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MAXIM INSTITUTE OF TECHNOLOGY, BHOPAL Session: 2012-2013 Student Name : Enrollment No.: Subject :Lab-II (Software and simulation) Semester: M.Tech I Sem (Power Electronics)_ Subject Code : MEPE 107 List of Experiments S. NO QUESTIONS PAGE NO. 1. Simulation of single phase Half wave converter circuit using MATLAB. \ 2. 3. 4. 5. 6. Simulation MATLAB. of chopper circuit using Simulation of speed torque characteristics of DC motor using MATLAB. Simulation of single phase Half wave Inverter Circuit using MATLAB. Simulation of 3Φ Inverter in 180º mode of conduction using MATLAB. Find the output response of single phase uncontrolled & controlled bridge rectifier Using MATLAB. 7. Simulation of transfer operational amplifier. function using 8. Simulink model of armature voltage speed control. . SIGNATURE REMARKS Experiment 01 single-Phase Rectifier Description This system contains two identical circuits showing the operation of a single phase rectifier. The rectifiers are fed by a 120 V/ 24 V linear transformer. The rectified voltage is filtered by a 100 mH / 200 uF filter and applied to a 5 ohm resistive load. The load voltages are measured by two Voltage Measurement blocks Vd1 and Vd2. The top circuit (circuit 1) uses four individual diodes connected in a bridge configuration. The currents of diodes 2 and 4 are obtained at the measurement 'm' output of the diode blocks and sent to input 1 of Scope 2 through Selector and Multiplex blocks. The bottom circuit (circuit 2) is functionally identical to circuit 1, but the circuit assembly is considerably simplified by the use of the Universal Bridge. Demonstration Open the Universal Bridge dialog box and notice that in order to obtain a four-diode bridge configuration, the Power Electronic device field has been set to Diodes and that the number of arms has been set to 2. Also, observe that the Measurements field has been set to Device currents, thus allowing measurement of diode currents through the Multimeter block. Now, double click on the Multimeter block. The four diode currents are listed in the left column. Notice that only currents in diodes 2 and 4 have been selected and transferred in the right column. The number of available signals at the multimeter output (2) is displayed on the block icon. Open the two scopes and start the simulation. Compare the two load voltages Vd1 and Vd2 which are superimposed on Scope1. Also, compare on Scope2 the currents flowing in diodes 2 and 4 for circuit 1 and circuit 2. Notice that the circuit has been discretized by means of the Powergui block. The sample time (50e-6 s) appears on the block icon. Now, open the Powergui block and select the simulation type Continuous. The continuous ode23tb solver specified in the Simulation Parameters will now be used. Restart the simulation and compare the continuous simulation results with the previous simulation results obtained with a discretized system. Continuous powergui m k g a Thyristor + i - dc current Current Measurement 1 AC Voltage Source + - v Voltage Measurement 1 R Load t Pulse Generator Thyristor 1 g a m k + - v + ac volt Voltage Measurement t Pulse Generator 1 Simulink Model Scope 1 v dc volt Voltage Measurement 2 Experiment 02 SIMULATION AND PERFORMANCE OF POWER ELECTRONIC CIRCUITS The simplest phase controlled rectifier circuit connected to inductive load is shown in Fig. 2. The presence of a commutating diode which prevents the load voltage reversing beyond the diode volt-drop value, resulting in the waveformsis shown in Fig. 3. Fig. 2 Single phase half wave controlled rectifying circuit with commutating diode Fig. 3a Waveform for signal phase half wave controlled circuit with commutating diode During the “thyristor on” period the load current is dictated by equation (1), but once the voltage reverses VL is effectively zero and the load current follows an exponential decay. If the current level decays below the diode holding level then the load current is discontinuous as shown Fig. 3b. Fig. 3 shows a continuous load current condition where the decaying load current is still following when a thyristor is fired in next cycle. The load voltage waveform has a mean value for voltage given by: Inspection of the waveforms clearly shows that the greater the firing delay angle σ the lower is the mean load voltage, equation 2 confirmation that it falls to zero when σ=180o. The thyristor voltage waveform Vt (Fig. 4) shows a positivevoltage during the delay period and also both the peak forward and peak reverse voltage are equal to Vmax of the supply. Inspection of the waveforms in Fig. 2 and Fig. 3 clearly shows the two roles of the commutating diode, to prevent negative load voltage and to allow the thyristor to regain its blocking state at the voltage zero by transferring (or commutating) the load current away from the thyristor. Fig. 3b Thyristor voltage waveforms for single phase half wavecontrol circuit with commutating diode with σ=30o, σ=120o A. Fully Controlled Single Phase Converter The main elements of a fully controlled single phase converter are illustrated in Fig. 4, comprise four thyristors connected in a bridge formation [5]. The positive load terminal can be connected (via Thy1) to terminal A or (via Thy2) to terminal B of the input source and likewise the negative load terminal can be connected either to A or to B via Thy3 or Thy4 respectively. The interest is to find the model operation applicability of the output voltage waveform on the d.c. side and in particular to discover how it can be controlled by varying the firing delay angle σ. The voltage waveform for a given σ will depend up on the nature of the load and to explore the basic mechanism of phase control the case where the load is a resistive is considered. .. .. Fg. 5a Output voltage waveforms of signal phase fully controlledrectifier with resistive load for firing angle delays of 60o Thyristors Thy1 and Thy4 are fired together when terminal A of the supply is positive while on the other half cycle when B is positive Thy2 and Thy3 are fired simultaneously. The output voltage waveforms are illustrated in Fig. 5. At every instant the load is either connected to the mains by the pair of switches Thy1 and Thy4 or it is connected by the pair of switches Thy2 and Thy3 or it is disconnected. It is much smoother than in the single pulse circuit, although again it is far from pure d.c. The waveform shown in Fig. 5a corresponds to σ=60o, while Fig. 5b is for σ=120o. It is clear that the larger the delay angle the lower the output voltage. The maximum output voltage (Vdo) is obtained with σ=0,and given by: Where Vmax is the r.m.s voltage of the incoming mains. Obviously when σ is zero the output voltage is the same as it would be for an uncontrolled diode bridge rectifier, since the thyristors conduct for the whole of the half cycle for which they are forward biased. The variation of the mean d.c. voltage with σ is given by: From which it can be seen that with a resistive load the d.c voltage can be varied from a maximum of Vdo down to zero by varying σ from 0 to 180O. B. Inductive Load Motor loads are inductive and it is well known that thecurrent cannot change instantaneously in an inductive load. Therefore the behaviour of the converter with an inductive load differs from that of a converter with a resistive load. With a fixed σ, the mean output voltage with a resistiveinductive load is not the same as with a purely resistive load and therefore it is difficult to give a simple general formula for the mean output voltage in terms of σ. However, fortunately it transpires that the output voltage for a given σ does become independent of the load inductance once there is sufficient inductance to prevent the load current from falling to zero. This condition is known as continuous current and many motor circuits have sufficient self inductance to ensure that this condition is achieved. Under continuous current conditions the output voltage waveform only depends on the firing angle, and not on the actual value of the inductance present in the circuit. This makes matters straightforward and typical output voltage waveforms for this continuous current condition are illustrated in Fig. 6. Fig. 6 Output voltage waveforms for fully controlled rectifiersupplying an inductive load for σ=120o VI. CONCLUSION The transient analysis of power electronic circuits presents a case where any small amount of gain in speed in any aspect of the solution accumulates into a large saving in costly computer time due to the number of computations done. Methods have been suggested to increase the computational efficiency using the Matlab/Simulink package version 4.1 and 3.1. This is achieved by representing the thyristors based converter systems by a series of switches. The power of the simulation is evident in the clear presentation of the models in this paper. Model for single phase half wave controlled rectifying circuit with commutating diode Model for fully controlled single phase converter Experiment 03 Simulation of Chopper Circuit using MATLAB. Circuit Description The DC motor is fed by the DC source through a chopper which consists of GTO thyristor and free-wheeling diode D1. The motor drives a mechanical load characterized by inertia J, friction coeficient B, and load torque TL. The hysteresis current controller compares the sensed current with the reference and generates the trigger signal for the GTO thyristor to force the motor current to follow the reference. The speed control loop uses a proportional-integral controller which produces the reference for the current loop. Current and Voltage Measurement blocks provide signals for visualization purpose. Demonstration Motor starting Start the simulation. Observe the motor current, voltage, and speed during the starting on the scope. At the end of the simulation time (1.5 s), the system has reached its steadystate. Response to a change in reference speed and load torque The initial conditions state vector 'xInitial' to start with wm = 120 rad/s and TL = 5 N.m has been saved in the 'power_dcdrive_init.mat' file. This file is automatically loaded in your workspace when you start the simulation (see Model Properties). In order to use these initial conditions you have to enable them. Check the Simulation/Configuration Parameters menu , then select "Data Import/Export" and check "Initial state". Now, double click the two Manual Switch blocks to switch from the constant "Ref. Speed (rad/s) " and "Torque (N.m)" blocks to the Step blocks. (Reference speed wref changed from 120 to 160 rad/s at t = 0.4 s and load torque changed from 5 to 25 N.m at t= 1.2s). Restart the simulation and observe the drive response to successive changes in speed reference and load torque. Chopper-Fed DC Motor Drive (Discrete) Circuit Description A DC motor is fed by a DC source through a chopper which consists of GTO thyristor and a free-wheeling diode. The motor drives a mechanical load characterized by inertia J, friction coeficient B, and load torque TL. The motor uses the discrete DC machine provided in the Machines library. The hysteresis current controller compares the sensed current with the reference and generates the trigger signal for the GTO thyristor to force the motor current to follow the reference. The speed control loop uses a proportional-integral controller which produces the reference for the current loop. Demonstration Start the simulation and observe the motor voltage (Va), current (Ia) and speed (wm) on the scope. The following observations can be made: 0 < t < 0.8 s: Starting and Steady State Operation During this period, the load torque is TL = 5.N.m and the motor reaches the reference speed (wref = 120 rad/s) given to the speed controller . The initial values of reference torque and speed are set in the two Step blocks connected to the TL torque input of the motor. Notice that during the motor starting the current is maintained to 30 A, according to the current limit set in the speed regulator. Zoom in the motor current Ia in steady state. Observe the current triangular waveshape varying between 5 A and 7 A, corresponding to the specified hysteresis of 2 A. The commutation frequency is approximately 1.5 kHz. t = 0.8 s: Reference Speed Step The reference speed is increased from 120 rad/s to 160 rad/s. The speed controller regulates the speed in approximately 0.25 s, and the average current stabilizes at 6.6 A. During the transient period, current is still limited at 30 A. t = 1.5 s: Load Torque Step The load torque is suddenly increased from 5 N.m to 25 N.m. The current increases to 23 A, while speed is maintained at the 160 rad/s set point. Experiment 04 Simulation of speed torque characteristics of permanent magnet synchronous motor using MATLAB. Circuit Description This circuit uses the AC6 block of SimPowerSystems™ library. It models a permanent magnet (PM) synchronous motor drive with a braking chopper for a 3HP motor. The PM synchronous motor is fed by a PWM voltage source inverter, which is built using a Universal Bridge Block. The speed control loop uses a PI regulator to produce the flux and torque references for the vector control block. The vector control block computes the three reference motor line currents corresponding to the flux and torque references and then feeds the motor with these currents using a three-phase current regulator. Motor current, speed, and torque signals are available at the output of the block. Demonstration Start the simulation. You can observe the motor stator current, the rotor speed, the electromagnetic torque and the DC bus voltage on the scope. The speed set point and the torque set point are also shown. At time t = 0 s, the speed set point is 300 rpm. Observe that the speed follows precisely the acceleration ramp. At t = 0.5 s, the full load torque is applied to the motor. You can observe a small disturbance in the motor speed, which stabilizes very quickly. At t = 1 s, the speed set point is changed to 0 rpm. The speed decreases down to 0 rpm following precisely the deceleration ramp. At t = 1.5 s., the mechanical load passes from 11 Nm to -11 Nm. The motor speed stabilizes very quickly after a small overshoot. Finally, note how well the DC bus voltage is regulated during the whole simulation period. 1) The power system has been discretised with a 2 us time step. The speed controller uses a 140 us sample and the vector controller uses a 20 us sample time in order to simulate a microcontroller control device. 2) A simplified version of the model using average-value inverter can be used by selecting 'Average' in the 'Model detail level' menu of the graphical user-interface. The time step can then be increased up to 75 us. This can be done by typing 'Ts = 75e-6' in the workspace, by setting Vector control sample time to 75e-6 and by setting Speed controler sample time to 150e-6 in the case of this example. See also ac6_example_simplified.mdl. Experiment 05 Simulation of 3Φ Inverter in 180º mode of conduction using MATLAB. THEORY:A basic three phase inverter is a six-stepbridge inverter. This inverter usesminimum of six switches and six diodes. This circuit is made of six MOSFET’s, butpresently, the use of IGBT’s in place of switches is on rise.In 180-mode operation, eachswitch conducts for 180 degree for everyfull cycle and for other half cycle theother switch connected to the same leg isconnected CIRCUIT DIAGRAM FOR PHASE VOLTAGES WAVEFORMS FOR PHASE VOLTAGES: Van,Vbn, Vcn CIRCUIT DIAGRAM FOR LINE VOLTAGES: Waveform for phase voltages: Experiment 06 SIMULINK MODEL OF ARMATURE VOLTAGE SPEED CONTROL In this section, MATLAB/Simulink model of DC motor driven from single phase AC/DC semi and full converters are presented and the performance of the DC motor drive is analyzed. A 5-HP DC motor of 240-V rating 1220 rpm is used in the simulation model. Fig. 3 shows the Simulink realization of the semi converter drive. The armature circuit is supplied from a single phase semi converter in which a thyristor is used as an electronic switch and a freewheeling diode is used to solve the stored inductive energy problem in the circuit. The field circuit is separately excited from an ideal DC voltage source. A DC motor block of SimPowerSystems toolbox is used. Where, Fig. 4 shows the Simulink realization of the full converter drive. Thearmature circuit is supplied from a single phase full converter in which a thyristor is used as an electronic switch and no freewheeling diode is used. The field circuit is separately excited from an ideal DC voltage source. A DC motor block of SimPowerSystems toolbox is used. Fig: Simulink model Single Phase Semi converter Drive In order to investigate the effect of armature voltage on the torque-speed characteristic, Four different armature voltages with average values Vt = 240 V, 200 V, 160 V and 120 V are applied while the voltage applied to the field circuit is kept constant at its nominal value 240 V. A constant 380 V, 60 HZ AC is applied to the input of single phase semi converter. The average value of the converter output is changed by changing the firing angle (α). A pulse generator is used to change the firing angle. The following firing angles are used to obtain 120, 160, 200 and 240 V average output voltages applied to the armature: α = 89 o, 70o, 47.5o and 0 o. The torque-speed characteristics are obtained for these armature voltages. Fig. 5 shows the torque-speed curves for a single phase semi converter drive. It is clear that torque-speed curves contain both linear and nonlinear regions. The linear region of operation for 240V approximately starts at TL = 30 N.m. But for 200V starts at TL = 50 N.m. While for 160V approximately starts at TL = 60 N.m. Finally for 120V approximately starts at TL = 75 N.m. The discontinuous armature current results in a highly nonlinear torque-speed characteristic. Fig. 6 and Fig. 7 show the armature voltage and current obtained at 25 Nm (in the nonlinear region) and 125 Nm (in the linear region) for average value of 160 V. These figures clearly illustrate the discontinuous and continuous operation of the single phase semi converter drive in non-linear and linear regions, respectively. Experiment 07 Simulation of 1Φ Half Wave Inverter Circuit using MATLAB. This demonstration illustrates use of the IGBT/Diode block in voltage-sourced converters. It also demonstrates harmonic analysis of PWM waveforms using the Powergui/FFT tool. Circuit Description The system consists of two independent circuits illustrating single-phase PWM voltagesourced converters (VSC). 1. Half-bridge converter 2. Full-bridge converter The converters are built with the IGBT/Diode block which is the basic building block of all VSCs. The IGBT/Diode block is a simplified model of an IGBT (or GTO or MOSFET)/Diode pair where the forward voltages of the forced-commutated device and diode are ignored. You may replace these blocks by individual IGBT and diode blocks for a more detailed representation. VSCs are controlled in open loop with the Discrete PWM Generator block available in the Extras/Discrete Control Blocks library. The two circuits use the same DC voltage (Vdc = 400V), carrier frequency (1080 Hz) and modulation index (m = 0.8). In order to allow further signal processing, signals displayed on the two Scope blocks (sampled at simulation sampling rate of 3240 samples/cycle) are stored in two variables named 'sps1phPWM1_str' and 'sps1phPWM2_str' (structures with time). Demonstration Run the simulation and observe the following two waveforms on the two Scope blocks: Current into the load (trace 1), Voltage generated by the PWM inverter (trace 2). Once the simulation is completed, open the Powergui and select "FFT Analysis" to display the 0 - 5000 Hz frequency spectrum of signals saved in the three "sps1phPWMx_str" structures. The FFT will be performed on a 2-cycle window starting at t = 0.1 - 2/60 (last 2 cycles of recording). For each circuit, select Input labeled "V inverter" . Click on "Display" and observe the frequency spectrum of last 2 cycles. The fundamental component of V inverter is displayed above the spectrum window. Compare the magnitude of the fundamental component of the inverter voltage with the theoretical values given in the circuit. Compare also the harmonic contents in the inverter voltage. The half-bridge inverter generates a bipolar voltage (-200V or +200V) . Harmonics occur around the carrier frequency (1080 Hz +- k*60 Hz), with a maximum of 103% at 1080 Hz. The full-bridge inverter generates a monopolar voltage varying between 0 and+400V for one half cycle and then between 0 and -400V for the next half cycle. For the same DC voltage and modulation index, the fundamental component magnitude is twice the value obtained with the half-bridge. Harmonics generated by the full-bridge are lower and they appear at double of the carrier frequency (maximum of 40% at 2*1080+-60 Hz) As a result, the current obtained with the full-bridge is smoother. If you now perform a FFT on the signal "I load" you will notice that the THD of load current is 7.3% for the half-bridge inverter as compared to only 2% for the full-bridge inverter. Fig: Half Bridge inverter