Modelling a 2.5 MW direct driven wind turbine with permanent magnet generator

Size: px
Start display at page:

Download "Modelling a 2.5 MW direct driven wind turbine with permanent magnet generator"

Transcription

1 Modelling a.5 MW direct driven wind turbine with permanent magnet generator Report for the final examination project of the Nordic PhD coure on Wind Power by Thoma P. Fugleth Department of Electrical Power Engineering Norwegian Univerity of Science and Technology NO-749 TRONDHEIM, NORWAY

2 Introduction Thi report i the concluion of the pot-coure work following the Nordic PhD-coure on Wind Power, which wa held on Smøla 5 th th June 5. The goal of the project wa to contruct a Simulink model of a.5 MW wind turbine with direct-driven permanent magnet generator connected to the grid via a back-to-back three-phae converter. The model wa then to be teted in imulation run.

3 Content Introduction... Content... 3 Sytem decription and modelling Mechanical dynamic Permanent magnet generator Generator-ide converter Grid ide converter and inductance DC-link dynamic Sytem parameter Wind model... 9 Control trategie.... Generator ide control.... Grid ide converter control... 3 Simulation reult... 3 Concluion and further work... 9 Reference... 3

4 Sytem decription and modelling Thi chapter um up the equation which were implemented in the imulink model. The ytem in it entirety conit of the following component. A wind turbine generate torque from wind preure. The torque i tranferred via the generator haft to the rotor of the generator. The generator produce an electrical torque, and the difference between the mechanical torque from the wind turbine and the electrical torque from the generator determine whether the mechanical ytem accelerate, decelerate or remain at contant peed. The generator i connected to a three-phae converter which rectifie the current from the generator to charge a DC-link capacitor. The DC-link feed a econd three-phae converter which i connected to the grid through a tranformer. Tranformer inductance Back-to-back converter ~ = + V _ dc = ~ PM generator V3 ϕ Grid figure Sytem overview. Mechanical dynamic It i not a part of thi exercie to model the wind turbine itelf and the pitching action of the blade. Intead it i aumed that the turbine i run at variable peed to enure that the tippeed ratio remain at a contant optimal point? opt =7.5 with a power coefficient C p =.474. The mechanical torque delivered by the wind turbine i given by: 3 Mt = π ρair Rwt Cp( λ) v (.) Here,? air i the denity of air, in kg/m 3. R wt i the radiu of the wind turbine rotor in meter and v 8 i the wind peed far away from the turbine. That i, the wind peed before it i lowed down by the wind turbine. C p (?) i the coefficient of power a a function of the tip-peed ratio?. Normally thi will alo be a function of the rotor pitch, but pitching dynamic are not modelled. The tip peed ratio? i calculated a: ωmek Rwt λ = v Thi value i fed to a look-up table to find value of C p (?). The turbine i connected to the rotor of the generator via a haft. The turbine, haft and generator are modelled a a ingle rotating ma: dωmek = ( Me + Mt) (.) dt J total 4

5 where M e i the electromechanical torque developed by the electrical machine (when the electrical machine i operated a a generator M e will be negative) and J total i the moment of inertia of the entire mechanical ytem. In p.u. value equation (.) become: dn = ( me + mt ) (.3) dt Tm For more accurate reult, the mechanical dynamic could be modelled a a two-ma-ytem with a pring and damper between them, but thi wa not done due to contraint in time and in available information.. Permanent magnet generator The generator model i implemented entirely in dq-coordinate. That i to ay, there are no AC-tate in the model. The generator i modelled with dc voltage and current in a rotorfixed rotating coordinate ytem with the d-axi being in the direction of the flux from the permanent magnet. Thi model i a caled per-unit model, and eentially the ame a that hown in [Nilen, 5]. The equation for the d- and q-axi voltage are a follow: dψ d ud = r id + n ψ q (.4) ω dt n dψ u = r i + + n (.5) q q q ψ d ωn dt Here, i d, i q, v d and v q are the p.u. d- and q-axi current and voltage repectively, r i the p.u. tator reitance.? n i the baic electrical frequency of the generator, n i the p.u. frequency og the generator and? d and? q are the d- and q-axi fluxe repectively. The d- and q-axi fluxe are given a follow: ψ = x i + ψ (.6) d d d m ψ = x i (.7) q q q We ee that by keeping the q-axi current equal to zero, we can orient the flux entirely in the d-axi direction. More on thi will follow later. Next, (.6) and (.7) are inerted into (.4) and (.5) to get the following: xd did ud = r id + n xq iq (.8) ω dt n x q diq q q d d ψ m ωn dt u = r i + + n ( x i + ) (.9) Tranforming thee equation a bit we get: did ωn = ( ud r id + xq ni q ) (.) dt x d q ωn di = ( uq r iq n ( xd id + ψ m) ) dt xq (.) The p.u. torque developed i given by: τ = ψ i ψ i (.) e d q q d 5

6 Thee equation are implemented in the imulink diagram hown below. r id id ud wn/xd Wn/Xd I_d -Cpim xd Gain pid pid*iq Me n*pid 3 n n piq*id n*piq piq xq Gain4 uq wn/xq Gain3 I_q iq 3 iq r figure Simulink model of permanent magnet generator.3 Generator-ide converter When working with a implified dq-model it i common to neglect witching dynamic, ripple current and other fat dynamic in the electrical ytem. In thi cae, we follow the example of [Nilen, 5] and model the generator ide converter a a imple time delay. That i, the voltage on the generator clamp are given a: u () t = u ( t t) u () t (.3) d contd, v dc q contq, v dc u () t = u ( t t) u () t (.4) where u cont,d and u cont,q are the control ignal given a output from the controller..4 Grid ide converter and inductance For the grid/tranformer inductance, the model given in [Molina et al. 5] i ued: g g g did g c ud = rg id + lg ng lg iq + ud (.5) dt g di g g q g c uq = rg iq + lg + ng lg iq + uq (.6) dt c Here, the upercript g tand for grid, to differ from the generator variable. v d and v c q are the voltage on the clamp of the front-end converter. 6

7 By tranforming thee equation we get: di dt g d g c g g = ( ud ud rg id + ng iq ) (.7) l g g diq g c g g = ( uq uq rg iq ng id ) (.8) dt lg Which i the model implemented in the imulink diagram hown in figure 3. ud_grid uq_grid /L i_dq u_dq_grid P i_dq Q Power calculation id 3 P 4 Q 3 ud_converter Add Gain Integrator R Gain [x] iq 4 uq_converter Product 5 n_grid Gain figure 3 grid inductance model The grid ide converter i modelled a a time delay jut like the generator ide converter..5 DC-link dynamic The equation for the DC-link dynamic are taken from the lecture note given at the Smøla coure [Norheim, 5], and are a follow: dudc c c c c = ( ( ud id + uq iq ) ( ud id + uq iq ) ( Prlo, + Pdlo, )) (.9) dt C udc Thi follow eaily from the principle of conervation of energy. The total power flowing into the capacitor bank mut equal the um of the power flowing out of the capacitor and the loe in the conductor. (.9) can alo be written a du dt d = ( Iv Id ) (.) C where ( Iv = ud id + uq iq Prlo, ) i the current flowing out of the generator ide udc converter and ( c c c c Id = ud id + uq iq Pdlo, ) i the current flowing into the grid ide udc converter. Thi mean that in when the PM machine i operating a a generator thee will both be negative. 7

8 The loe are modelled a imple reitance, IE Prlo, = rv ( id + iq ) and c c Pdlo, = rd ( id + iq ) Thi lo model give a imple approximation to the real loe in the ytem, but for more accurate imulation a better lo model that include witching loe and nonlinear loe in the generator would be preferable..6 Sytem parameter The p.u. value ued in the imulation are baed on a.5 MW wind turbine. The turbine itelf 6 i 8 meter in diameter, and with a moment of inertia Jwt = 9. kgm [DAWE 4]. A mentioned earlier, the pitching dynamic are not modelled. It i aumed that the blade are pitched to maintain optimum energy capture. The objective of the generator control i to keep the turbine running at a rotational peed correponding to a tip-peed ratio which give u the optimal power coefficient C p,opt =.474. In reality thi i imilar to controlling a fixed-pitch turbine. The C p -table data are taken from [DAWE, 4]. The generator i a permanent magnet generator with urface mounted magnet and ymmetrical rotor. In other word, the reactance i the ame in both the d- and q-axi. The p.u. value that have been ued in thi imulation are: r =. x d = x =.5 Thee are approximate value that are reaonably repreentative of a ynchronou PM machine in the.5 MW range. If we aume that p.u. peed and no load torque require p.u. tator voltage, we get a p.u. flux of ψ m =.865 Phyically, the rotor of the generator i aumed to conit of three cylinder ection: a center ection with a radiu of.5 meter and a length of.5 meter, a dic ection with an outer radiu of. meter and a length of.4 meter and an outer cylinder with an outer radiu of.5 meter and a length of meter. For the purpoe of calculating moment of inertia, the rotor i aumed to conit of homogenou teel. Uing the formula for moment of inertia for a cylinder 4 4 J = π ρ ( ) teel l router rinner with a denity? teel of 785 kg/m 3 6 we get a total moment of inertia J total = 9.93 kgm. The per unit mechanical time contant i Jtotal ωmekn, Tm = Sn where? mek,n i the nominal rotational frequency in rad/ec, which in thi cae equal π rad ω mek, n= 6rpm = and S n i the nominal power, in thi cae,5 MW. Thi give u a time contant of Tm = = q 8

9 The DC-link capacitor i dimenioned uing an empirical rule that i commonly ued in literature: CU dc, rated S n = τ dc (.) Here, C i the capacitance of the DC-link capacitor, U dc i the nominal DC-link voltage and S n i the nominal power of the generator. The time contant t dc i generally elected to be a proportion of a full cycle for the grid voltage. A full cycle for a 5 Hz grid i m, and a time contant of 6-8 m eem common. (.) give u: Sn τ dc C = U dcrated, Next, we know that the per unit capacitive reactance i: Idcrated, x = c ω CU (.) dcrated, If we inert the expreion for C into (.) and take into account that Idcrated, = Sn / Vdcrated, we get: Sn Udc, rated x = c Sn τ = dc ω U ωτ dc dcrated, Udc, rated We ee that the per unit capacitive reactance i independent of the phyical rated voltage and current. If we choe the DC-link time contant to be 7. m (.36 cycle) we get an x c value of: x c = =. 3 ( π 5 Hz)7. In teting, thi proved to be a bit too mall. In the end, x c wa et to be.5, which yielded better reult..7 Wind model The wind model ued i one developed at the Riø National Laboratory in Denmark. The imulink implementation i deigned at the Univerity of Aalborg, and i available from a part of the Wind Turbine Blocket beta, a toolbox for wind turbine imulation in Simulink. 9

10 Control trategie Thi chapter detail the trategie ued in the control ytem of the generator and the grid ide converter.. Generator ide control The generator ide control i baed on the tator voltage equation (.) and (.). To implify the control deign we divide the control ytem into two part: a decoupling controller and a PI controller. In other word, we give the input voltage the form: u = u + u (.) d di dii uq = uqi + uqii (.) We ee that if we give u dii and u qii the following form: u = n x i (.3) dii q q uqii = n xd id + n ψ m (.4) then we get the following firt order ytem to control: did ωn r ωn = i d + u di (.5) dt xd xd diq ωn r ωn = i q + u qi (.6) dt xq xq Equation (.5) and (.6) repreent two firt order ytem with one control variable each. In hort, we ue the control ytem to decouple the d- and q-axi equation from each other, a well a removing the peed-dependent term. The d- and q-axi current can now be controlled with two ordinary PI controller. The decoupling controller i dependent on meaurement of the current a well a knowledge of the impedance x d and x q and the flux generated by the permanent magnet. However, by uing PI controller, any error introduced by minor inaccuracie in the aumed value of? m, x d and x q are compenated for by the integrating controller. A hown in [Nilen, 5], the ytem defined by (.5) and (.6) can be repreented by the following implified tranfer function: id() ωn Td hd () = = (.7) u () x ( + T )( + T ) h q di d d um iq() ωn Tq () = = u () x ( + T )( + T ) qi q q um x x d q where Td = and Tq = ωn r ωn r T um i the um of all the maller time contant in the ytem uch a filtering of current meaurement and linearized witching delay. The current controller are PI controller with limited output and anti- wind-up feature. Antiwind-up i implemented by diabling the integrator while the output from the controller i equal to the upper or lower limit. The general tranfer function of the PI controller i a follow: (.8)

11 + Ti hpi() = Kp (.9) Ti Controller deign follow the guideline given in [Nilen, 5]. Since the generator ha a ymmetrical rotor with x d =x q the controller deign for both axe will be the ame. We tart out with what i termed the numerical optimum deign, which give u: xd K pd, = Tid, = Td ωn Tum When number are inerted, we get: K pd, = 5.65 T id, =.85 During teting, it wa revealed that thee controller value gave a controller that wa too aggreive, leading to rapid aturation and overhoot. After ome teting and tuning, the following current controller parameter were elected: K pd, =. T id, =.5 which yielded better performance. The peed controller i quite intereting compared to mot regular motor drive, a what we are really intereted in controlling i the tip peed ratio. While thi work quite well in imulation, tip peed ratio can be difficult to control in a real turbine. The rotational peed of the turbine can be meaured with a high degree of accuracy, but wind peed meaurement (which are neceary to calculate the tip peed ratio) are eaily affected by turbulence and other factor. In thi imulation we aume perfect wind peed meaurement, but in reality ome form of etimation baed on meaurement and modelling will probably have to be ued. Thi will again lead to ome lo of production, a the controller i unable to perfectly optimize the production. For peed control, the ytem wa teted with a PI-type controller deigned uing the ymmetrical optimum trategy, again taken from [Nilen, 5]. Thi method give the following controller parameter: Tm K = pn, T T in = 4 T ψ, umn, umn, m T m i the mechanical time contant of the generator and turbine, a detailed in ection.. T um,n i the um of the maller time contant: Tumn, = Teqi, + Tfin,. T fi,n i the peed filter time contant, while T eq,i i the equivalent time contant for the electrical ytem. In other word, the time contant we find if we repreent the electrical dynamic a a ingle firt-order ytem: T = ( T + T ). Thi method gave the following controller parameter: eqi, v f, i K pn, = 3978 T in, =, Thi illutrate that while method for obtaining controller parameter are a ueful tool for initial controller deign, they are not perfect. In thi cae the high proportional amplification meant that the controller for all practical purpoe worked like a hyterei controller. The reult wa a lot of overhoot and a high degree of ocillatory behaviour of the ytem, and the controller had to be tuned manually. Unfortunately none of the PI controller deign gave atifactory behaviour. Generally the ytem dynamic were either too low, or untable.

12 In the end, after a lot of teting and trial and error, it wa decided to go for a limited PID-type controller. The tranfer function of a PID controller i + Ti + Ti Td hpid() = K p (.) Ti The tructure of a PID controller with limited derivative control i illutrated in figure 4. The limitation in derivative i implemented with a rate limitation imulink block. The purpoe of thi limitation i to avoid controller aturation caued by high frequency ignal. K p T d d dt T i Controller parameter were elected motly through manual tuning to be: K pn, = T in, =.8 T dn, =. Thee were found to give atifactory performance.. Grid ide converter control The controller tructure for the grid ide converter i taken from [Norheim, 5]. The original deign conit of two PI controller, one for the amplitude and one for the phae angle of the converter voltage. That i: j u = m u e α (.) c The amplitude m control the reactive power to the grid, while the phae angle a control the DC-link voltage. In thi cae, the ytem wa difficult to tabilize with only PI controller. In particular, m wa prone to ocillatory behaviour. A relatively common occurrence wa that m would ocillate, while a teadily dropped. Thi would continue up to a point where a would drop harply, cauing high grid current, and making the DC-link voltage to drop almot immediately to zero. Naturally, thi would not happen in a phyical ytem. Thi behaviour wa only poible becaue of the implification done in modelling the ytem. However, it hould till be avoided. Eventually, a olution with a PI controller for a and a PID controller for m wa ettled upon, and wa found to give atifactory performance. The controller parameter were: K pm, =.5 T im, =.5 T dm, =.5 K α = T, α =.5 p, figure 4 PID controller i dc

13 3 Simulation reult The reult in thi chapter are baed on a 5 econd imulation with a mean wind peed of 6 m/. Simulation over a longer time frame would have been better, but imulation time wa limited by the amount of memory on the PC ued to run the imulation. The firt illutration, figure 5, how the wind peed time erie, and the correponding generator peed: 7.5 v w ind 7 [m/] n t [] figure 5 wind peed and correponding rotational peed A we can ee, the peed controller doe a good job of controlling the peed depending on the wind peed. The next illutration, figure 6, how the correponding tip peed ratio: 8 tip peed ratio t [] figure 6 tip peed ratio 3

14 A we can ee, the controller managed to keep the tip peed ratio within an acceptable region of the deired tip peed ratio of 7.5. Next, we look at the generator current and voltage. Figure 7 how the generator dq-axi current, while figure 8 how the correponding voltage..4 i d i q iq -.5 iq ref t [] figure 7 d- and q-axi generator current u d u q t [] figure 8 d- and q-axi generator voltage 4

15 In figure 7, the d-axi reference i contantly equal to zero. While the d-axi current tay reaonably cloe to zero the entire time, the controller performance probably could have been a bit better. The q-axi reference depend on the commanded torque from the peed controller, and i hown in red in the lower plot of figure 7. The obtained q-axi current i hown in blue. In general, the obtained current follow the commanded current quite well, but we ee that it overhoot the reference mot of the time, o perhap a lightly le aggreive controller would have been better. On the grid ide, we get the current hown in figure 9. i d,grid i q,grid t [] figure 9 grid d- and q-axi current The q-axi current tay quite well around zero, while the d-axi current varie with the power produced by the wind turbine. Note that the d-axi current i negative becaue the turbine produce power, in other word we are uing a load reference for the converter ytem. The grid ide converter voltage are hown in figure. Thee how pretty much what we would expect, with the d-axi voltage taying nearly contant around p.u. while the q-axi voltage varie with the reactive power required to control the dc-link voltage. Figure how the active and reactive power while figure how the commanded voltage vector given by m and a. 5

16 .5 u d,grid u q,grid t [] figure grid ide converter voltage Active power P Reactive Power Q t [] figure active and reactive power 6

17 -.4 m alpha -.5 [rad] t [] figure m and a 7

18 Finally, figure 3 how the DC-link voltage, a well a the current I v and I d. U dc I v I d t [] figure 3 DC-link voltage and current flowing into and out of the DC-link capacitor While the controller doe a reaonable job of controlling the DC-link voltage around the et point of.75, performance could be better. A imple way of tabilizing the DC-link voltage i by electing a bigger capacitor, but there probably i room for ome controller improvement a well. 8

19 Concluion and further work The imulation how that the model and controller are functioning well. The control trategy work well, although the DC-link voltage ideally hould be controlled more accurately. While the controller worked very well during initial teting with imple wind condition (contant or lowly varying wind peed), imulation with more complex wind condition how that the controller are not quite perfect yet. While the wind turbine model doe a reaonable job of imulating a real turbine, accuracy can be improved in ome repect. Implementation of a better lo model would improve the quality of the model greatly. Alo, it would be intereting to have data from a real wind turbine to bae the model parameter on intead of approximate value. The controller tructure hould be improved by adding a power limiting controller for when the wind peed increae above nominal wind peed. Thi hould be coupled with a model including pitching dynamic and better modelling of the aerodynamic to improve the controllability of the model. Now that a working wind turbine model i in place, it would be intereting to tet it with different controller tructure. One area that could be explored i in the ue of nonlinear control of the DC-link voltage, a thi i a ytem that i inherently nonlinear in nature. Alo, it could be intereting to compare the current olution with a pair of PI-controller and a decoupling grid for generator control with a multivariable nonlinear controller that include the cro-coupling term. 9

20 Reference [Nilen, 5] Roy Nilen, Elektrike Motordrifter, Department of Electrical Power Engineering, Norwegian Univerity of Science and Technology 5 [Norheim, 5] Ian Norheim, Dynamic modelling of turbine (), Generator, converter and control, Preentation from the Nordic Wind Coure, Smøla 7 th June 5 [DAWE, 4] Variou author, DAWE PhD Coure/Advanced chool 4, Compendium and coure material, Intitute of Energy Technology, Aalborg Univerity 4.

BASIC INDUCTION MOTOR CONCEPTS

BASIC INDUCTION MOTOR CONCEPTS INDUCTION MOTOS An induction motor ha the ame phyical tator a a ynchronou machine, with a different rotor contruction. There are two different type of induction motor rotor which can be placed inide the

More information

Section Induction motor drives

Section Induction motor drives Section 5.1 - nduction motor drive Electric Drive Sytem 5.1.1. ntroduction he AC induction motor i by far the mot widely ued motor in the indutry. raditionally, it ha been ued in contant and lowly variable-peed

More information

No-load And Blocked Rotor Test On An Induction Machine

No-load And Blocked Rotor Test On An Induction Machine No-load And Blocked Rotor Tet On An Induction Machine Aim To etimate magnetization and leakage impedance parameter of induction machine uing no-load and blocked rotor tet Theory An induction machine in

More information

15 Problem 1. 3 a Draw the equivalent circuit diagram of the synchronous machine. 2 b What is the expected synchronous speed of the machine?

15 Problem 1. 3 a Draw the equivalent circuit diagram of the synchronous machine. 2 b What is the expected synchronous speed of the machine? Exam Electrical Machine and Drive (ET4117) 6 November 009 from 9.00 to 1.00. Thi exam conit of 4 problem on 4 page. Page 5 can be ued to anwer problem quetion b. The number before a quetion indicate how

More information

ISSN: [Basnet* et al., 6(3): March, 2017] Impact Factor: 4.116

ISSN: [Basnet* et al., 6(3): March, 2017] Impact Factor: 4.116 IJESR INERNAIONAL JOURNAL OF ENGINEERING SCIENCES & RESEARCH ECHNOLOGY DIREC ORQUE CONROLLED INDUCION MOOR DRIVE FOR ORQUE RIPPLE REDUCION Bigyan Banet Department of Electrical Engineering, ribhuvan Univerity,

More information

Basic parts of an AC motor : rotor, stator, The stator and the rotor are electrical

Basic parts of an AC motor : rotor, stator, The stator and the rotor are electrical INDUCTION MOTO 1 CONSTUCTION Baic part of an AC motor : rotor, tator, encloure The tator and the rotor are electrical circuit that perform a electromagnet. CONSTUCTION (tator) The tator - tationary part

More information

Gain and Phase Margins Based Delay Dependent Stability Analysis of Two- Area LFC System with Communication Delays

Gain and Phase Margins Based Delay Dependent Stability Analysis of Two- Area LFC System with Communication Delays Gain and Phae Margin Baed Delay Dependent Stability Analyi of Two- Area LFC Sytem with Communication Delay Şahin Sönmez and Saffet Ayaun Department of Electrical Engineering, Niğde Ömer Halidemir Univerity,

More information

Digital Control System

Digital Control System Digital Control Sytem - A D D A Micro ADC DAC Proceor Correction Element Proce Clock Meaurement A: Analog D: Digital Continuou Controller and Digital Control Rt - c Plant yt Continuou Controller Digital

More information

Performance Improvement of Direct Torque Controlled Interior Permanent Magnet Synchronous Motor Drive by Considering Magnetic Saturation

Performance Improvement of Direct Torque Controlled Interior Permanent Magnet Synchronous Motor Drive by Considering Magnetic Saturation Performance Improvement of Direct Torque Controlled Interior Permanent Magnet Synchronou Motor Drive by Conidering Magnetic Saturation Behrooz Majidi * Jafar Milimonfared * Kaveh Malekian * *Amirkabir

More information

Representation of a Group of Three-phase Induction Motors Using Per Unit Aggregation Model A.Kunakorn and T.Banyatnopparat

Representation of a Group of Three-phase Induction Motors Using Per Unit Aggregation Model A.Kunakorn and T.Banyatnopparat epreentation of a Group of Three-phae Induction Motor Uing Per Unit Aggregation Model A.Kunakorn and T.Banyatnopparat Abtract--Thi paper preent a per unit gregation model for repreenting a group of three-phae

More information

Lecture 4. Chapter 11 Nise. Controller Design via Frequency Response. G. Hovland 2004

Lecture 4. Chapter 11 Nise. Controller Design via Frequency Response. G. Hovland 2004 METR4200 Advanced Control Lecture 4 Chapter Nie Controller Deign via Frequency Repone G. Hovland 2004 Deign Goal Tranient repone via imple gain adjutment Cacade compenator to improve teady-tate error Cacade

More information

Comparison of Hardware Tests with SIMULINK Models of UW Microgrid

Comparison of Hardware Tests with SIMULINK Models of UW Microgrid Comparion of Hardware Tet with SIMULINK Model of UW Microgrid Introduction Thi report include a detailed dicuion of the microource available on the Univerity- of- Wiconin microgrid. Thi include detail

More information

FUNDAMENTALS OF POWER SYSTEMS

FUNDAMENTALS OF POWER SYSTEMS 1 FUNDAMENTALS OF POWER SYSTEMS 1 Chapter FUNDAMENTALS OF POWER SYSTEMS INTRODUCTION The three baic element of electrical engineering are reitor, inductor and capacitor. The reitor conume ohmic or diipative

More information

A Simplified Dynamics Block Diagram for a Four-Axis Stabilized Platform

A Simplified Dynamics Block Diagram for a Four-Axis Stabilized Platform A Simplified Dynamic Block Diagram for a FourAxi Stabilized Platform Author: Hendrik Daniël Mouton a Univerity of Cape Town, Rondeboch, Cape Town, South Africa, 770 Abtract: t i relatively traightforward

More information

Figure 1 Siemens PSSE Web Site

Figure 1 Siemens PSSE Web Site Stability Analyi of Dynamic Sytem. In the lat few lecture we have een how mall ignal Lalace domain model may be contructed of the dynamic erformance of ower ytem. The tability of uch ytem i a matter of

More information

Social Studies 201 Notes for November 14, 2003

Social Studies 201 Notes for November 14, 2003 1 Social Studie 201 Note for November 14, 2003 Etimation of a mean, mall ample ize Section 8.4, p. 501. When a reearcher ha only a mall ample ize available, the central limit theorem doe not apply to the

More information

The Influence of the Load Condition upon the Radial Distribution of Electromagnetic Vibration and Noise in a Three-Phase Squirrel-Cage Induction Motor

The Influence of the Load Condition upon the Radial Distribution of Electromagnetic Vibration and Noise in a Three-Phase Squirrel-Cage Induction Motor The Influence of the Load Condition upon the Radial Ditribution of Electromagnetic Vibration and Noie in a Three-Phae Squirrel-Cage Induction Motor Yuta Sato 1, Iao Hirotuka 1, Kazuo Tuboi 1, Maanori Nakamura

More information

Massachusetts Institute of Technology Dynamics and Control II

Massachusetts Institute of Technology Dynamics and Control II I E Maachuett Intitute of Technology Department of Mechanical Engineering 2.004 Dynamic and Control II Laboratory Seion 5: Elimination of Steady-State Error Uing Integral Control Action 1 Laboratory Objective:

More information

Physics 2. Angular Momentum. Prepared by Vince Zaccone For Campus Learning Assistance Services at UCSB

Physics 2. Angular Momentum. Prepared by Vince Zaccone For Campus Learning Assistance Services at UCSB Phyic Angular Momentum For Campu earning Angular Momentum Thi i the rotational equivalent of linear momentum. t quantifie the momentum of a rotating object, or ytem of object. To get the angular momentum,

More information

Neural Network Linearization of Pressure Force Sensor Transfer Characteristic

Neural Network Linearization of Pressure Force Sensor Transfer Characteristic Acta Polytechnica Hungarica Vol., No., 006 Neural Network Linearization of Preure Force Senor Tranfer Characteritic Jozef Vojtko, Irena Kováčová, Ladilav Madaráz, Dobrolav Kováč Faculty of Electrical Engineering

More information

Induction Motor Drive

Induction Motor Drive Induction Motor Drive 1. Brief review of IM theory.. IM drive characteritic with: Variable input voltage Variable rotor reitance Variable rotor power Variable voltage and variable frequency, VVVF drive

More information

into a discrete time function. Recall that the table of Laplace/z-transforms is constructed by (i) selecting to get

into a discrete time function. Recall that the table of Laplace/z-transforms is constructed by (i) selecting to get Lecture 25 Introduction to Some Matlab c2d Code in Relation to Sampled Sytem here are many way to convert a continuou time function, { h( t) ; t [0, )} into a dicrete time function { h ( k) ; k {0,,, }}

More information

Design By Emulation (Indirect Method)

Design By Emulation (Indirect Method) Deign By Emulation (Indirect Method he baic trategy here i, that Given a continuou tranfer function, it i required to find the bet dicrete equivalent uch that the ignal produced by paing an input ignal

More information

Homework #7 Solution. Solutions: ΔP L Δω. Fig. 1

Homework #7 Solution. Solutions: ΔP L Δω. Fig. 1 Homework #7 Solution Aignment:. through.6 Bergen & Vittal. M Solution: Modified Equation.6 becaue gen. peed not fed back * M (.0rad / MW ec)(00mw) rad /ec peed ( ) (60) 9.55r. p. m. 3600 ( 9.55) 3590.45r.

More information

Bernoulli s equation may be developed as a special form of the momentum or energy equation.

Bernoulli s equation may be developed as a special form of the momentum or energy equation. BERNOULLI S EQUATION Bernoulli equation may be developed a a pecial form of the momentum or energy equation. Here, we will develop it a pecial cae of momentum equation. Conider a teady incompreible flow

More information

ECE 325 Electric Energy System Components 6- Three-Phase Induction Motors. Instructor: Kai Sun Fall 2015

ECE 325 Electric Energy System Components 6- Three-Phase Induction Motors. Instructor: Kai Sun Fall 2015 ECE 35 Electric Energy Sytem Component 6- Three-Phae Induction Motor Intructor: Kai Sun Fall 015 1 Content (Material are from Chapter 13-15) Component and baic principle Selection and application Equivalent

More information

Physics 6A. Angular Momentum. Prepared by Vince Zaccone For Campus Learning Assistance Services at UCSB

Physics 6A. Angular Momentum. Prepared by Vince Zaccone For Campus Learning Assistance Services at UCSB Phyic 6A Angular Momentum For Campu earning Angular Momentum Thi i the rotational equivalent of linear momentum. t quantifie the momentum of a rotating object, or ytem of object. f we imply tranlate the

More information

The Measurement of DC Voltage Signal Using the UTI

The Measurement of DC Voltage Signal Using the UTI he Meaurement of DC Voltage Signal Uing the. INRODUCION can er an interface for many paive ening element, uch a, capacitor, reitor, reitive bridge and reitive potentiometer. By uing ome eternal component,

More information

Social Studies 201 Notes for March 18, 2005

Social Studies 201 Notes for March 18, 2005 1 Social Studie 201 Note for March 18, 2005 Etimation of a mean, mall ample ize Section 8.4, p. 501. When a reearcher ha only a mall ample ize available, the central limit theorem doe not apply to the

More information

SMALL-SIGNAL STABILITY ASSESSMENT OF THE EUROPEAN POWER SYSTEM BASED ON ADVANCED NEURAL NETWORK METHOD

SMALL-SIGNAL STABILITY ASSESSMENT OF THE EUROPEAN POWER SYSTEM BASED ON ADVANCED NEURAL NETWORK METHOD SMALL-SIGNAL STABILITY ASSESSMENT OF THE EUROPEAN POWER SYSTEM BASED ON ADVANCED NEURAL NETWORK METHOD S.P. Teeuwen, I. Erlich U. Bachmann Univerity of Duiburg, Germany Department of Electrical Power Sytem

More information

EE 4443/5329. LAB 3: Control of Industrial Systems. Simulation and Hardware Control (PID Design) The Inverted Pendulum. (ECP Systems-Model: 505)

EE 4443/5329. LAB 3: Control of Industrial Systems. Simulation and Hardware Control (PID Design) The Inverted Pendulum. (ECP Systems-Model: 505) EE 4443/5329 LAB 3: Control of Indutrial Sytem Simulation and Hardware Control (PID Deign) The Inverted Pendulum (ECP Sytem-Model: 505) Compiled by: Nitin Swamy Email: nwamy@lakehore.uta.edu Email: okuljaca@lakehore.uta.edu

More information

Lecture 8 - SISO Loop Design

Lecture 8 - SISO Loop Design Lecture 8 - SISO Loop Deign Deign approache, given pec Loophaping: in-band and out-of-band pec Fundamental deign limitation for the loop Gorinevky Control Engineering 8-1 Modern Control Theory Appy reult

More information

ECEN620: Network Theory Broadband Circuit Design Fall 2018

ECEN620: Network Theory Broadband Circuit Design Fall 2018 ECEN60: Network Theory Broadband Circuit Deign Fall 08 Lecture 6: Loop Filter Circuit Sam Palermo Analog & Mixed-Signal Center Texa A&M Univerity Announcement HW i due Oct Require tranitor-level deign

More information

A Simplified Methodology for the Synthesis of Adaptive Flight Control Systems

A Simplified Methodology for the Synthesis of Adaptive Flight Control Systems A Simplified Methodology for the Synthei of Adaptive Flight Control Sytem J.ROUSHANIAN, F.NADJAFI Department of Mechanical Engineering KNT Univerity of Technology 3Mirdamad St. Tehran IRAN Abtract- A implified

More information

5.5 Application of Frequency Response: Signal Filters

5.5 Application of Frequency Response: Signal Filters 44 Dynamic Sytem Second order lowpa filter having tranfer function H()=H ()H () u H () H () y Firt order lowpa filter Figure 5.5: Contruction of a econd order low-pa filter by combining two firt order

More information

What lies between Δx E, which represents the steam valve, and ΔP M, which is the mechanical power into the synchronous machine?

What lies between Δx E, which represents the steam valve, and ΔP M, which is the mechanical power into the synchronous machine? A 2.0 Introduction In the lat et of note, we developed a model of the peed governing mechanim, which i given below: xˆ K ( Pˆ ˆ) E () In thee note, we want to extend thi model o that it relate the actual

More information

Estimation of Temperature Rise in Stator Winding and Rotor Magnet of PMSM Based on EKF

Estimation of Temperature Rise in Stator Winding and Rotor Magnet of PMSM Based on EKF 2010 3rd International Conference on Computer and Electrical Engineering (ICCEE 2010) IPCSIT vol. 53 (2012) (2012) IACSIT Pre, Singapore DOI: 10.7763/IPCSIT.2012.V53.No.2.37 Etimation of Temperature Rie

More information

Bogoliubov Transformation in Classical Mechanics

Bogoliubov Transformation in Classical Mechanics Bogoliubov Tranformation in Claical Mechanic Canonical Tranformation Suppoe we have a et of complex canonical variable, {a j }, and would like to conider another et of variable, {b }, b b ({a j }). How

More information

Pulsed Magnet Crimping

Pulsed Magnet Crimping Puled Magnet Crimping Fred Niell 4/5/00 1 Magnetic Crimping Magnetoforming i a metal fabrication technique that ha been in ue for everal decade. A large capacitor bank i ued to tore energy that i ued to

More information

SERIES COMPENSATION: VOLTAGE COMPENSATION USING DVR (Lectures 41-48)

SERIES COMPENSATION: VOLTAGE COMPENSATION USING DVR (Lectures 41-48) Chapter 5 SERIES COMPENSATION: VOLTAGE COMPENSATION USING DVR (Lecture 41-48) 5.1 Introduction Power ytem hould enure good quality of electric power upply, which mean voltage and current waveform hould

More information

7.2 INVERSE TRANSFORMS AND TRANSFORMS OF DERIVATIVES 281

7.2 INVERSE TRANSFORMS AND TRANSFORMS OF DERIVATIVES 281 72 INVERSE TRANSFORMS AND TRANSFORMS OF DERIVATIVES 28 and i 2 Show how Euler formula (page 33) can then be ued to deduce the reult a ( a) 2 b 2 {e at co bt} {e at in bt} b ( a) 2 b 2 5 Under what condition

More information

EE C128 / ME C134 Problem Set 1 Solution (Fall 2010) Wenjie Chen and Jansen Sheng, UC Berkeley

EE C128 / ME C134 Problem Set 1 Solution (Fall 2010) Wenjie Chen and Jansen Sheng, UC Berkeley EE C28 / ME C34 Problem Set Solution (Fall 200) Wenjie Chen and Janen Sheng, UC Berkeley. (0 pt) BIBO tability The ytem h(t) = co(t)u(t) i not BIBO table. What i the region of convergence for H()? A bounded

More information

Sensorless speed control including zero speed of non salient PM synchronous drives

Sensorless speed control including zero speed of non salient PM synchronous drives BULLETIN OF THE POLISH ACADEMY OF SCIENCES TECHNICAL SCIENCES Vol. 54, No. 3, 2006 Senorle peed control including zero peed of non alient PM ynchronou drive H. RASMUSSEN Aalborg Univerity, Fredrik Bajer

More information

Dynamic Simulation of a Three-Phase Induction Motor Using Matlab Simulink

Dynamic Simulation of a Three-Phase Induction Motor Using Matlab Simulink Dynamic Simulation of a ThreePhae Induction Motor Uing Matlab Simulink Adel Aktaibi & Daw Ghanim, graduate tudent member, IEEE, M. A. Rahman, life fellow, IEEE, Faculty of Engineering and Applied Science,

More information

CHAPTER 4 DESIGN OF STATE FEEDBACK CONTROLLERS AND STATE OBSERVERS USING REDUCED ORDER MODEL

CHAPTER 4 DESIGN OF STATE FEEDBACK CONTROLLERS AND STATE OBSERVERS USING REDUCED ORDER MODEL 98 CHAPTER DESIGN OF STATE FEEDBACK CONTROLLERS AND STATE OBSERVERS USING REDUCED ORDER MODEL INTRODUCTION The deign of ytem uing tate pace model for the deign i called a modern control deign and it i

More information

EE 508 Lecture 16. Filter Transformations. Lowpass to Bandpass Lowpass to Highpass Lowpass to Band-reject

EE 508 Lecture 16. Filter Transformations. Lowpass to Bandpass Lowpass to Highpass Lowpass to Band-reject EE 508 Lecture 6 Filter Tranformation Lowpa to Bandpa Lowpa to Highpa Lowpa to Band-reject Review from Lat Time Theorem: If the perimeter variation and contact reitance are neglected, the tandard deviation

More information

Singular perturbation theory

Singular perturbation theory Singular perturbation theory Marc R. Rouel June 21, 2004 1 Introduction When we apply the teady-tate approximation (SSA) in chemical kinetic, we typically argue that ome of the intermediate are highly

More information

Introduction to Laplace Transform Techniques in Circuit Analysis

Introduction to Laplace Transform Techniques in Circuit Analysis Unit 6 Introduction to Laplace Tranform Technique in Circuit Analyi In thi unit we conider the application of Laplace Tranform to circuit analyi. A relevant dicuion of the one-ided Laplace tranform i found

More information

POWER SYSTEM SMALL SIGNAL STABILITY ANALYSIS BASED ON TEST SIGNAL

POWER SYSTEM SMALL SIGNAL STABILITY ANALYSIS BASED ON TEST SIGNAL POWE YEM MALL INAL ABILIY ANALYI BAE ON E INAL Zheng Xu, Wei hao, Changchun Zhou Zheang Univerity, Hangzhou, 37 PChina Email: hvdc@ceezueducn Abtract - In thi paper, a method baed on ome tet ignal (et

More information

ECE 3510 Root Locus Design Examples. PI To eliminate steady-state error (for constant inputs) & perfect rejection of constant disturbances

ECE 3510 Root Locus Design Examples. PI To eliminate steady-state error (for constant inputs) & perfect rejection of constant disturbances ECE 350 Root Locu Deign Example Recall the imple crude ervo from lab G( ) 0 6.64 53.78 σ = = 3 23.473 PI To eliminate teady-tate error (for contant input) & perfect reection of contant diturbance Note:

More information

Lecture 8. PID control. Industrial process control ( today) PID control. Insights about PID actions

Lecture 8. PID control. Industrial process control ( today) PID control. Insights about PID actions Lecture 8. PID control. The role of P, I, and D action 2. PID tuning Indutrial proce control (92... today) Feedback control i ued to improve the proce performance: tatic performance: for contant reference,

More information

Tuning of High-Power Antenna Resonances by Appropriately Reactive Sources

Tuning of High-Power Antenna Resonances by Appropriately Reactive Sources Senor and Simulation Note Note 50 Augut 005 Tuning of High-Power Antenna Reonance by Appropriately Reactive Source Carl E. Baum Univerity of New Mexico Department of Electrical and Computer Engineering

More information

Sensorless PM Brushless Drives

Sensorless PM Brushless Drives IEEE UK Chapter Seminar 15 December 3 Senorle PM Bruhle Drive Prof. D. Howe and Prof. Z. Q. Zhu The Univerity of Sheffield Electrical Machine & Drive Reearch Group Outline Review of enorle technique Zero-croing

More information

CHAPTER 8 OBSERVER BASED REDUCED ORDER CONTROLLER DESIGN FOR LARGE SCALE LINEAR DISCRETE-TIME CONTROL SYSTEMS

CHAPTER 8 OBSERVER BASED REDUCED ORDER CONTROLLER DESIGN FOR LARGE SCALE LINEAR DISCRETE-TIME CONTROL SYSTEMS CHAPTER 8 OBSERVER BASED REDUCED ORDER CONTROLLER DESIGN FOR LARGE SCALE LINEAR DISCRETE-TIME CONTROL SYSTEMS 8.1 INTRODUCTION 8.2 REDUCED ORDER MODEL DESIGN FOR LINEAR DISCRETE-TIME CONTROL SYSTEMS 8.3

More information

SIMON FRASER UNIVERSITY School of Engineering Science ENSC 320 Electric Circuits II. Solutions to Assignment 3 February 2005.

SIMON FRASER UNIVERSITY School of Engineering Science ENSC 320 Electric Circuits II. Solutions to Assignment 3 February 2005. SIMON FRASER UNIVERSITY School of Engineering Science ENSC 320 Electric Circuit II Solution to Aignment 3 February 2005. Initial Condition Source 0 V battery witch flip at t 0 find i 3 (t) Component value:

More information

Control Systems Analysis and Design by the Root-Locus Method

Control Systems Analysis and Design by the Root-Locus Method 6 Control Sytem Analyi and Deign by the Root-Locu Method 6 1 INTRODUCTION The baic characteritic of the tranient repone of a cloed-loop ytem i cloely related to the location of the cloed-loop pole. If

More information

Correction for Simple System Example and Notes on Laplace Transforms / Deviation Variables ECHE 550 Fall 2002

Correction for Simple System Example and Notes on Laplace Transforms / Deviation Variables ECHE 550 Fall 2002 Correction for Simple Sytem Example and Note on Laplace Tranform / Deviation Variable ECHE 55 Fall 22 Conider a tank draining from an initial height of h o at time t =. With no flow into the tank (F in

More information

Simulations and Control of Direct Driven Permanent Magnet Synchronous Generator

Simulations and Control of Direct Driven Permanent Magnet Synchronous Generator Simulations and Control of Direct Driven Permanent Magnet Synchronous Generator Project Work Dmitry Svechkarenko Royal Institute of Technology Department of Electrical Engineering Electrical Machines and

More information

EE/ME/AE324: Dynamical Systems. Chapter 8: Transfer Function Analysis

EE/ME/AE324: Dynamical Systems. Chapter 8: Transfer Function Analysis EE/ME/AE34: Dynamical Sytem Chapter 8: Tranfer Function Analyi The Sytem Tranfer Function Conider the ytem decribed by the nth-order I/O eqn.: ( n) ( n 1) ( m) y + a y + + a y = b u + + bu n 1 0 m 0 Taking

More information

µ-analysis OF INDIRECT SELF CONTROL OF AN INDUCTION MACHINE Henrik Mosskull

µ-analysis OF INDIRECT SELF CONTROL OF AN INDUCTION MACHINE Henrik Mosskull -ANALYSIS OF INDIRECT SELF CONTROL OF AN INDUCTION MACHINE Henrik Mokull Bombardier Tranportation, SE-7 7 Väterå, Sweden S, Automatic Control, KTH, SE- Stockholm, Sweden Abtract: Robut tability and performance

More information

Given the following circuit with unknown initial capacitor voltage v(0): X(s) Immediately, we know that the transfer function H(s) is

Given the following circuit with unknown initial capacitor voltage v(0): X(s) Immediately, we know that the transfer function H(s) is EE 4G Note: Chapter 6 Intructor: Cheung More about ZSR and ZIR. Finding unknown initial condition: Given the following circuit with unknown initial capacitor voltage v0: F v0/ / Input xt 0Ω Output yt -

More information

A Constraint Propagation Algorithm for Determining the Stability Margin. The paper addresses the stability margin assessment for linear systems

A Constraint Propagation Algorithm for Determining the Stability Margin. The paper addresses the stability margin assessment for linear systems A Contraint Propagation Algorithm for Determining the Stability Margin of Linear Parameter Circuit and Sytem Lubomir Kolev and Simona Filipova-Petrakieva Abtract The paper addree the tability margin aement

More information

LTV System Modelling

LTV System Modelling Helinki Univerit of Technolog S-72.333 Potgraduate Coure in Radiocommunication Fall 2000 LTV Stem Modelling Heikki Lorentz Sonera Entrum O heikki.lorentz@onera.fi Januar 23 rd 200 Content. Introduction

More information

Overview: Induction Motors. Review Questions. Why the Rotor Moves: Motor Speed

Overview: Induction Motors. Review Questions. Why the Rotor Moves: Motor Speed Overview: nduction Motor Motor operation & Slip Speed-torque relationhip Equivalent circuit model Tranformer Motor efficiency Starting induction motor Smith College, EGR 35 ovember 5, 04 Review Quetion

More information

PI control system design for Electromagnetic Molding Machine based on Linear Programing

PI control system design for Electromagnetic Molding Machine based on Linear Programing PI control ytem deign for Electromagnetic Molding Machine baed on Linear Programing Takayuki Ihizaki, Kenji Kahima, Jun-ichi Imura*, Atuhi Katoh and Hirohi Morita** Abtract In thi paper, we deign a PI

More information

USING NONLINEAR CONTROL ALGORITHMS TO IMPROVE THE QUALITY OF SHAKING TABLE TESTS

USING NONLINEAR CONTROL ALGORITHMS TO IMPROVE THE QUALITY OF SHAKING TABLE TESTS October 12-17, 28, Beijing, China USING NONLINEAR CONTR ALGORITHMS TO IMPROVE THE QUALITY OF SHAKING TABLE TESTS T.Y. Yang 1 and A. Schellenberg 2 1 Pot Doctoral Scholar, Dept. of Civil and Env. Eng.,

More information

An estimation approach for autotuning of event-based PI control systems

An estimation approach for autotuning of event-based PI control systems Acta de la XXXIX Jornada de Automática, Badajoz, 5-7 de Septiembre de 08 An etimation approach for autotuning of event-baed PI control ytem Joé Sánchez Moreno, María Guinaldo Loada, Sebatián Dormido Departamento

More information

EELE 3332 Electromagnetic II Chapter 10

EELE 3332 Electromagnetic II Chapter 10 EELE 333 Electromagnetic II Chapter 10 Electromagnetic Wave Propagation Ilamic Univerity of Gaza Electrical Engineering Department Dr. Talal Skaik 01 1 Electromagnetic wave propagation A changing magnetic

More information

III.9. THE HYSTERESIS CYCLE OF FERROELECTRIC SUBSTANCES

III.9. THE HYSTERESIS CYCLE OF FERROELECTRIC SUBSTANCES III.9. THE HYSTERESIS CYCLE OF FERROELECTRIC SBSTANCES. Work purpoe The analyi of the behaviour of a ferroelectric ubtance placed in an eternal electric field; the dependence of the electrical polariation

More information

Molecular Dynamics Simulations of Nonequilibrium Effects Associated with Thermally Activated Exothermic Reactions

Molecular Dynamics Simulations of Nonequilibrium Effects Associated with Thermally Activated Exothermic Reactions Original Paper orma, 5, 9 7, Molecular Dynamic Simulation of Nonequilibrium Effect ociated with Thermally ctivated Exothermic Reaction Jerzy GORECKI and Joanna Natalia GORECK Intitute of Phyical Chemitry,

More information

S_LOOP: SINGLE-LOOP FEEDBACK CONTROL SYSTEM ANALYSIS

S_LOOP: SINGLE-LOOP FEEDBACK CONTROL SYSTEM ANALYSIS S_LOOP: SINGLE-LOOP FEEDBACK CONTROL SYSTEM ANALYSIS by Michelle Gretzinger, Daniel Zyngier and Thoma Marlin INTRODUCTION One of the challenge to the engineer learning proce control i relating theoretical

More information

Theory and Practice Making use of the Barkhausen Effect

Theory and Practice Making use of the Barkhausen Effect Theory and Practice aking ue of the Barkhauen Effect David C. Jile Anon arton Ditinguihed Profeor Palmer Endowed Chair Department of Electrical & Computer Engineering Iowa State Univerity Workhop on Large

More information

Nonlinear Single-Particle Dynamics in High Energy Accelerators

Nonlinear Single-Particle Dynamics in High Energy Accelerators Nonlinear Single-Particle Dynamic in High Energy Accelerator Part 6: Canonical Perturbation Theory Nonlinear Single-Particle Dynamic in High Energy Accelerator Thi coure conit of eight lecture: 1. Introduction

More information

Supplementary Figures

Supplementary Figures Supplementary Figure Supplementary Figure S1: Extraction of the SOF. The tandard deviation of meaured V xy at aturated tate (between 2.4 ka/m and 12 ka/m), V 2 d Vxy( H, j, hm ) Vxy( H, j, hm ) 2. The

More information

Moment of Inertia of an Equilateral Triangle with Pivot at one Vertex

Moment of Inertia of an Equilateral Triangle with Pivot at one Vertex oment of nertia of an Equilateral Triangle with Pivot at one Vertex There are two wa (at leat) to derive the expreion f an equilateral triangle that i rotated about one vertex, and ll how ou both here.

More information

A Simple Approach to Synthesizing Naïve Quantized Control for Reference Tracking

A Simple Approach to Synthesizing Naïve Quantized Control for Reference Tracking A Simple Approach to Syntheizing Naïve Quantized Control for Reference Tracking SHIANG-HUA YU Department of Electrical Engineering National Sun Yat-Sen Univerity 70 Lien-Hai Road, Kaohiung 804 TAIAN Abtract:

More information

EE 508 Lecture 16. Filter Transformations. Lowpass to Bandpass Lowpass to Highpass Lowpass to Band-reject

EE 508 Lecture 16. Filter Transformations. Lowpass to Bandpass Lowpass to Highpass Lowpass to Band-reject EE 508 Lecture 6 Filter Tranformation Lowpa to Bandpa Lowpa to Highpa Lowpa to Band-reject Review from Lat Time Theorem: If the perimeter variation and contact reitance are neglected, the tandard deviation

More information

Department of Mechanical Engineering Massachusetts Institute of Technology Modeling, Dynamics and Control III Spring 2002

Department of Mechanical Engineering Massachusetts Institute of Technology Modeling, Dynamics and Control III Spring 2002 Department of Mechanical Engineering Maachuett Intitute of Technology 2.010 Modeling, Dynamic and Control III Spring 2002 SOLUTIONS: Problem Set # 10 Problem 1 Etimating tranfer function from Bode Plot.

More information

LOAD FREQUENCY CONTROL OF MULTI AREA INTERCONNECTED SYSTEM WITH TCPS AND DIVERSE SOURCES OF POWER GENERATION

LOAD FREQUENCY CONTROL OF MULTI AREA INTERCONNECTED SYSTEM WITH TCPS AND DIVERSE SOURCES OF POWER GENERATION G.J. E.D.T.,Vol.(6:93 (NovemberDecember, 03 ISSN: 39 793 LOAD FREQUENCY CONTROL OF MULTI AREA INTERCONNECTED SYSTEM WITH TCPS AND DIVERSE SOURCES OF POWER GENERATION C.Srinivaa Rao Dept. of EEE, G.Pullaiah

More information

60 p. 2. A 200hp 600V, 60 Hz 3-phase induction motor has start code F. What line current should be expected at starting? 4 marks.

60 p. 2. A 200hp 600V, 60 Hz 3-phase induction motor has start code F. What line current should be expected at starting? 4 marks. EE 004 Final Solution : Thi wa a hr exam. A 60 Hz 4 pole -phae induction motor rotate at 740rpm. a) What i the lip? mark b) What i the peed o rotation o the rotor magnetic ield (in rpm)? mark The motor

More information

Analysis of Prevention of Induction Motors Stalling by Capacitor Switching

Analysis of Prevention of Induction Motors Stalling by Capacitor Switching 16th NTIONL POWER SYSTEMS CONFERENCE, 15th-17th DECEMER, 2010 260 nalyi of Prevention of Induction Motor Stalling by Capacitor Switching S.Maheh and P.S Nagendra rao Department of Electrical Engineering

More information

Lecture 12 - Non-isolated DC-DC Buck Converter

Lecture 12 - Non-isolated DC-DC Buck Converter ecture 12 - Non-iolated DC-DC Buck Converter Step-Down or Buck converter deliver DC power from a higher voltage DC level ( d ) to a lower load voltage o. d o ene ref + o v c Controller Figure 12.1 The

More information

Question 1 Equivalent Circuits

Question 1 Equivalent Circuits MAE 40 inear ircuit Fall 2007 Final Intruction ) Thi exam i open book You may ue whatever written material you chooe, including your cla note and textbook You may ue a hand calculator with no communication

More information

Linearteam tech paper. The analysis of fourth-order state variable filter and it s application to Linkwitz- Riley filters

Linearteam tech paper. The analysis of fourth-order state variable filter and it s application to Linkwitz- Riley filters Linearteam tech paper The analyi of fourth-order tate variable filter and it application to Linkwitz- iley filter Janne honen 5.. TBLE OF CONTENTS. NTOCTON.... FOTH-OE LNWTZ-LEY (L TNSFE FNCTON.... TNSFE

More information

Evolutionary Algorithms Based Fixed Order Robust Controller Design and Robustness Performance Analysis

Evolutionary Algorithms Based Fixed Order Robust Controller Design and Robustness Performance Analysis Proceeding of 01 4th International Conference on Machine Learning and Computing IPCSIT vol. 5 (01) (01) IACSIT Pre, Singapore Evolutionary Algorithm Baed Fixed Order Robut Controller Deign and Robutne

More information

Clustering Methods without Given Number of Clusters

Clustering Methods without Given Number of Clusters Clutering Method without Given Number of Cluter Peng Xu, Fei Liu Introduction A we now, mean method i a very effective algorithm of clutering. It mot powerful feature i the calability and implicity. However,

More information

THE IDENTIFICATION OF THE OPERATING REGIMES OF THE CONTROLLERS BY THE HELP OF THE PHASE TRAJECTORY

THE IDENTIFICATION OF THE OPERATING REGIMES OF THE CONTROLLERS BY THE HELP OF THE PHASE TRAJECTORY Mariu M. B LA Aurel Vlaicu Univerity of Arad, Engineering Faculty Bd. Revolu iei nr. 77, 3030, Arad, Romania, E-mail: mariu.bala@ieee.org THE IDENTIFICATION OF THE OPERATING REGIMES OF THE CONTROLLERS

More information

Designing scroll expanders for use in heat recovery Rankine cycles

Designing scroll expanders for use in heat recovery Rankine cycles Deigning croll expander for ue in heat recovery Rankine cycle V Lemort, S Quoilin Thermodynamic Laboratory, Univerity of Liège, Belgium ABSTRACT Thi paper firt invetigate experimentally the performance

More information

Math Skills. Scientific Notation. Uncertainty in Measurements. Appendix A5 SKILLS HANDBOOK

Math Skills. Scientific Notation. Uncertainty in Measurements. Appendix A5 SKILLS HANDBOOK ppendix 5 Scientific Notation It i difficult to work with very large or very mall number when they are written in common decimal notation. Uually it i poible to accommodate uch number by changing the SI

More information

Constant Force: Projectile Motion

Constant Force: Projectile Motion Contant Force: Projectile Motion Abtract In thi lab, you will launch an object with a pecific initial velocity (magnitude and direction) and determine the angle at which the range i a maximum. Other tak,

More information

LOW ORDER MIMO CONTROLLER DESIGN FOR AN ENGINE DISTURBANCE REJECTION PROBLEM. P.Dickinson, A.T.Shenton

LOW ORDER MIMO CONTROLLER DESIGN FOR AN ENGINE DISTURBANCE REJECTION PROBLEM. P.Dickinson, A.T.Shenton LOW ORDER MIMO CONTROLLER DESIGN FOR AN ENGINE DISTURBANCE REJECTION PROBLEM P.Dickinon, A.T.Shenton Department of Engineering, The Univerity of Liverpool, Liverpool L69 3GH, UK Abtract: Thi paper compare

More information

Direct Torque Control of Saturated Induction Machine with and without speed sensor

Direct Torque Control of Saturated Induction Machine with and without speed sensor Journal of Advanced Reearch in Science and Technology ISSN: 2352-9989 Direct Torque Control of Saturated Induction Machine with and without peed enor Tahar Djellouli,2, Samir Moulahoum, Med Seghir Boucherit

More information

Chapter 13. Root Locus Introduction

Chapter 13. Root Locus Introduction Chapter 13 Root Locu 13.1 Introduction In the previou chapter we had a glimpe of controller deign iue through ome imple example. Obviouly when we have higher order ytem, uch imple deign technique will

More information

ECE382/ME482 Spring 2004 Homework 4 Solution November 14,

ECE382/ME482 Spring 2004 Homework 4 Solution November 14, ECE382/ME482 Spring 2004 Homework 4 Solution November 14, 2005 1 Solution to HW4 AP4.3 Intead of a contant or tep reference input, we are given, in thi problem, a more complicated reference path, r(t)

More information

NCAAPMT Calculus Challenge Challenge #3 Due: October 26, 2011

NCAAPMT Calculus Challenge Challenge #3 Due: October 26, 2011 NCAAPMT Calculu Challenge 011 01 Challenge #3 Due: October 6, 011 A Model of Traffic Flow Everyone ha at ome time been on a multi-lane highway and encountered road contruction that required the traffic

More information

CONTROL OF INTEGRATING PROCESS WITH DEAD TIME USING AUTO-TUNING APPROACH

CONTROL OF INTEGRATING PROCESS WITH DEAD TIME USING AUTO-TUNING APPROACH Brazilian Journal of Chemical Engineering ISSN 004-6632 Printed in Brazil www.abeq.org.br/bjche Vol. 26, No. 0, pp. 89-98, January - March, 2009 CONROL OF INEGRAING PROCESS WIH DEAD IME USING AUO-UNING

More information

Stability regions in controller parameter space of DC motor speed control system with communication delays

Stability regions in controller parameter space of DC motor speed control system with communication delays Stability region in controller parameter pace of DC motor peed control ytem with communication delay Şahin Sönmez, Saffet Ayaun Department of Electrical and Electronic Engineering, Nigde Univerity, 5124,

More information

Lecture 5 Introduction to control

Lecture 5 Introduction to control Lecture 5 Introduction to control Tranfer function reviited (Laplace tranform notation: ~jω) () i the Laplace tranform of v(t). Some rule: ) Proportionality: ()/ in () 0log log() v (t) *v in (t) () * in

More information

6.447 rad/sec and ln (% OS /100) tan Thus pc. the testing point is s 3.33 j5.519

6.447 rad/sec and ln (% OS /100) tan Thus pc. the testing point is s 3.33 j5.519 9. a. 3.33, n T ln(% OS /100) 2 2 ln (% OS /100) 0.517. Thu n 6.7 rad/ec and the teting point i 3.33 j5.519. b. Summation of angle including the compenating zero i -106.691, The compenator pole mut contribute

More information

A FUNCTIONAL BAYESIAN METHOD FOR THE SOLUTION OF INVERSE PROBLEMS WITH SPATIO-TEMPORAL PARAMETERS AUTHORS: CORRESPONDENCE: ABSTRACT

A FUNCTIONAL BAYESIAN METHOD FOR THE SOLUTION OF INVERSE PROBLEMS WITH SPATIO-TEMPORAL PARAMETERS AUTHORS: CORRESPONDENCE: ABSTRACT A FUNCTIONAL BAYESIAN METHOD FOR THE SOLUTION OF INVERSE PROBLEMS WITH SPATIO-TEMPORAL PARAMETERS AUTHORS: Zenon Medina-Cetina International Centre for Geohazard / Norwegian Geotechnical Intitute Roger

More information