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        High-order sliding mode control of a doubly salient permanent magnet machine driving marine current turbine

        2021-05-21 02:43:28HoChenShifengTngJingngHnTinhoTngNiAhmeZhiinZhouMohmeBenouzi

        Ho Chen ,,Shifeng Tng ,Jingng Hn ,Tinho Tng ,Ni A?t-Ahme ,Zhiin Zhou ,Mohme Benouzi ,

        a The Institute of Power Drive and Control,Shanghai Maritime University,201306,Shanghai,China

        b Institut de Recherche en Energie Electrique de Nantes Atlantique,University of Nantes,44602,Saint-Nazaire,France

        c ISEN Yncréa Ouest,University of Brest,FRE CNRS 3744 IRDL,29200,Brest,France

        d University of Brest,UMR CNRS 6027 IRDL,29238,Brest,France

        Abstract Due to the harsh and changeable marine environment,one low speed stator-permanent magnet machine named doubly salient permanent magnet machine with toothed pole is applied for marine current energy conversion system.Indeed,this machine has simple structure,intriguing fault tolerance,and higher power density,which could adequately satisfy the different complicated operation conditions.However,its permanent magnet flux-linkage has the same variation period as the inductance which leads to a strong nonlinear coupling system.Moreover,the torque ripple caused by this special characteristics,uncertainty of system parameters and disturbance of load greatly increases the difficulty of control in this strongly coupling system.Consequently,the classical linear PI controller is difficult to meet the system requirement.In this paper,the high-order sliding mode control strategy based on the super-twisting algorithm for this system is creatively utilized for the first time.The stability of the system within a limited time is also proved with a quadratic Lyapunov function.The relative simulation results demonstrate convincingly that,the high-order sliding mode control has little chattering,high control accuracy and strong robustness.

        Keywords:Doubly salient permanent magnet machine;Torque ripple;Chattering;High-order sliding mode control;Super-twisting algorithm.

        1.Introduction

        In recent years,the fossil energy is gradually exhausted due to the acceleration of the global industrialization process.Meanwhile,the environmental pollution caused by the extensive use of fossil energy becomes more and more serious.Consequently,the renewable energy has attracted widespread attention during the past decades.Nowadays,both the efficiency and dependability of the renewable energy technologies have been continuously enhanced [1–4].According to the statistics,the estimated renewable energy accounted for 24.5% of the global generation of electricity by the end of 2017,while this value approximately reached up to 26.5%in 2018 [5].Among the various renewable energies,ocean energy becomes more and more interesting due to its abundant energy reserves.Unfortunately,among various forms of ocean energy,only marine current energy appears the enormous commercial value considering its high energy density,strong predictability and similar technologies to the mature Wind Energy Conversion System (WECS) [6,7].Even for the marine current energy,there is approximated 50 GW or 180 TWh annually of the economically exploitable resource worldwide [1].Thus,the utilization of the marine current energy will certainly mitigate the energy crisis to a certain extent.

        The generator,the main component of Marine Current Energy Conversion System (MCECS) to transform the mechanical energy into the electrical energy,must be considered cautiously.Normally,the low marine current speed results in relatively low rotation speed of the turbine.An external gearbox is always demanded to achieve relative high machine rotor speed.However,it will inevitably bring the relative high failure rate and increase the difficulties of the maintenance in the harsh working environment.Consequently,the direct drive MCECS with low speed machine is preferred [8].The application of the conventional generators such as Permanent Magnet Generator (PMG),Induction Generator (IG)and Doubly-Fed Induction Generator (DFIG) has been greatly limited in virtue of this reason.In this paper,one low speed stator-Permanent Magnet (PM) machine:toothed pole Doubly Salient Permanent Magnet (DSPM) machine (50 rpm,10 kW)is proposed.This kind machine employs the magnets in the stator and can decouple of the frequency from the pole pair[9].In addition,the forward,reverse and four-quadrant operation of this machine can be easily realized by changing the order of the inverter conduction phase and the sense of winding current.Accordingly,the DSPM machine is quite suitable for the frequent start-stop,acceleration and deceleration occasions including marine current power generation and ship propulsion.

        However,due to its special structure,the back-Electromotive Force (back-EMF) has the same variation as the inductance which would bring big torque ripple even with conventional sinusoidal current waveform.This torque ripple would degrade the performance of the transmission system and even cause the shafting oscillation to endanger the mechanical device.Moreover,this toothed pole DSPM machine is difficult to control by the conventional linear controllers because of the nonlinear dynamic model.Therefore,it is of great significance to study the current waveform and corresponding control methods of this special machine..In Ref.[10],the causes of torque ripple are firstly analyzed in detail;then,the switching angle adjustment method and rotor skew slot technology are proposed to reduce the ripple.Nevertheless,this control method needs to confirm the conduction angle which will make the control mode more complex.The skew technology needs to change the structure of the machine which increases the cost.In Ref.[11],the maximum torque and torque pulsation are reduced by optimizing the turn-on and turn-off angles and reducing the number of conducting phases.However,the output torque is also reduced.In Ref.[12]and Ref.[13],they propose the forward commutation method.This method can reduce the commutation torque ripple by changing the current rising time.Neverthless,the advance angle is not easy to determine.In Ref.[14],a variable parameter PI controller based on a single-chip TMS320F28335 is proposed.The current loop,as well as the voltage loop,employs gain-scheduled PI controller based on the linearized model of the DSPM machine.Unfortunately,this simplified linear system cannot achieve precise control results.In Ref.[9]and Ref.[15],they propose one complex quasi-sinusoidal current waveform to diminish the torque ripple and one First-Order Sliding Mode Control (FOSMC) to deal with the nonlinear model.However,the mathematical current formula highly depends on the parameters of the DSPM machine.Meanwhile,FOSMC will undoubtedly bring the chattering which may also bring the torque ripple.Actually,the chattering is the inherent phenomenon of Sliding Mode Control (SMC) and is mainly due to the discontinuous switch character in essence of this control.

        For the sake of decreasing the torque ripple and increasing the robustness,one High-Order Sliding Mode Control (HOSMC) strategy based on Super-Twisting Algorithm(STA) is adopted for this toothed pole DSPM machine-based MCECS in this paper.This paper is structured as follows:the partially typical model of MCECS is established in Section 2,including the marine current resource,turbine and DSPM machine;in Section 3,HOSMC strategy based on STA,which has great robustness and convergence rapidity,is introduced and optimized for the DSPM machine;subsequently,a quadratic Lyapunov function is used to prove stability of the whole control system within a limited time;Section 4 deals with the simulation and analysis in different situations;eventually,a conclusion is given in Section 5.

        2.Marine current turbine modeling

        The global scheme of MCECS is very similar with that of WECS.Ordinarily,the global scheme of MCECS contains some essential components:the resource,the marine turbine,the generator,the transformer and the grid-connected converter (Fig.1).When the turbine blades are driven by the marine current,a lift perpendicular to the direction of the flow is produced.This continuous force makes the turbine rotate.Sebsequently,the generator is driven by the mechanical transmission structure and generates electricity under the control of the inverter.

        For the MCECS,an appropriate model for the marine current resources is required firstly.Many researchers have developed several different models of the marine current speed to assess their potential energy.One first-order model provided by SHOM (Service Hydrographique et Océanographique de la Marine,France) is adopted in this part due to the remarkable reliability and simplicity [18].The tidal current velocityVtideis given by Eq.(1).

        Where:Cis the tide coefficient;95 and 45 are mean spring tide and neap tide medium coefficients according to experimental research respectively;VntandVstare the hourly intervals neap and spring tide current velocities.

        According to the model above,the marine current velocity data in Penmarc’h,France is shown in Fig.2.From this figure,the maximum value of the absolute velocity of flow does not exceed 3.5 m/s.The available mechanical powerPmecof the marine current turbine,extracted from the fluid is expressed by the following Eq.(2) [19,20].

        Where:Phydis the hydrodynamic power;ρis the density of the ocean (1024 kg/m3);Ais the cross section of the turbine (m2);Vtideis the current velocity (m/s);Cpis the power coefficient.

        Fig.1.Global scheme of MCECS [16,17].

        Fig.2..Marine current velocity.

        Fig.3..DSPM machine structure.

        In order to meet nominal operation condition,the power coefficientCpof marine current turbine is limited with the restriction as Eq.(3) [15].

        Where:λis the Tip Speed Ratio;ηis the system mechanical losses percentage;ωmis the mechanical speed (rad/s).

        As described in the introduction,this toothed pole DSPM machine is accepted by MCECS due to its prominent advantages and simple maintenance considerations.This machine has been already designed and optimized to achieve the maximum volume torque,with a maximum torque of 45.5 kNm/m3.The stator of this machine has four non-rotating PM,48 teeth and 12 slots;while the rotor only contains 64 teeth[21].Some more details of this DSPM machine design can be found in Ref.[22].The simplified structure of this DSPM machine is shown in Fig.3.

        Actually,the establishment of the dynamic mathematical model needs to consider a number of factors.According to the previous model analysis in Ref.[23],some assumptions are required to simplify the analysis.A dynamic park model of the DSPM machine in d-q frame is derived with the Concordia and Park transformations and presented in the following Eqs.(4) –(6) [15].

        Where:Ld,qrepresents the model of stator inductance based on d-q coordinate;Mdqis the mutual inductance;TmandTemare mechanical torque and electromagnetic torque;θeis the electrical angle;ωeis the electrical angular velocity;Jmandfare rotary inertia and viscosity coefficient,respectively;Nris the number of rotor teeth.

        3.Control strategies

        It is generally true that the classical linear controllers including the PI and PID are very suitable for the linear timeinvariant system.However,as for this toothed pole DSPM machine,it is a typical non-linear system.Even for the sinusoidal current waveform,the PI controllers cannot effectively make the speed and current tracking error within the allowable range.Moreover,for the appropriate current waveform which contains certain harmonics to reduce the torque ripple,it would undoubtedly make the input complicated and increase the difficulties in control [9,15].Furthermore,the system usually needs to operate at different states with variable input and load due to the harsh underwater working environment.Consequently,a robust controller is extremely beneficial to these problems.It is recognized that SMC is a prominent method of nonlinear control.It is widely used in many fields owing to its great robustness and fast convergence to external interference and internal parameter variations.

        3.1. Introduction of HOSMC

        Essentially,the principle of SMC is to force the trajectories of desired plant states onto some predesigned sliding surfaces by discontinuous controls.FOSMC is intensely easy to design and possesses certain robust performance.However,the application of FOSMC is hindered by the chattering phenomenon due to the multifarious inertia,which might lead to high-frequency vibration of the system.Thus,HOSMC appears subsequently.According to the theory proposed by Arie Levant,the sliding sets=s˙=¨s=...=s(r?1)=0 on sliding mode surfaces(t,x)=0 is non-empty and consists of Filippov trajectories of discontinuous dynamic systems.Then,the relevant motion satisfying this condition is called the “r-order sliding mode’’ with respect to the sliding mode surface (r≥2).HOSMC extends the idea of traditional sliding mode.It does not apply the discontinuous control variable to the first derivative of the sliding modulus,but applies it to the higher-order derivative.This not only retains the advantages of FOSMC,but also significantly reduces chattering [24,25].At present,the Second-Order Sliding Mode Control (SOSMC) is widely accepted and supported by the theory [26–28].Moreover,it is the most frequently applied HOSMC which has simple structure and little requirement of target information.In order to establish the controller based on HOSMC appropriately,the modeling process is explained by the following content.

        By treating the DSPM machine control system as a controlled dynamic system,the control objectives can be handled more easily..The state equation of a single input nonlinear dynamic system is defined as the Eq.(8).

        Where:xis the system state variables;uis the control input;f(x,t) andg(x,t) are both smooth uncertain continuous functions.

        It is worthwhile to design a suitable sliding surface,which is necessary to construct a feasible SMC.Firstly,the state variables of the DSPM machine should be defined as the Eq.(9).

        Where:xrefis the reference value;xis the actual measurement.

        Next,the sliding surface is designed under the utilization of system variablesx1andx2as shown in the Eq.(11).

        Then,the derivation of the Eq.(11) can be obtained in the following Eq.(12) in combination with the Eqs.(5) - (9).

        Where:sω,sdandsqare sliding mode surfaces of the speed and current controllers respectively;x1ω,x1dandx1qare the tracking errors of the speed and current controllers respectively.

        It is also essential to set up an initial integral value which is given in the Eq.(13).The system trajectory can be quickly transferred to the sliding surface (s=0) even at the initial time (t=0) under the action ofI0.It means that the control system has global robustness.

        Where:cis a positive number;x0is the initial value ofx1.

        The control objective is to make the system state reach the sliding surface (s(x,t)=0) in a finite time and has a secondorder sliding mode (=s=0).Therefore,some assumptions must be satisfied:

        Case 1:uis bounded and continuous;for any virtual value oft,the system is steady;

        Case 2:‖f(x)‖2≤F,‖g(x)‖2≤G,F?Rn,G?

        When the system satisfies the above conditions,it is necessary to assume global boundedness of uncertainty.Thus,positive real numbers,includingC,KmandKM,must meet the respective ranges as shown in the formula (14).

        Fig.4.STA structure diagram.

        The following controllable first-order system is considered to replace the error tracking system of the direct and quadrature axes currents.

        Where:xis the state value of the current errors in direct and quadrature axes;ξ(t) is the uncertain disturbance term of the system;u(t) is the super-twisting control law [29].

        Conventionally,the control law can be defined in the Eq.

        Where:sign(s) is the symbolic function;αandβare positive real numbers.

        Actually,HOSMC based on STA is difficult to prove its system stability.Moreover,the relative controller parameters are difficult to determine due to uncertain boundaries.Fortunatel,HOSMC can further weaken the chattering theoretically and converge in a limited time under certain conditions.It only requires the sliding mode variablesand the suitable systems with a relative order of 1.Furthermore,because of positive gain parameters of the super-twisting control law,the restrictive conditions ofαandβin the Eq.(18) should also be satisfied [30].

        According to the description,the structure diagram of STA is shown in Fig.4.

        In the two-dimensional plane coordinated bysand,the uncertain state trajectory can spirally converge to the origin stable state within a finite time.The derivative formula of the sliding surfacesestablished according to the formula Eq.(12),combined with Eqs.(15) - Eq.(16),the electromagnetic torque and voltage are obtained as below.

        3.2. Stability based on improved HOSMC

        Although HOSMC has obvious advantages,it still ineluctably produces chattering that worse the system reliability and safety.It is worth noting that according to the formula,the traditional control law will bring contradictory phenomena.Once the speed towards to the sliding surface is accelerated,the convergence speed is also increased,while the chattering will be also increased dramatically.Conversely,the chattering and convergence speeds will be greatly reduced with the reduced speed to the sliding surface.Consequently,it’s very important to establish a reasonable control law to balance the chattering and convergence speeds when the point is not on the sliding mode surface.In order to solve this problem,the saturation function is proposed instead of the ideal symbol function to further reduce the chattering for this non-linear system [31].Compared with the sign function,this function will make the velocity gradually decrease to zero when it approaches the switching planes.The expression of the saturation function sat(s) is shown in the Eq.(19).Actually,it is a switching control outside the boundary layer and a linear feedback control inside the boundary layer.

        Where:Δis boundary layer.

        Accoridng to this equation,the Eq.(18) can be rewritten with this substitution function.

        Then,the system model is further simplified and the system state quantityyis constructed.In practice,it is necessary to assume the absolute value of the system uncertain term not exceed an upper limit.Therefore,a constant value can be set to make the first derivative zero.Ultimately,the Eq.(15) is transformed into the Eq.(21).

        In order to demonstrate the stability of whole system,it only needs to verify the deviation system can converge to the origin in a finite time.It means that the equation=xmust work.Thus,a matrixAneeds to be set for the confirmation[32,33].The proof process is simply summarized as follows.

        Secondly,a non-smooth quadratic-like function is chosen as the alternative Lyapunov function,which is defined as the Eq.(23) [34].

        Meanwhile,it is noteworthy that the functionVis not only continuous positive definite but also radially unbounded.Except for the point set {x=0},Vis divisible everywhere.When the system does not converge to the origin,the system state does not always stay at a certain point of the set{x=0}[31][32].Then,let the derivative ofVbeV,thus:

        Since the Lyapunov functionVis a quadratic positive definite function,there are:

        Fig.5.Control strategy of MCECS.

        Where:λmin(P) andλmax(P) are the minimum and maximum eigenvalues of the positive definite symmetric matrixP;represents the 2-norm in the Euclid spaceR2.

        Finally,this is a constant who depends on the control law parameter (λ,α) and the matrixQ.From Lyapunov’s comparison theorem,the following inequality (28) is established[35].

        That is to say,the system can stabilize to the origin within a limited time,and its convergence time can be estimated.

        4.Simulation and analysis

        After the establishment of the control model,a double closed-loop simulation model based on MATLAB/Simulink was built to demonstrate the validity of the HOSMC.Moreover,the decoupling method was also applied in the model to reduce the complexity of the control system.The control strategy block diagram of the whole MCECS is shown in Fig.5.The speed controller aims to achieve the maximum power from the marine current.The current controllers are to follow the expected quasi-sinusoidal current waveform perfectly to reduce the torque ripple.The relevant parameters of MCECS are shown in TABLE1.

        Fig.6.A D-axis current (B) Q-axis current (C) Electromagnetic torque (D) Electrical angular velocity,Verification of STA-based HOSMC.

        TABLE1 Parameters of DSPM machine.

        In the previous work [23]and [36],various simulation results have verified that,this toothed pole DSPM machine still has larger torque ripple even with the conventional sinusoidal current.Therefore,one special current waveform called quasi-sinusoidal current is proposed to decrease the torque ripple.The definition of this current waveform is simplified in Appendix A,which is not elaborated in detail here.

        4.1. Verification of STA-based HOSMC

        In the previous sections,the construction of the controller has been completed.The performance of the controller will be verified by MATLAB/Simulation in this section.Indeed,it is very essential to design a simulation strategy that fits the reality.Obviously,the velocity of ocean current cannot always be considered as constant in the marine environment.Therefore,the control effect of the toothed pole DSPM machine can be checked by variable velocities at different stages.In this simulation,the given marine current velocity is 2.5 m/s at the beginning;then,it is abruptly changed to 3.0 m/s at the moment of 1 s and remains until the end.As shown in Fig.6 below,the detailed results of different objects are given subsequently.

        Firstly,as shown in Fig.6.A,the tracking error of daxis current fluctuates within the range of [-0.8,0.8].At the moment of 1 s,the marine current velocity suddenly changes to 3.0 m/s.The value of the d-axis current control error can also be stabilized to [-0.5,1].Fig.6.B shows the variations of the q-axis current.

        Unlike the conventional sinusoidal current waveform,the q-axis current through coordinate transformation is not constant due to the desired harmonic terms.Fortunately,with the STA-based HOSMC,such current component can also be accurately tracked.For the variation of electromagnetic torque in Fig.6.C,the electromagnetic torque has a certain overshoot inevitably in the start-up stage.The tracking error of electromagnetic torque can be controlled within 2.0% when it reaches the stable state in the first stage.Once the ocean current velocityVtidesuddenly changes to 3.0 m/s,the electromagnetic torque can be adjusted perfectly in a relatively short time.By comparing the torque ripple,it is found that the tracking error is smaller.As the electrical angular velocity of the machine is proportional to the mechanical angular velocity,the change of the electrical angular velocity reflects the mechanical angular velocity.Fig.6.D shows that the tracking error of electrical angular velocity is far less than 1%.

        4.2. Testing the robustness of STA

        Actually,SMC is highly favored owing to its robustness and good dynamic performance.Hence,the main emphasis is always placed on proof of the robustness.In this section,the parameters of the machine will be changed to verify the robustness of the controllers.If the machine can still resume stable operation in a limited time when the parameters change,it is considered to be robust.

        Fig.7.A Electromagnetic torque.(B) Electromagnetic angular velocity.Influence of R s .

        Fig.8.A Electromagnetic torque.(B) Electrical angular velocity.Influence of L.

        The operation of the overall system was tested under different multiples of the stator resistanceRsand inductanceL.The values ofRsandLin the machine model will be changed from 50% to 200% of the initial value with other constant parameters.The electromagnetic torque and electrical angular velocity are selected and shown in Fig.7 and Fig.8 consequently.In order to facilitate the simulation,the marine current velocity is given as a fixed value.The red lines indicate that the stator resistance or inductance is twice the original value.Similarly,the cyan lines indicate that the parameter is half of the original value.

        From Fig.7.A and Fig.7.B,STA-based HOSMC can still approach the reference at the same response time and track the reference well with the great variation of the resistanceRs.Evidently,the changes in both electrical angular velocity and electromagnetic torque caused by the variation in resistance is negligible.From the other two pictures in Fig.8.A and Fig.8.B,the results equally illustrate that there is only slight distinction generated by the inductance variation.According to the simulation results,they can well validate the robustness to the significant variation of parameters under the STA-based HOSMC.

        5.Conclusion

        This paper mainly studies the control strategy for the DSPM machine,which is used for direct drive MCECS.Firstly,the turbine model is established.Under the SHOM method,a practical first-order marine current resource model is obtained.Then,a STA-based HOSMC is firstly proposed to control the speed and current of the DSPM machine.The integral sliding surface and control law are well designed and improved subsequently.Meanwhile,a quadratic Lyapunov function is used to prove the stability of the system within a limited time.According to the simulation results,not only the effective control under the variable marine current velocity but also the strong robustness with different machine parameters are verified.However,although the control effect has been greatly improved,the parameters of the controller are fixed and cannot be changed as the control parameters change.Therefore,it is meaningful to combine the intelligent algorithm to obtain the real-time optimal solution of controller parameters.

        Declaration of Competing Interest

        The authors declare that they have no known competing financial interests or personal relationships that could have appeared

        Acknowledgments

        This work was supported by National Natural Science Foundation of China,China (Grant No:61503242) and Natural Science Foundation of Shanghai,China (15ZR1419800).

        Appendix A

        The quasi-sinusoidal current in a three-phase stationary coordinate system is shown in Eq.(A.1):

        Where:Im(θe) is quasi-sinusoidal current amplitude,which varies with electrical angleθe.

        Meanwhile,the formula of the basic electromagnetic torque can be rewritten as follows:

        Because the current has to be some actual value in theory,the amplitude of this current is shown in the Eq.(A.3).

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