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Automated Tuning and Controller Design for DC-DC Boost Converter
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Automated Tuning and Controller Design for DC-DC Boost Converter
1.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 10 | Oct -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 731 Automated Tuning and Controller Design for DC-DC Boost Converter B. Amarendra Reddy1, M.S.V. Santosh Kumar2 1,2 Dept. of Electrical & Electronics Engineering, Andhra University, AP, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - Design of Controller of any converter plays an important role in effective disturbance rejection, noise attenuation etc. MATLAB based SISOTOOL provided an effective way of designing controller and also provides optimizing the parameters of the controller. In this paper the procedural steps are given to design a controller and to tune the control parameters. Key Words: Controller Design,TuningMethods,MATLAB Simulation, Steep Descent, Loop Shaping, IMC Tuning. 1. INTRODUCTION In SMPS (Switched-mode power supply) DC-DC boost converter has played very important to handle high power. Boost converters are used in many applicationsforregulated power supply. In some applications output changes due to isolation level, temperature change etc, and in other applications output changes according to discharging characteristics and the load change. So there is need for controller for boost converter in many applications. The controller is designed using MATLAB sisotool(single input single output).SisotoolopenstheSISODesignToolwith root locus view andBodediagram.Thecontrollerparameters are optimized by tuning. Manual tuning is purely trail and error process, time consuming and non - systematic. It may not produce optimal design and can lead to dangerous conditions. Sisotool hassomestandarddesignproceduresfor tuning the parameters of the controller. This paper is organized as follows:-Thecontrollerdesign and tuning methods are described in section 2 and 3. Examples shown are described in section 4. Conclusion is given in section 5. 2. DESIGN OF CONTROLLER The design process using SISO Tool in MATLAB environment includes the following points Step 1:The compensator elements are to be optimized for example Gain, Real Pole, Real Zero, Complex Zeros, Complex Poles etc. Step2:Choose the typeofthedesignrequirementforexample Step response bounds/Step response lower/ upper amplitude limit, Impulse Response lower/ upper amplitude limit, Bode magnitude upper/lower Limit, Phase Margin. Step3:The response specifications for the design requirement are to be specified for example the PM and GM in Frequency Response Specifications (OR) Specify rise time, settling time, Peak Overshoot in Time Response Specifications Step4:Type of response is to be specified for example closed loop from r to y/closed loop from r to u/compensator C/ Input sensitivity/Noise sensitivity/open loop/output sensitivity). Step5: We have choose the method for optimization like Gradient search method (or Pattern Search method or Simplex Search method)and Maximum number of iterations and function tolerance etc. Step6:As a final step the optimization can be started by clicking button. After successful termination with desired convergence, we obtain the compensated transfer function. Fig -1: Command of sisotool in workspace Fig -2: SISO design for SISO design task
2.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 10 | Oct -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 732 Fig -3: (a) Arrangement of pole zero pair positions (b)Corresponding Bode plot Fig -4: Transfer function in compensator editor. 3. AUTOMATED TUNING For automated tuning leading edge boost converter system transfer function and the open–loop frequency response specifications are to be noted. Optimization Based Tuning is to create an initial compensator design (or) to refine the current compensator design. In the Optimization Based Tuning there are three important steps (i) Selecting the compensators to optimize. (ii) Select the design requirements. (iii) Select the Optimizing options and Optimize. 3.1 Steepest Descent Method The classical steepest Descent method is one of the oldest methods for minimization of a general nonlinear function .The steepest descent method is also known as gradient descent method was first proposed by Cauchy in 1847.The basis for the method is the continuous function should decrease at least initially if one takes a step along the direction of the negative gradient. 3.2 Simplex Search Method Simplex-based direct search methods are based on comparison of the objective function values at the vertices of a simplex (which is a set of n+ 1 point in dimension n) that is updated by the algorithms steps. 3.3 IMC Tuning Method It obtains a full-order stabilizing feedback controller using the IMC design method. A Control System design is expected to providea fastand accurateset pointtrackingthatisoutput of the system should follow the input as closely as possible. Also any external disturbances must be corrected by control system as efficiently as possible. In practice an open loop system is sensitive to modeling errors and inability to deal with external disturbances entering the system. To deal with disturbances and modeling error,controlsystemsarealways of closed loop type. A design strategy is to shape directly the relevant closed loop transfer functions. Specify the desired closed loop response and solve for resulting controller. The key step is to specify a good closed- loop response. 3.4 Loop Shaping Method It finds a full-order stabilizing feedback controller with a desired open loop bandwidth or shape. Principle of Loop Shaping: This is the classical approach in which the magnitude of the open loop transfer function is shaped. Usually no optimization is involved and the designer aims to obtain magnitude of loop gain with desired band width, slopes. Loop Shaperefers to the magnitude oftheloop transfer function as a function of frequency. By loop shaping we mean a design procedure that involves explicitly shaping the magnitude of the loop transfer function. 4. EXAMPLES To show the effectiveness of these stabilizing PI controller design methods third-order systems are considered for simulation in MATLAB. 4.1 Steepest Descent Method Original Compensator Transfer Function: (Which is to be refined) 2 6.535(z -1.985z+0.987) (z-1)(z-0.8008) After fine adjustments by changing the pole zero locations in the vicinity of original compensator after compensation 2 3.4605(z -1.969z+0.9718) (z-1)(z-0.7071) With this compensator the Open loop system is having GM 9.74dB PM 44.4 degrees
3.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 10 | Oct -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 733 Case (a) : Input Disturbances: Input Perturbation: Initially the system Operates with an input of 10V DC Supply and itis perturbed withastepchange of 10volts to 15 volts at 50 milliseconds. Chart -1: Input Disturbances of SD method Observations: The system with original compensator is exhibiting more overshoot and it takes more settling time after input perturbation at 50 milliseconds. The system with Steepest Descent method optimized compensator is exhibiting lesser overshoot and less settling time after input perturbation at 50 milliseconds. Case (b) : Load Disturbances: Initially the system Operates with a load resistance of 10 ohms and it is perturbed with a step change of 10 ohms to 110 ohms at 50 milliseconds. Chart -2: Load Disturbances of SD method Observations: The system with original compensator is exhibiting more overshoot after load disturbance at 50 milliseconds. The system with Steepest Descent method optimized compensator exhibiting overshoot less than the system with original 4.2 Simplex Search Method Original Compensator Transfer Function: (Which is to be refined) 2 6.535(z -1.985z+0.987) (z-1)(z-0.8008) After fine adjustments by changing the pole zero locations in the vicinity of original compensator after compensation 2 4.038(z -1.986z+0.989) (z-1)(z-0.7723) With this compensator the Open loop system is having GM 6.74dB PM 36.6 degrees Case (a) : Input Disturbances: Input Perturbation: Initially the system Operates with an input of 10V DC Supply and itis perturbed withastepchange of 10volts to 15 volts at 50 milliseconds. Chart -3: Input Disturbances of SS method Observations: The system with original compensator is exhibiting more overshoot and it takes more settling time after input perturbation at 50 milliseconds. The system with Simplex Search method optimized compensator is exhibiting lesser overshoot and less settling time after input perturbation at 50 milliseconds. Case (b) : Load Disturbances: Initially the system Operates with a load resistance of 10 ohms and it is perturbed with a step change of 10 ohms to 110 ohms at 50 milliseconds.
4.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 10 | Oct -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 734 Chart -4: Load Disturbances of SS method Observations: The system with original compensator is exhibiting more overshoot after load disturbance at 50 milliseconds. The system with Simplex Search method optimized compensator exhibiting overshoot less than the system with original 4.3 IMC Tuning Method Original Compensator Transfer Function: (Which is to be refined) After fine adjustments by changing the pole zero locations in the vicinity of original compensator after compensation With this compensator the Open loop system is having GM 10.3dB PM 65.6 degrees Case (a) : Input Disturbances: Input Perturbation: Initially the system Operates with an input of 10V DC Supply and itis perturbed withastepchange of 10volts to 15 volts at 50 milliseconds. Chart -5: Input Disturbances of IMC method Observations: The system with original compensator is exhibiting more overshoot and it takes more settling time after input perturbation at 50 milliseconds. The system with IMC tuningmethod optimized compensator is exhibiting lesser overshoot and less settling time after input perturbation at 50 milliseconds. Case (b) : Load Disturbances: Initially the system Operates with a load resistance of 10 ohms and it is perturbed with a step change of 10 ohms to 110 ohms at 50 milliseconds. Chart -6: Load Disturbances of IMC method Observations: The system with original compensator is exhibiting more overshoot after load disturbance at 50 milliseconds. The system with IMC method optimized compensator exhibiting overshoot less than the system with original 4.4 Loop Shaping Method Original Compensator Transfer Function: (Which is to be refined) After fine adjustments by changing the pole zero locations in the vicinity of original compensator after compensation 2 With this compensator the Open loop system is having GM 10.1dB PM 58.9 degrees Case (a) : Input Disturbances: (z-1)(z-0.3333) 7.704(z -1.985z+0.9872)2 (z-1)(z-0.8008) 6.535(z -1.985z+0.987)2 (z-1)(z-0.5445) 0.94667(z+1)(z -1.985z+0.9872)2 (z-1)(z-0.8008) 6.535(z -1.985z+0.987)2
5.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 10 | Oct -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 735 Input Perturbation: Initially the system Operates with an input of 10V DC Supply and itis perturbed withastepchange of 10volts to 15 volts at 50 milliseconds. Chart -7: Input Disturbances of LS method Observations: The system with original compensator is exhibiting more overshoot and it takes more settling time after input perturbation at 50 milliseconds. The system with loop shaping method optimized compensator is exhibiting lesser overshoot and less settling time after input perturbation at 50 milliseconds. Case (b) : Load Disturbances: Initially the system Operates with a load resistance of 10 ohms and it is perturbed with a step change of 10 ohms to 110 ohms at 50 milliseconds. Chart -8: Load Disturbances of LS method Observations: The system with original compensator is exhibiting more overshoot after load disturbance at 50 milliseconds. The system with IMC method optimized compensator exhibiting overshoot less than the system with original 5. CONCLUSIONS Controller is designed using SISO tool. The parameters of controller resulted from this tool is modified using Automated tuning. This automated tuning allows parameter's optimization, parameter's tuning for robust time response and shaping the frequency response for desired bandwidth etc. Here the controller parameters are optimized. The performance of a DC-DC converter is evaluatedusing original compensator and different possible compensators against input disturbances and load disturbances. REFERENCES [1] Jaen, Carles, et al. "A linear-quadratic regulator with integral action applied to pwm dc-dc converters." IEEE Industrial Electronics, IECON 2006-32nd Annual Conference on. IEEE, 2006 [2] Dragan Maksimovic, Senior Member, IEEE, and Regan Zane,SeniorMember,IEEE“ Small-Signal Discrete-Time Modeling of Digitally ControlledPWMConverters”IEEE TRANSACTIONS ON POWER ELECTRONICS, VOL. 22, NO. 6, NOVEMBER 2007. [3] V. Yousefzadeh, M. Shirazi, and D. Maksimovic, “Minimum phase response in digitally 870. controlled boost and flyback converters,” in Proc. IEEE Appl. Power Electron. Conf., 2007. [4] Maksimovic, Dragan, and Regan Zane. "Small-signal discrete-time modeling of digitally controlled DC-DC converters." Computers in Power Electronics, 2006. COMPEL'06. IEEE Workshops on. IEEE, 2006. [5] MATLAB – Mathworks .com
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