 ( t n ) f 0 ( t )) j j f 0 ( t ) j j f 0 ( t n ) f 0 ( t ) j = 2 = = 2 Then since f ( t ) 2 C 1 one ha v e j Z t n + a f 0 ( t ) dt Z t n a f 0 ( t ) dt j = j Z t n + t n f 0 ( t ) dt j Z t n + t n j f 0 ( t ) j dt Z t n + t n = 2 dt = = 2 Ho we v er lim t !1 j Z t n + a f 0 ( t ) dt Z t n a f 0 ( t ) dt j = lim t !1 j f ( t n + ) f ( t n ) j = j lim t !1 f ( t n + ) lim t !1 f ( t n ) j = j j j j = 0 This is a contradiction. Therefore lim t !1 f 0 ( t ) = 0 3.3. A pplication of the Lemma One assume the L yapuno v function is V = z 2 1 + z 2 2 + z 2 3 + z 2 4 + z 2 5 + z 2 6 2 (35) The deri v ati v e of the L yapuno v function gi v en by _ V = z 1 _ z 1 + z 2 _ z 2 + z 3 _ z 3 + z 4 _ z 4 + z 5 _ z 5 + z 6 _ z 6 = k 1 z 2 1 k 2 z 2 2 k 3 z 2 3 k 4 z 2 4 k 5 z 2 5 k 6 z 2 6 (36) From equation (36), one ha v e _ V k 1 z 2 1 , then V (0) V ( 1 ) Z 1 0 k 1 z 2 1 dt (37) V is bounded. According to Barbalat’ s lemma one can ha v e lim t !1 z 1 = 0 (38) Also, one can ha v e lim t !1 z 2 = lim t !1 z 3 = li m t !1 z 4 = lim t !1 z 5 = lim t !1 z 6 = 0 (39) At last, according equations (38) and (39), one can notice that motor speed , torque and rotor flux can track reference v alues asymptotically . T or que ripples impr o vement of dir ect tor que ... (Hamdi Ec heikh) Evaluation Warning : The document was created with Spire.PDF for Python.
70 r ISSN: 2088-8694 4. SIMULA TIONS RESUL TS AND DISCUSSION DTC-Backstepping control system block diagram is sho wn in Figure 1. Whene v er the reference speed command ! is gi v en, system compares it with the actual speed ! . The error is used to determine the virtual reference torque T . The reference virtual torque is compared with actual t orque T . The torque err o r obtained is used to obtain the appropriate virtual v oltage v ector u T . The second reference input that is ux compare with actual flux. The error added to determinate the virtual control X . Lik e torque control loop, flux control loop is also operated to select the appropriate virtual v oltage v ector u   . Ho we v er , After the determination of the t w o virtual v ol tage v ectors which used t o obtain t h e actual v ol tage v ectors ( ) . The tw o other v oltage v ectors ( x y ) are obtains from a small loop current controller . A program in Matlab/Simulink en vironment has been d e signed for both the v oltage source in v erter (VSI)-fed v e-phase induction machine, and performed to analyze the viability of the de v eloped control technique a number of simulations ha v e been performed. A small prototype around 1.5 kW symmetrical v e-phase induction machine with four poles has been used. T able 1 sho ws the parameters of the machine, which correspond to those of the real v e-phase induction machine. ! ! z 1     T T z 3 z 2   r  u T u   !   z 4 i s v s v sabcde   X T   r  i s i sabcde i s v s X X   s V dc 5 S i i sabcde ! Computing of reference v oltages Computing of reference torque Computing of v oltages virtual Computing of reference para virtual Computing of paras Rotor flux Computing Stator flux Computing Svpwm Lar ge Medium V ectors [ C ] 1 [ C ] Figure 1. Scheme of Direct torque Backstepping Control of v e-phase Induction Motor T able 1. P arameters of the v e-phase Induction Machine Motor Data P arameters Symbol V alue Units Stator resistance R s 10 Rotor resistance R r 6.3 Mutual Inductance M 0.42 H Stator leakage inductance L ls 0.04 H Rotor leakage inductance L lr 0.04 H Moment of inertia J m 0.03 k g :m 2 Stator inductance L s 0.46 H Rotor inductance L r 0.46 H Number of pole pairs P 2 - Rated stator flux   n 1.27 Wb Int J Po w Elec & Dri Syst, V ol. 11, No. 1, March 2020 : 64 74 Evaluation Warning : The document was created with Spire.PDF for Python.
Int J Po w Elec & Dri Syst ISSN: 2088-8694 r 71 Figures 2 and 3 summarize the simulation results. A start-up transient under no-load condi tions, with speed references re v ersion from 400 rpm/min to -400 rpm, is considered, and the motor -speed, electromagnetic-torque, stator -flux, and stator -current responses and the torque ripple are sho wn for both methods (DTC and DTC-Backstepping). The obtained speed response using the DTC-Backstepping method is quick er than that using the DTC method, while the settling time is practically the same. By using DTC- Backstepping technique, torque ripples is reduced from 2.5 N.m to1.2 N.m as sho wn in figure.3. Hence torque ripple is reduced by 52%. Flux ripple is reduced from 0.1 Wb to 0.01 Wb as sho wn in figure.3. Therefore flux ripple is reduced by 90%. It is observ ed that the DTC-Backstepping which based on non-linear approach allo ws ef fecti v ely to reduce torque ripple as well as flux ripple. From the simulation figures, it can be concluded that torque and flux direct backstepping control has small torque, speed , flux and current ripple. T orque and flux direct backstepping control ha v e better performance than classical direct torque control. The scheme can not only a v oid the ef fect of rotor resist ance to rotor flux ori entation, b ut also reduce ef fect of h ysteresi s to torque and flux. From simulation results, one vie w that system design can achie v e direct torque and flux control and motor speed tracking performance i s better than classical direct torque control. The control scheme can realize system state v ariable decoupling ef ficiently . 0 , 0 0 , 2 0 , 4 0 , 6 0 , 8 1 , 0 - 4 0 0 - 2 0 0 0 2 0 0 4 0 0 0 , 0 0 , 2 0 , 4 0 , 6 0 , 8 1 , 0 - 4 0 0 - 2 0 0 0 2 0 0 4 0 0 T i m e   ( s )   w *   w M o t o r   s p e e d   ( r p m ) T i m e   ( s )   w *   w M o t o r   s p e e d   ( r p m ) 0 , 0 0 , 2 0 , 4 0 , 6 0 , 8 1 , 0 - 1 0 - 5 0 5 1 0 0 , 0 0 , 2 0 , 4 0 , 6 0 , 8 1 , 0 - 1 0 - 5 0 5 1 0 T i m e   ( s )   T e m T o r q u e   ( N . m ) T i m e   ( s )   T e m T o r q u e   ( N . m ) 0 , 0 0 , 2 0 , 4 0 , 6 0 , 8 1 , 0 0 , 0 0 , 3 0 , 6 0 , 9 1 , 2 1 , 5 0 , 0 0 , 2 0 , 4 0 , 6 0 , 8 1 , 0 0 , 0 0 , 3 0 , 6 0 , 9 1 , 2 1 , 5 T i m e   ( s )   s S t a t o r   f l u x   ( w b ) T i m e   ( s )   s S t a t o r   f l u x   ( w b ) 0 , 2 0 , 4 0 , 6 0 , 8 1 , 0 - 1 0 - 5 0 5 1 0 0 , 2 0 , 4 0 , 6 0 , 8 1 , 0 - 1 0 - 5 0 5 1 0 T i m e   ( s )   i s a   i s b S t a t o r   c u r r e n t s   i n   ( a - b )   p l a n e   ( A ) T i m e   ( s )   i s a   i s b S t a t o r   c u r r e n t s   i n   ( a - b )   p l a n e   ( A ) Figure 2. Motor speed,torque, stator flux and currents left side DTC and right side DTC-backstepping T or que ripples impr o vement of dir ect tor que ... (Hamdi Ec heikh) Evaluation Warning : The document was created with Spire.PDF for Python.
72 r ISSN: 2088-8694 - 1 , 4 - 0 , 7 0 , 0 0 , 7 1 , 4 - 1 , 4 - 0 , 7 0 , 0 0 , 7 1 , 4 - 1 , 4 - 0 , 7 0 , 0 0 , 7 1 , 4 - 1 , 4 - 0 , 7 0 , 0 0 , 7 1 , 4 S t a t o r   f l u x   r e v o l u t i o n   S t a t o r   f l u x   r e v o l u t i o n 0 , 1 3 5 0 0 , 1 3 5 5 0 , 1 3 6 0 0 , 1 3 6 5 0 , 1 3 7 0 0 , 1 3 7 5 0 , 1 3 8 0 4 5 6 7 0 , 1 3 5 0 0 , 1 3 5 5 0 , 1 3 6 0 0 , 1 3 6 5 0 , 1 3 7 0 0 , 1 3 7 5 0 , 1 3 8 0 4 5 6 7 T i m e   ( s )   Z o o m   T e m T o r q u e   r i p p l e s   ( N . m ) T i m e   ( s )   Z o o m   T e m T o r q u e   r i p p l e s   ( N . m ) 0 , 1 3 5 0 0 , 1 3 5 5 0 , 1 3 6 0 0 , 1 3 6 5 0 , 1 3 7 0 0 , 1 3 7 5 0 , 1 3 8 0 1 , 2 0 1 , 2 2 1 , 2 4 1 , 2 6 1 , 2 8 1 , 3 0 1 , 3 2 1 , 3 4 0 , 1 3 5 0 0 , 1 3 5 5 0 , 1 3 6 0 0 , 1 3 6 5 0 , 1 3 7 0 0 , 1 3 7 5 0 , 1 3 8 0 1 , 2 0 1 , 2 4 1 , 2 8 1 , 3 2 1 , 3 6 T i m e   ( s )   Z o o m   s S t a t o r   f l u x   r i p p l e s   ( w b )   T i m e   ( s )   Z o o m   s S t a t o r   f l u x   r i p p l e s   ( w b ) Figure 3. Stator flux re v olution, torque and flux ripples, left side DTC and right side DTC-backstepping 5. CONCLUSION This paper separates induction motor into mechanical part and electrical part. Backstepping coupling is applied to realize torque and flux decoupling. This can reduce the couple between state v ariable, and can mak e speed, torque and flux f ast track reference v alues. System design is based on static coordinate of stator . The control scheme synthesize the direct torque and v ector control, which not only realizes torque and rotor flux direct control, b ut also ha v e the little torque and rotor flux ripple. Backstepping control design can not only pro vide better speed, torque and flux tracking performance, b ut also assert system rob ust performance under speed re v ersal. Moreo v er , the torque and flux are respecti v ely reduced by 52% and 90%. REFERENCES [1] M. Bermudez, I. Gonzal ez-Prieto, F . Barrero, H. Guzman, M. J. Duran, and X. K estelyn, ”Open-phase f ault-tolerant direct torque control technique for v e-phase induction motor dri v es, IEEE T ransactions on Industrial Electronics , v ol. 64, pp. 902–911, Feb 2017. [2] H. Guzman, M. J. Duran, F . Barrero, B. Bog ado, and S. T oral, ”Speed control of v e-phase induction mo- tors with inte grated open-phase f ault operation using model-based predicti v e current control techniques, IEEE T ransactions on Industrial Electronics , v ol. 61, pp. 4474–4484, Sept 2014. [3] H. Guzman, F . Barrero, and M. J. Duran, ”Igbt-g ati ng f ailure ef fect on a f ault-tolerant predicti v e current- controlled v e-phase induction motor dri v e, IEEE T ransactions on Industrial Electronics , v ol. 62, pp. 15–20, Jan 2015. [4] H. Guzman, M. J. Duran, F . Barrero, L. Zarri, B. Bog ado, I. G. Prieto, and M. R. Arahal, ”Comparati v e study of predicti v e and resonant controllers in f ault-tolerant v e-phase induction motor dri v es, IEEE T ransactions on Industrial Electronics , v ol. 63, pp. 606–617, Jan 2016. [5] C. Mart ın, M. R. Arahal, F . Barrero, and M. J. Dur ´ an, ”Fi v e-phase induction motor rotor current observ er for finite control set model predicti v e control of stator current, IEEE T ransactions on Indus- trial Electronics , v ol. 63, pp. 4527–4538, July 2016. Int J Po w Elec & Dri Syst, V ol. 11, No. 1, March 2020 : 64 74 Evaluation Warning : The document was created with Spire.PDF for Python.
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