Control and simulation of doubly fed induction generator for variable speed wind turbine systems based on an integrated finite element approach
|
|
- Jody Cunningham
- 6 years ago
- Views:
Transcription
1 Control and iulation of doubly fed induction generator for variable peed wind turbine yte baed on an integrated finite eleent approach Qiong-zhong Chen*, Michel Defourny #, Olivier Brül* * Univerity of iège, Departent of Aeropace and Mechanical Engineering (TAS) Chein de Chevreuil (B52/3), 4000 iège, Belgiu Eail: qz.chen@ulg.ac.be, o.brul@ulg.ac.be # SAMTECH Headquarter, iège cience park, Rue de Chaeur-Ardennai 8, 403 iège (Angleur), Belgiu Eail: ichel.defourny@atech.co Abtract: Regarding renewable energy and environentfriendly iue, wind energy nowaday ha becoe the fatet-growing energy ource in the world, and thu attract a lot of reearch interet in the wind turbine generation yte. A doubly fed induction generator (DFIG) i ued for variable peed operation in a wind turbine yte to extract ore power. Following a yteatic approach, thi paper invetigate on the odelling and iulation of wind turbine generating yte uing the flexible ultibody iulation oftware SAMCEF/MECANO []. The objective of thi work i to analyze the control-generator-tructure interaction in a wind turbine yte. Firtly, an extenion of the finite eleent ethod i integrated into the flexible ultibody dynaic olver, and thu extend the olver to repreent echatronic yte in a trongly-coupled way. Secondly, DFIG and the control yte are odularly odeled for the wind turbine package. Control of DFIG for grid ynchronization and power optiization are elaborated in detail, and the ethod are validated through a 2MW DFIG wind turbine prototype odel. At the end, a yteatic yte odel of wind turbine tructure connected with the DFIG generating yte i preented, which provide the dynaic analyi for the whole yte in an overall range. Keyword: DFIG, wind turbine, control, trongly-coupled finite eleent approach Introduction A one of the ot proiing renewable energy ource, wind power ha ubtantially increaed for the pat decade and i evaluated a the bet choice to fill the electricity generation gap according to the publihed finding by the International Energy Agency (IEA) in A wind turbine yte i ued to convert wind energy into electrical energy. For a given turbine blade airfoil, the power extracted fro an air trea depend on the wind peed, the air denity and alo the turbine rotating peed. Since wind cannot be controlled, turbine rotating peed i then controlled for optiizing wind power extraction. Therefore, a variable-peed wind turbine i of higher energy efficiency than fixed-peed wind turbine. Beide, variable peed operation can reduce echanical tre on turbine tructure and i claied to be better for acoutic noie reduction [2]. Variable-peed wind turbine are typically baed on a doubly-fed induction generator (DFIG), which can operate over a lip range of /-30% and thu enable the turbine to extract the axiu power fro the wind with variable operating peed. One iportant advantage of DFIG in the application of wind turbine, epecially large-power wind turbine, i that only a lip power, typically 20-30% of the total power, ha to be handled by the bidirectional rotor converter. Conequently, both the power rating requireent and loe can be highly reduced. For the control of a wind-turbine-driven DFIG, different trategie like direct torque control (DTC) and variable tructure control (VSC) have been propoed over the lat decade [3]. However, one coon way i to ue vector control on the bai of d,q-tranforation with tator-flux orientation or tator-voltage orientation (alo referred to a grid-voltage or grid-flux orientation) [4]. Typically, two way can be ued for vector control chee. One i by ean of integral-proportional (IP) regulator and the other i by proportional-integral (PI) regulator. The difficulty then lie in the configuration and the deterination of the coefficient of the regulator. Since a wind turbine yte i a hybrid yte featuring not only echanical tructure, but alo aerodynaic, control yte and the coupling interaction in-between. Coputer-aided tool
2 provide a way to reduce cot and iprove efficiency in the deign of wind turbine yte. While pecializing on the echanical tructure and the otion, ot coercial finite eleent ethod (FEM) baed wind turbine oftware can be extended to repreent non-echanical yte by ipleenting a uer-eleent in a weakly-coupled way, which ean that pecific olver are ued for control yte and echanical ubyte repectively, and data are exchanged only at particular counication tie [5]. However, ince the dynaic of the actuator or generator are continuou in tie, weakly-coupled approache could lead to large nuerical error if the tie tep are not et all enough. Thi ethod ight be quite intricate in application, and oetie even unreliable. On thi account, the developent of an integrated flexible ultibody dynaic olver baed on a trongly-coupled ethod would be iportant for achieving better reliability and efficiency. Aong the wind turbine oftware, Sacef for Wind Turbine (S4WT) i baed on the flexible ultibody dynaic olver Sacef/Mecano []. Funded by the Walloon governent, Satech and the Univerity of iège are jointly engaged to develop and iprove the wind-tubine oftware package S4WT under the project Dynawind. The general ai i to develop a coputer-aided tool for cutoization, fatprototyping and optial deign of wind turbine yte baed on the dynaic iulation of the overall yte. Sacef/Mecano offer everal option to include control yte and other non-echanical yte in a nuerical odel. For intance, it i poible to link a D decribing a control algorith or to ue a co-iulation interface with Matlab/Siulink. The proble i then olved according to a weakly coupled trategy. Beide the weakly-coupled approache, functionalitie to decribe the control yte according to the block diagra language have newly been integrated into the flexible ultibody dynaic olver, and thu extend the olver to repreent echatronic yte in a trongly-coupled way [6]. The work preented in thi paper i a contribution by Dynawind. It feature the odelling and control of wind turbine DFIG yte baed on a trongly coupled finite eleent approach. The reaining ection of the paper are organized into three ain part. In the firt part, dynaic odelling of DFIG and it control trategie for variable peed operation are elaborated in detail. The econd part decribe the trongly-coupled iulation approach and the odularly odelling ethod of DFIG control yte on Sacef. Syteatic exaple are given in the lat part for the validation of the odel, the control trategie and the trongly-coupled iulation approach, and alo for the analyi of the control-generator-tructure interaction. 2 Dynaic odel of DFIG For deriving decoupled vector control law for a DFIG, d-q tranforation i ued to ap the 3-phae tator and rotor winding into two orthogonal fictitiou coil with the tator-flux-oriented reference frae. A generalized 5 th order atheatic odel i ued for the odelling of DFIG. For power yte tudie, it i a coon way to ue a per-unit repreentation [7], where the quantitie are expreed a fraction of the bae value. Aue that the tator current i poitive when flowing fro the grid to the achine, then the voltage expreion can be repreented a follow: d v d = R id ψ q ψd ω d v q = R i q ψ d ψq ω d v = R i ψ ψ d v = R i ψ ψ dr r dr l qr dr ω qr r qr l dr qr ω, () where the following notation i ued: v: voltage; i: current; ψ: flux linkage; R, R r : tator and rotor reitance; ω : ynchronou angular peed in electrical eaureent; l : rotor lip; the ubcript d and q repreent the d- and q-axi tator coponent repectively, dr and qr, the d- and q-axi rotor coponent repectively; the upercript "-", a hereinafter defined, indicate per-unit repreentation. The flux linkage equation are: ψ = i i ψ = i i ψ = i i ψ = i i d d dr q q qr dr r dr d qr r qr q, (2) where repreent the tator inductance, r i the rotor inductance and i the utual inductance between the tator and the rotor. The electroagnetic torque expreion can be derived a: Te = ψdiq ψqid. (3) The active and reactive power at the tator and rotor are repectively: P = V i V i, Q = V i V i P = V i V i, Q = V i V i d d q q q d d q r dr dr qr qr r qr dr dr qr, (4)
3 where P repreent the tator active power, Q i the tator reactive power, P r i the rotor active power and Q r i the rotor reactive power. 3 Control of DFIG Wind turbine Gear box SWr DFIG RSC AC/ DC SW GSC DC/ AC Tranforer SWg Grid Figure : A cheatic configuration of a DFIG wind turbine Grid ynchronization and power control are two control ode of a DFIG in a turbine yte. For a better undertanding of the control proce, it i worth briefly tating the working proce of the wind turbine yte. A cheatic configuration of a DFIG wind turbine i hown in Fig.. In the beginning fro tandtill, the DFIG i diconnected fro the grid. Wind peed i eaured by an aneoeter. Once it reache the cut-in value, the brake i releaed and the rotor blade are driven by the pitch regulation echani fro the feathering poition to a pre-optiized angle. The echanical torque created by the aerodynaic lift fro the blade drive the haft to rotate. At the ae oent, the witch SWg i on, and the dc-link voltage in the bidirectional converter i oon charged. When the rotating peed of the wind turbine reache a certain value (e.g % of the rated peed), SWr i turned on and the oft grid ynchronization proce tart. For variable-peed wind turbine, grid ynchronization i poible at any operational peed. Uually, grid ynchronization proce take le than one econd [8]. Once thi proce i accoplihed, SW i turned on and the tator of the DFIG i connected to the grid, and then the power control ode, which coprie active power optiization and reactive power control, tart. Active power control i for tracking a predefined power-peed characteritic profile and reactive power control i to control the power factor at the grid terinal. DFIG i controlled via the converter on the rotor. The grid ide converter (GSC) i controlled to aintain a contant dc-link voltage and to guarantee the operation of the converter with unity power factor, i.e., zero reactive power [9]. The rotor ide converter (RSC) i controlled for both grid ynchronization and power optiization. To oe degree, RSC can be conidered a a current-controlled voltage ource. Baed on d,q-tranforation with the tator-flux oriented reference frae, control on the d,q-axi rotor current can be decoupled for active and reactive power. Conidering that the tator reitance i coparatively very all, the grid flux orientation align with the tator flux orientation without any ignificant error [4]. On thi account, both the tator-flux-oriented reference and the grid-voltage-oriented reference can be ued for vector control. 3. Grid ynchronization Grid ynchronization control i to regulate the voltage, frequency and phae angle at the tator terinal to be the ae a thoe of the grid before connection. Uing the grid-voltage oriented reference frae, the ynchronization requireent can be forulated a: vd = 0 p.u. v q = v grid = p.u., (5) where v grid repreent the grid voltage aligned with the quadrature axi. Given that the tator i open, the tator current equal zero. Subtitute the flux linkage forulation (2) into equation (), then the tator voltage expreion can be rewritten a: d v = i i d v q = i dr iqr ω d qr dr ω. (6) Cobine equation (5) and (6), and coponent of rotor current in teady tate hould be a: vd i dr= = i qr= 0. (7) Conequently, thee are the reference input to the current controller for grid ynchronization. Since RSC i conidered a a current-controlled voltage ource, rotor voltage expreion can be rewritten a follow by ubtituting equation (2) into () and leaving out the tator current ter: d v = R i i i d v = R i i i r dr r dr l r qr dr ω r qr r qr l r dr qr ω. (8) Then the tranfer function between the rotor current and the rotor voltage can be written in ter of the coplex variable a: i ( ) dr ( ) iqr Gr ( ) = = v ( ) v ( ) R ( / ω ) =. (9) dr qr r r
4 idrref FF ter C dr () % i% l r qr i V dr l r qr DFIG G r () idr α α α R C = G =, (0) r r dr ( ) r ( ) ω where α i a IMC deign paraeter. In the cae of a firt-order yte, α i et to be the deired bandwih of the cloed-loop yte. The relationhip between the bandwih and the rie tie i α =ln9/t rie, where t rie repreent the rie tie [4]. Figure 2: Control bock of q-axi rotor current for grid ynchronization Take the d-axi rotor current control for intance. The control block i hown a Fig. 2, where C dr () repreent a PI controller. The paraeter of the PI controller can be derived by the internal odel control (IMC) ethod a: The ter l r i qr can be conidered a a diturbance. A diturbance etiation i exploited a a feed-forward ter for copenation, a hown in the red box in Fig. 2. However, it i alo poible to introduce an "active daping" factor to the control loop, o that the diturbance can be daped with the ae tie contant a the control dynaic [4]. ω ref C Tω () T eref C it () i qrref C viqr () v qr ω i qr Qref C iq () i drref C vidr () vdr DFIG i dr Figure 3: Decoupled peed (active power) and reactive power control of DFIG 3.2 Active power optiization control A entioned before, DFIG i controlled according to a predefined power-peed characteritic profile to optiize the wind power extraction. Thu, the active power optiization control i actually the peed control. According to decoupled d-q axi apping, d- and q-axi rotor current coponent are controlled for reactive and active power repectively. Cacaded PI or IP controller are ued, and the IMC or pole placeent ethod i ued repectively to derive the paraeter of the controller. Active power control coprie 3 cacaded loop: q-axi rotor current control, torque control and peed control, while the reactive power control coprie reactive power and d-axi rotor current control. A cheatic diagra of the decoupled peed (active power) and reactive power control i hown in Fig. 3, where the controller are either IP or PI regulator except for the torque control part. Conidering that torque i difficult to be eaured, it i ot often controlled in an open-loop anner [4] Current control To derive decoupled rotor current control law, everal condition hould be noted beforehand. Fro equation (), ψ and ψ approxiately equal vq and d vd repectively in teady tate. Thu, ψ d v q = p.u. ψ q v d = 0 p.u. q. () Then, according to d,q-axi tator flux linkage forulation in equation (2): Denote ( ), i i i i d dr q qr X = r 2. (2), and ubtitute the rotor flux linkage equation (2) and the tator-rotor current equation (2) into the rotor voltage equation (), then, where X d v = R i i E qr r qr qr qr ω Eqr = l X idr, (3) can be treated a a diturbance. Thu, the tranfer function between the
5 rotor current and the rotor voltage i: G viqr Iqr ( ) ( ) = = Vqr ( ) X Rr ω. (4) Siilar to that of the grid ynchronization proce, the paraeter of the PI controller can be derived by the IMC ethod a: α α X α R C = G =. (5) r viqr ( ) qr ( ) ω Torque control Torque can be expreed in the for of controllable q-axi rotor current by ubtituting equation (-2) into (3): T i e = qr. (6) The tranfer function between the q-axi rotor current and the torque then becoe iqr ( ) CiT ( ) = =, (7) T ( ) which i ued for the open-loop torque control Speed control e The inertia of the rotating wind turbine yte i very high. However, copared to the turbine itelf and the generator rotor, the inertia of the haft i negligibly all [0]. Fro the generator rotor point of view and neglecting the haft inertia, the echanical balance equation can then be derived a []: TT JT dωr Te = J g 2 ηn ηn, (8) where T T i the turbine torque created by the aerodynaic lift on the blade; T e i the generator electroagnetic torque, id. et., the reiting torque; J g i the inertia of the generator rotor itelf; J T i the inertia of the turbine; n i the gearbox reduction ratio; η i the energy traniion efficiency; ω r i the rotating peed of the generator rotor in echanical eaureent. Norally, the wind turbine i a lot heavier than the generator, and J T /ηn 2 i larger than the generator rotor inertia [0]. Denote the equivalent inertia and the input torque by J and T repectively, the above equation can be rewritten a: d =, (9) ωr T Te J Since the torque to peed loop i a pure integral eleent, an IP regulator i ued for the peed control to derive a econd-order for for the cloed-loop yte, a hown in Fig. 4. Conidering that current dynaic are uch fater than peed dynaic, the electroagnetic torque T e can be expreed a T eref. ω ref K i / T eref K p T /(J) Figure 4: Control block of the peed The tranfer function of the cloed loop yte turn to be a tandard econd-order for a: ω ( ) K /J = ω K /J K /J r i 2 ref ( ) ( p ) i ω r. (20) The paraeter of the controller are then tuned through pole placeent. Denote the daping factor and the natural frequency of the econd order yte by ζ d and ω nd repectively, and the paraeter of the IP controller can then be given by: K p= 2ζ dωnd J 2 K i= ωnd J. (2) There are oe approxiation ethod on evaluating the relationhip between the ettling tie t d and ζ d and ω nd. In a particular ituation of an over-daped yte, ω nd 5.8/t d [3]. Once the deired dynaic repone i evaluated, the IP controller paraeter can then be tuned accordingly. et' recall that the ynchronization proce i very fat, uually le than 00, and once it i accoplihed, right after the power control proce tart. Conidering that the inertia of a wind turbine i very high, the peed i alot contant during the ynchronization. Therefore, the initial value of the integral ter of the IP controller can be accordingly et a ω t K p /K i, where ω t tand for the predefined initial peed of the ynchronization. 3.3 Reactive power control A entioned above, the converter GSC i controlled to operate with unity power factor. Thi ean that the traniion of reactive power between DFIG and the grid i only through the tator [9]. The reactive power at the grid terinal i then equal to the tator reactive power: Q = Q = v i v i, (22) q d d q ikewie, ubtitute equation (5) and (2) into (22) and the expreion can be derived in the for of controllable d-axi rotor current a:
6 Then, Q = ( i dr ) i dr= ( Q ). (23). (24) Particularly, when the deired tator reactive power i zero, then i =. (25) dr The current control in the reactive control loop i iilar to that of the peed (active power) control loop, and will not be reiterated here. 4 Strongly coupled approach and odelling ethod on Sacef 4. Strongly coupled approach A coupled echatronic proble can be odularly decopoed into a echanical yte and a control yte. The echanical yte can be odelled uing the finite eleent flexible ultibody forali, and the control yte i uually decribed uing block diagra language. To olve the coupled proble, nuerical tie integration ethod have to be applied for both ubyte. In the cae of a weak coupling approach, repective integration olver are ued for the ubyte accordingly. The coupling of the ubyte then iplie the coupling of the different olver, o that tability and convergence propertie can be affected [5]. For the cae of a trongly-coupled approach, only one optiized olver i applied to both ubyte o that the required order of accuracy and tability can be eaily enured for the iulation of a echatronic yte. In flexible ultibody dynaic, the Newark faily of iplicit olver have been applied extenively. To extend the olver to repreent a echatronic yte, an extended generalized-α ethod i propoed in reference [6]. Baed on that, an integrated olver ha newly been developed into Sacef for the iulation of flexible ultibody tructure coupled with non-echanical ubyte. The forulation relie on a odular block diagra decription of the control yte, which i now available on Sacef. y ( q, q&, q&&, λ ) Mechani Control yte Figure 5: Scheatic diagra of the coupling in a echatronic yte Baed on the finite eleent ethod for the echanical part and on the block diagra language for the control part, a echatronic yte can be decribed a hown in Fig. 5, where q i the vector of echanical coordinate, λ i the vector of agrange ultiplier related with the kineatic contraint and y i the vector of control output. The dynaic can be repreented by the following coupled equation: Mq && Φ ( λ Φ) g(q,q, & ) y 0 T a q k p t = kφ(q) = 0 x& f (q,q,q,λ, & && x, y, t) = 0 y h(q,q,q,λ, & && x, y, t) = 0, (26) where the firt two equation are the equation of otion of the echanical ubyte and the lat two equation are the tate pace equation of the control ubyte. a i the output localization atrix, the ter a y repreent the generalized force exerted by the actuator and generator on the echanical yte, x i the vector of control tate variable and the other ybol are coonly known and can be referred to [6]. The trongly coupled echanical and tate equation are obtained by nuerical aebly and their tie-doain iulation i baed on an extenion of the generalized-α ethod. A detailed decription of the tie integration algorith can be found in [6]. 4.2 Modular odelling of DFIG control yte on Sacef With the integration of the new trongly-coupled olver, the DFIG control yte were odelled for S4WT. The yte i decopoed into ubyte and odularized. Decopoition i baed on the analyi of the function of each coponent. All odel, including the generator itelf and the controller, are aied at general-purpoe ue. Extra node are introduced to repreent the tate and output variable fro the generating control yte, which i iilar to the way for the tructure yte. A tangent atrix can then be derived for the Newton iteration, with difference in the coefficient for tate variable and tructural node. 5 Siulation and validation In thi ection, two iulation exaple will be preented for validating the odel of the DFIG control yte and alo the trongly-coupled olver. A 2MW DFIG prototype odel i ued for the iulation analyi. The paraeter of the DFIG are lited a follow [7]:
7 Bae voltage (line-to-line): V bae = 690 V; Bae power: P bae = 2 MW; Grid frequency: f = 50 Hz; Nuber of pole: n p = 4; Stator reitance: R = p.u.; Rotor reitance : R r = p.u.; Stator eakage inductance: l = p.u.; Rotor leakage inductance: rl = p.u.; Mutual inductance: = p.u.. The inertia of the generator itelf i 00kg 2. However, ince the inertia of the wind turbine yte i barely known, everal etiation ethod are dicued in reference [2]. Uually, the inertia tie contant of a 2MW wind turbine range fro 3.5 to 6. For the per-unit repreentation, here in thi paper, the bae current i defined a I bae =P bae /V bae ; the bae reitance R bae = V bae /I bae = ω bae, where bae i the bae inductance; the bae flux linkage ψ bae =V bae /ω ; the bae peed ω bae =2ω /n p ; and conequently the bae torque T bae =P bae /ω bae. 5. DFIG alone with defined torque input In thi ection, a iple exaple of the DFIG running alone with defined driving torque i tudied. The purpoe of thi iulation exaple i to verify the odel and the control trategie. The DFIG i operating given p.u. driving torque in the very beginning. When the peed reache 0.8p.u. of the bae peed, the ynchronization proce tart. Once thi proce i copleted, then right away tart the peed and reactive power control. Initially, the reference peed i et to be p.u.. Then after 4, it i changed to 0.9p.u., and again, it i changed to.p.u. fro 6. Finally, while aintaining the ae reference peed, the driving torque i raped down to 0.5p.u. fro 8.5 to 9.5. A for the paraeter of the controller, ince the dynaic of the electrical yte i uch fater than the echanical yte, the rie tie for the current control loop i et to 0 (α = 29 for the PI controller), while the ettling tie for the peed control loop i et to (ζ d =, ω nd =5.8 for the IP controller). For the integrated FEM olver, an autoatic tie tep chee i ued for the iulation. Selected iulation reult are hown in Fig. 6. Fig.6(a) how the grid ynchronization proce of the A-phae tator voltage with the A-phae grid voltage. Thi proce take only about 25. A one can ee fro Fig.6(b) and Fig.6(c), the repone for both peed and reactive power control are atifactory. Fro Fig.6(d), it can be eaily derived that peed control i deterined by the control of q-axi rotor current and reactive power control i by the d-axi rotor current, and thu they are decoupled. ynchronization tart ynchronization finihe (a) (b) i qr i dr (c) (d) Figure 6: DFIG alone: (a) Grid ynchronization repone; (b) Speed repone; (c) Stator reactive power; (d) q,d-axi rotor current.
8 Figure 7: A odel of wind turbine generating yte on S4WT ynchronization tart ynchronization finihe Power 8/ / Turbine peed (a) (b) i dr Reactive power i qr Active power (c) (d) Figure 8: Full wind turbine repone: (a) Grid ynchronization proce; (b) Speed repone with different wind peed; (c) Power output; (d) q,d-axi rotor current. 5.2 The integration of the wind turbine tructure odel with the DFIG odel A yteatic odel of a 2MW wind turbine integrated with the DFIG odel i preented in thi ection. The odel on S4WT i hown in Fig. 7. Soe elected paraeter of the turbine yte are a: 4 of blade length, 75 of tower height and 06 of the gearbox ratio. The blade are odeled a elatic bea and the aerodynaic load are coputed uing the blade eleent oentu theory, ee [3] for ore detail about the underlying forulation. The interet here i to analyze the control-generator-tructure interaction in a wind turbine yte. An approxiate inertia tie contant 3.5 i ued for deriving the IP controller paraeter. However, ince it' difficult to be accurate, a higher daping factor could be ued for the econd-order yte of the cloed peed control loop. Given that the inertia of the turbine yte i very large, the ettling tie i et a 2.5. A for the PI controller, the ae paraeter are ued a thoe in the previou
9 exaple. The iulation ituation i a follow. The initial wind peed i et to 8/ and the initial turbine peed i to be.rad/ (accordingly 0.74p.u.). The aerodynaic torque drive the turbine to rotate. Grid ynchronization control tart when the generator rotating peed reache 0.8p.u.. After 8, the wind peed change to /. For 8/ of the wind peed, the axiu wind power i aued to be extracted with 0.9p.u. of the rotating peed, while.p.u. i that for a wind peed of /. A wind power-peed characteritic diagra i hown on the botto right of Fig. 8(b). Alo, an autoatic tie tep chee i applied. Selected iulation reult are hown in Fig Concluion Thi paper tudie the odelling and control of DFIG in variable-peed wind turbine yte baed on an integrated, trongly-coupled finite eleent approach. New block diagra functionalitie for the decription of control yte are integrated into Sacef/Mecano ultibody dynaic olver. Thi allow the iulation of echatronic yte in a trongly-coupled way, o that the intricacy and uncertainty of uing a third-party control engineering oftware can be avoided. The DFIG generator and the controller odel are developed in a odular, paraeterized way. They are built to expand the MECANO wind turbine package, and are alo aied at general-purpoe ue baed upon trongly-coupled iulation. Detailed control trategie are preented for grid ynchronization and power optiization. Siulation reult how the validity of the DFIG odel and the trongly-coupled iulation approach. A coprehenive wind turbine yte odel i preented to analyze the coupling effect aong different coponent. Control of the generator will influence both the energy extraction and the echanical tructure life due to the utual coupling. Acknowledgeent Thi reearch work wa carried out under grant nuber (DYNAWIND) fro the Walloon Region (Belgiu) which i gratefully acknowledged. Reference Superregui, A., "Methodology for ooth connection of doubly fed induction generator to the grid", IEEE Tranaction on Energy Converion, 2009, 24, [4]. Peteron, A., Analyi, odeling and control of Doubly-Fed Induction Generator for wind turbine, PhD thei, Chaler Univerity of Technology, Göteborg, Sweden, [5]. Buch, M. and Schweizer, B., "Nuerical Stability and Accuracy of Different Co-Siulation Technique: Analytical Invetigation Baed on a 2-DOF Tet Model", Proceeding of the t Joint International Conference on Multibody yte Dynaic, appeenranta, Finland, May 25-27, 200. [6]. Brül, O. and Golinval, J. C., "The generalized-α ethod in echatronic application", Zeitchrift für angewane atheatik und echanik (ZAMM), 2006, 86, [7]. Ekanayake, J. B., Holdworth,. and Jenkin N., "Coparion of 5th order and 3rd order achine odel for doubly fed induction generator (DFIG) wind turbine", Electric Power Syte Reearch, 2003, 67, [8]. Goez, S. A. and Aenedo, J.. R., "Grid ynchroniation of doubly fed induction generator uing direct torque control", Proceeding of IEEE 28th Annual conference of the Indutrial Electronic Society, Sevilla, Spain, Nov. 5-8, [9]. Hanen, A. D., Sørenen, P., Iov, F. and Blaabjerg, F., "Centralied power control of wind far with doubly fed induction generator", Renewable Energy, 2006, 3, [0]. Rotoen, H. O., Undeland, T. M. and Gjengedal T., "Doubly fed induction generator in a wind turbine", Proceeding of the IEEE/Cigre workhop on wind power and the ipact on power yte, Olo, Norway, Jun. 7-8, []. Cetinkunt, S., Mechatronic, John Wiley & Son, Inc., Hoboken, New Jerey, [2]. Rodriguez, A. G. G., Iproveent of a fixed-peed wind turbine oft-tarter baed on a liding-ode controller, PhD thei, Univerity of Seville, Seville, Spain, [3]. Heege, A., Betran, J. and Radovcic, Y., "Fatigue load coputation of wind turbine gearboxe by coupled finite eleent, ulti-body yte and aerodynaic analyi", Wind Energy, 2007, 0, []. Géradin, M. and Cardona, A., Flexible ultibody dynaic: a finite eleent approach, John Wiley & Son, New York, 200. [2]. Chowdhury, B. H. and Chellapilla, S., "Double-fed induction generator control for variable peed wind power generation", Electric Power Syte Reearch, 2006, 76, [3]. Tapia, G. Santaaria, G. Telleria, M. and
Control and simulation of doubly fed induction generator for variable speed wind turbine systems based on an integrated Finite Element approach
Control and simulation of doubly fed induction generator for variable speed wind turbine systems based on an integrated Finite Element approach Qiong zhong Chen*, Michel Defourny #, Olivier Brüls* *Department
More informationThe Extended Balanced Truncation Algorithm
International Journal of Coputing and Optiization Vol. 3, 2016, no. 1, 71-82 HIKARI Ltd, www.-hikari.co http://dx.doi.org/10.12988/ijco.2016.635 The Extended Balanced Truncation Algorith Cong Huu Nguyen
More informationADAPTIVE CONTROL DESIGN FOR A SYNCHRONOUS GENERATOR
ADAPTIVE CONTROL DESIGN FOR A SYNCHRONOUS GENERATOR SAEED ABAZARI MOHSEN HEIDARI NAVID REZA ABJADI Key word: Adaptive control Lyapunov tability Tranient tability Mechanical power. The operating point of
More informationControl of industrial robots. Decentralized control
Control of indutrial robot Decentralized control Prof Paolo Rocco (paolorocco@poliiit) Politecnico di Milano Dipartiento di Elettronica, Inforazione e Bioingegneria Introduction Once the deired otion of
More informationSection 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 informationScale Efficiency in DEA and DEA-R with Weight Restrictions
Available online at http://ijdea.rbiau.ac.ir Int. J. Data Envelopent Analyi (ISSN 2345-458X) Vol.2, No.2, Year 2014 Article ID IJDEA-00226, 5 page Reearch Article International Journal of Data Envelopent
More informationGain 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 informationDynamic 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 informationA New Model and Calculation of Available Transfer Capability With Wind Generation *
The Eighth International Sypoiu on Operation Reearch and It Application (ISORA 09) Zhangjiajie, China, Septeber 0, 009 Copyright 009 ORSC & APORC, pp. 70 79 A New Model and Calculation of Available Tranfer
More informationImage Denoising Based on Non-Local Low-Rank Dictionary Learning
Advanced cience and Technology Letter Vol.11 (AT 16) pp.85-89 http://dx.doi.org/1.1457/atl.16. Iage Denoiing Baed on Non-Local Low-Rank Dictionary Learning Zhang Bo 1 1 Electronic and Inforation Engineering
More informationCHAPTER 13 FILTERS AND TUNED AMPLIFIERS
HAPTE FILTES AND TUNED AMPLIFIES hapter Outline. Filter Traniion, Type and Specification. The Filter Tranfer Function. Butterworth and hebyhev Filter. Firt Order and Second Order Filter Function.5 The
More informationMODE SHAPE EXPANSION FROM DATA-BASED SYSTEM IDENTIFICATION PROCEDURES
Mecánica Coputacional Vol XXV, pp. 1593-1602 Alberto Cardona, Norberto Nigro, Victorio Sonzogni, Mario Storti. (Ed.) Santa Fe, Argentina, Noviebre 2006 MODE SHAPE EXPANSION FROM DATA-BASED SYSTEM IDENTIFICATION
More informationPeriodic Table of Physical Elements
Periodic Table of Phyical Eleent Periodic Table of Phyical Eleent Author:Zhiqiang Zhang fro Dalian, China Eail: dlxinzhigao@6.co ABSTRACT Thi i one of y original work in phyic to preent periodic table
More informationS E V E N. Steady-State Errors SOLUTIONS TO CASE STUDIES CHALLENGES
S E V E N Steady-State Error SOLUTIONS TO CASE STUDIES CHALLENGES Antenna Control: Steady-State Error Deign via Gain 76.39 a. G( (50)(.3). Syte i Type. Step input: e( ) 0; Rap input: e( ) v 76.39.59 ;
More informationLecture 2 Phys 798S Spring 2016 Steven Anlage. The heart and soul of superconductivity is the Meissner Effect. This feature uniquely distinguishes
ecture Phy 798S Spring 6 Steven Anlage The heart and oul of uperconductivity i the Meiner Effect. Thi feature uniquely ditinguihe uperconductivity fro any other tate of atter. Here we dicu oe iple phenoenological
More informationPerformance Analysis of a Three-Channel Control Architecture for Bilateral Teleoperation with Time Delay
Extended Suary pp.1224 1230 Perforance Analyi of a Three-Channel Control Architecture for Bilateral Teleoperation with Tie Delay Ryogo Kubo Meber (Keio Univerity, kubo@u.d.keio.ac.jp) Noriko Iiyaa Student
More informationLecture 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 informationTopic 7 Fuzzy expert systems: Fuzzy inference
Topic 7 Fuzzy expert yte: Fuzzy inference adani fuzzy inference ugeno fuzzy inference Cae tudy uary Fuzzy inference The ot coonly ued fuzzy inference technique i the o-called adani ethod. In 975, Profeor
More informationConservation of Energy
Add Iportant Conervation of Energy Page: 340 Note/Cue Here NGSS Standard: HS-PS3- Conervation of Energy MA Curriculu Fraework (006):.,.,.3 AP Phyic Learning Objective: 3.E.., 3.E.., 3.E..3, 3.E..4, 4.C..,
More informationMoisture transport in concrete during wetting/drying cycles
Cheitry and Material Reearch Vol.5 03 Special Iue for International Congre on Material & Structural Stability Rabat Morocco 7-30 Noveber 03 Moiture tranport in concrete during wetting/drying cycle A. Taher
More informationMATHEMATICAL MODELING OF INDUCTION MOTORS
37 CHAPTER 3 MATHEMATICAL MODELING OF INDUCTION MOTORS To tart with, a well-known technique called the SVPWM technique i dicued a thi form the bai of the mathematical modeling of IM. Furthermore, the d
More information4 Conservation of Momentum
hapter 4 oneration of oentu 4 oneration of oentu A coon itake inoling coneration of oentu crop up in the cae of totally inelatic colliion of two object, the kind of colliion in which the two colliding
More informationRanking DEA Efficient Units with the Most Compromising Common Weights
The Sixth International Sypoiu on Operation Reearch and It Application ISORA 06 Xiniang, China, Augut 8 12, 2006 Copyright 2006 ORSC & APORC pp. 219 234 Ranking DEA Efficient Unit with the Mot Coproiing
More informationSection J8b: FET Low Frequency Response
ection J8b: FET ow Frequency epone In thi ection of our tudie, we re o to reiit the baic FET aplifier confiuration but with an additional twit The baic confiuration are the ae a we etiated ection J6 of
More informationPerformance Guaranteed Inertia Emulation for Diesel-Wind System Feed Microgrid via Model Reference Control
2017 IEEE PES Innovative Sart Grid Technologie Conference, Wahington D.C., USA Perforance Guaranteed Inertia Eulation for Dieel-Wind Syte Feed Microgrid via Model Reference Control arxiv:1710.05700v2 [c.sy]
More informationThree Phase Induction Motors
Chapter (8) hree Phae Induction Motor Introduction he three-phae induction otor are the ot widely ued electric otor in indutry. hey run at eentially contant peed fro no-load to full-load. However, the
More informationPerformance 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 informationNanotechnology and high-precision optical displacement sensor design for optomechatronical systems
Nanotechnology and high-preciion optical diplaceent enor deign for optoechatronical yte A. Rotai* a, b, c, R. Yadipour a and K. Abbaian a, Z. D. Koozehkanani a, A. Ghanbari b, c, d and F. J. Sharifi e
More informationExponentially Convergent Controllers for n-dimensional. Nonholonomic Systems in Power Form. Jihao Luo and Panagiotis Tsiotras
997 Aerican Control Conference Albuquerque, NM, June 4-6, 997 Exponentially Convergent Controller for n-dienional Nonholonoic Syte in Power For Jihao Luo and Panagioti Tiotra Departent of Mechanical, Aeropace
More informationConvergence of a Fixed-Point Minimum Error Entropy Algorithm
Entropy 05, 7, 5549-5560; doi:0.3390/e7085549 Article OPE ACCESS entropy ISS 099-4300 www.dpi.co/journal/entropy Convergence of a Fixed-Point Miniu Error Entropy Algorith Yu Zhang, Badong Chen, *, Xi Liu,
More informationANALOG REALIZATIONS OF FRACTIONAL-ORDER INTEGRATORS/DIFFERENTIATORS A Comparison
AALOG REALIZATIOS OF FRACTIOAL-ORDER ITEGRATORS/DIFFERETIATORS A Coparion Guido DEESD, Technical Univerity of Bari, Via de Gaperi, nc, I-7, Taranto, Italy gaione@poliba.it Keyword: Abtract: on-integer-order
More informationDifferential Evolution based Optimal Control of Induction Motor Serving to Textile Industry
IAENG International Journal of Coputer Science, 35:, IJCS_35 03 Differential Evolution baed Optial Control of Induction Motor Serving to Textile Indutry C. Thanga Raj, Meber, IAENG, S. P. Srivatava, and
More informationSimulation and Analysis of Linear Permanent Magnet Vernier Motors for Direct Drive Systems
Available online at www.ijpe-online.com vol. 3, no. 8, December 07, pp. 304-3 DOI: 0.3940/ijpe.7.08.p.3043 Simulation and Analyi of Linear Permanent Magnet Vernier Motor for Direct Drive Sytem Mingjie
More informationInvestigation of application of extractive distillation method in chloroform manufacture
Invetigation of application of etractive ditillation ethod in chlorofor anufacture Proceeding of uropean Congre of Cheical ngineering (CC-6) Copenhagen, 16-20 Septeber 2007 Invetigation of application
More informationAll Division 01 students, START HERE. All Division 02 students skip the first 10 questions, begin on # (D)
ATTENTION: All Diviion 01 tudent, START HERE. All Diviion 0 tudent kip the firt 10 quetion, begin on # 11. 1. Approxiately how any econd i it until the PhyicBowl take place in the year 109? 10 (B) 7 10
More informationCHAPTER 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 informationEE 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 informationInvestment decision for supply chain resilience based on Evolutionary Game theory
Invetent deciion for upply chain reilience baed on Evolutionary Gae theory Xiaowei Ji(jixw@hut.edu.cn), Haijun Wang Manageent School Huazhong Univerity of Science and Technology Wuhan, Hubei, 4374, China
More informationObtaining the Current-Flux Relations of the Saturated PMSM by Signal Injection
Obtaining the Current-Flux Relation of the Saturated PMSM by Signal Injection Pacal Cobe, Françoi Malrait, Philippe Martin and Pierre Rouchon Schneider Tohiba Inverter Europe, 7 Pacy-ur-Eure, France Eail:
More informationDIFFERENTIAL EQUATIONS
Matheatic Reviion Guide Introduction to Differential Equation Page of Author: Mark Kudlowki MK HOME TUITION Matheatic Reviion Guide Level: A-Level Year DIFFERENTIAL EQUATIONS Verion : Date: 3-4-3 Matheatic
More informationFrequency Response Analysis of Linear Active Disturbance Rejection Control
Senor & Tranducer, Vol. 57, Iue, October 3, pp. 346-354 Senor & Tranducer 3 by IFSA http://www.enorportal.co Freuency Repone Analyi of Linear Active Diturbance Reection Control Congzhi HUANG, Qing ZHENG
More informationEvolutionary 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 informationPhysics 20 Lesson 28 Simple Harmonic Motion Dynamics & Energy
Phyic 0 Leon 8 Siple Haronic Motion Dynaic & Energy Now that we hae learned about work and the Law of Coneration of Energy, we are able to look at how thee can be applied to the ae phenoena. In general,
More informationSIMPLIFIED MODEL FOR EPICYCLIC GEAR INERTIAL CHARACTERISTICS
UNIVERSITY OF PITESTI SCIENTIFIC BULLETIN FACULTY OF ECHANICS AND TECHNOLOGY AUTOOTIVE erie, year XVII, no. ( 3 ) SIPLIFIED ODEL FOR EPICYCLIC GEAR INERTIAL CHARACTERISTICS Ciobotaru, Ticuşor *, Feraru,
More informationLOAD AND RESISTANCE FACTOR DESIGN APPROACH FOR FATIGUE OF MARINE STRUCTURES
8 th ACE pecialty Conference on Probabilitic Mechanic and tructural Reliability PMC2000-169 LOAD AND REITANCE FACTOR DEIGN APPROACH FOR FATIGUE OF MARINE TRUCTURE Abtract I.A. Aakkaf, G. ACE, and B.M.
More informationSensorless 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 information24P 2, where W (measuring tape weight per meter) = 0.32 N m
Ue of a 1W Laer to Verify the Speed of Light David M Verillion PHYS 375 North Carolina Agricultural and Technical State Univerity February 3, 2018 Abtract The lab wa et up to verify the accepted value
More informationThe 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 informationBASIC 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 informationChapter 7. Principles of Unsteady - State and Convective Mass Transfer
Suppleental Material for Tranport Proce and Separation Proce Principle hapter 7 Principle of Unteady - State and onvective Ma Tranfer Thi chapter cover different ituation where a tranfer i taking place,
More informationµ-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 informationConditions for equilibrium (both translational and rotational): 0 and 0
Leon : Equilibriu, Newton econd law, Rolling, Angular Moentu (Section 8.3- Lat tie we began dicuing rotational dynaic. We howed that the rotational inertia depend on the hape o the object and the location
More informationName: Answer Key Date: Regents Physics. Energy
Nae: Anwer Key Date: Regent Phyic Tet # 9 Review Energy 1. Ue GUESS ethod and indicate all vector direction.. Ter to know: work, power, energy, conervation of energy, work-energy theore, elatic potential
More informationMassachusetts 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 informationAdvanced D-Partitioning Analysis and its Comparison with the Kharitonov s Theorem Assessment
Journal of Multidiciplinary Engineering Science and Technology (JMEST) ISSN: 59- Vol. Iue, January - 5 Advanced D-Partitioning Analyi and it Comparion with the haritonov Theorem Aement amen M. Yanev Profeor,
More information_10_EE394J_2_Spring12_Inertia_Calculation.doc. Procedure for Estimating Grid Inertia H from Frequency Droop Measurements
Procedure or Etiating Grid Inertia ro Frequency Droop Meaureent While the exion or inertia and requency droop are well known, it i prudent to rederive the here. Treating all the grid generator a one large
More informationSERIES 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 informationResearch Article An Adaptive Regulator for Space Teleoperation System in Task Space
Abtract and Applied Analyi, Article ID 586, 7 page http://dx.doi.org/.55/24/586 Reearch Article An Adaptive Regulator for Space Teleoperation Syte in Tak Space Chao Ge, Weiwei Zhang, Hong Wang, and Xiaoyi
More informationA 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 informationSIMM Method Based on Acceleration Extraction for Nonlinear Maneuvering Target Tracking
Journal of Electrical Engineering & Technology Vol. 7, o. 2, pp. 255~263, 202 255 http://dx.doi.org/0.5370/jeet.202.7.2.255 SIMM Method Baed on Acceleration Extraction for onlinear Maneuvering Target Tracking
More informationISSN: [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 informationLecture 2 DATA ENVELOPMENT ANALYSIS - II
Lecture DATA ENVELOPMENT ANALYSIS - II Learning objective To eplain Data Envelopent Anali for ultiple input and ultiple output cae in the for of linear prograing .5 DEA: Multiple input, ultiple output
More informationIndependent Joint Control
ME135 ADANCED OBOICS Independent oint Contro ee-hwan yu Schoo of Mechanica Engineering Introduction to Contro Contro: deterining the tie hitory of joint input to do a coanded otion Contro ethod are depend
More informationLEARNING DISCRIMINATIVE BASIS COEFFICIENTS FOR EIGENSPACE MLLR UNSUPERVISED ADAPTATION. Yajie Miao, Florian Metze, Alex Waibel
LEARNING DISCRIMINATIVE BASIS COEFFICIENTS FOR EIGENSPACE MLLR UNSUPERVISED ADAPTATION Yajie Miao, Florian Metze, Alex Waibel Language Technologie Intitute, Carnegie Mellon Univerity, Pittburgh, PA, USA
More informationA Robust RF-MRAS based Speed Estimator using Neural Network as a Reference Model for Sensor-less Vector Controlled IM Drives
Control Theory and Inforatic Vol, No.3, 0.iite.org A Robut RF-MRAS baed Speed Etiator uing Neural Netork a a Reference Model for Senor-le Vector Controlled IM Drive A. Venkadean, Reearch Scholar Departent
More information3.185 Problem Set 6. Radiation, Intro to Fluid Flow. Solutions
3.85 Proble Set 6 Radiation, Intro to Fluid Flow Solution. Radiation in Zirconia Phyical Vapor Depoition (5 (a To calculate thi viewfactor, we ll let S be the liquid zicronia dic and S the inner urface
More informationRepresentation 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 informationPHYSICS 151 Notes for Online Lecture 2.3
PHYSICS 151 Note for Online Lecture.3 riction: The baic fact of acrocopic (everda) friction are: 1) rictional force depend on the two aterial that are liding pat each other. bo liding over a waed floor
More informationHybrid technique based on chirp effect and phase shifts for spectral Talbot effect in sampled fiber Bragg gratings (FBGs)
Optica Applicata, Vol. XLI, No. 1, 011 Hybrid technique baed on chirp effect and phae hift for pectral Talbot effect in apled fiber Bragg grating (FBG) GUO DENG *, WEI PAN Center for Inforation Photonic
More information1-D SEDIMENT NUMERICAL MODEL AND ITS APPLICATION. Weimin Wu 1 and Guolu Yang 2
U-CHINA WORKHOP ON ADVANCED COMPUTATIONAL MODELLING IN HYDROCIENCE & ENGINEERING epteber 9-, Oxford, Miiippi, UA -D EDIMENT NUMERICAL MODEL AND IT APPLICATION Weiin Wu and Guolu Yang ABTRACT A one dienional
More informationAn Exact Solution for the Deflection of a Clamped Rectangular Plate under Uniform Load
Applied Matheatical Science, Vol. 1, 007, no. 3, 19-137 An Exact Solution for the Deflection of a Claped Rectangular Plate under Unifor Load C.E. İrak and İ. Gerdeeli Itanbul Technical Univerity Faculty
More informationRigorous analysis of diffraction gratings of arbitrary profiles using virtual photonic crystals
2192 J. Opt. Soc. A. A/ Vol. 23, No. 9/ Septeber 2006 W. Jiang and R. T. Chen Rigorou analyi of diffraction grating of arbitrary profile uing virtual photonic crytal Wei Jiang and Ray T. Chen Microelectronic
More informationCHAPTER 3. FUZZY LOGIC DIRECT TORQUE CONTROL.
CHAPTER 3. FUZZY LOGIC DIRECT TORQUE CONTROL. 3. - Introduction. In DTC induction otor drive there are torque and fux rippe becaue none of the VSI tate i abe to generate the exact votage vaue required
More informationResearch Article An Extension of Cross Redundancy of Interval Scale Outputs and Inputs in DEA
Hindawi Publihing Corporation pplied Matheatic Volue 2013, rticle ID 658635, 7 page http://dx.doi.org/10.1155/2013/658635 Reearch rticle n Extenion of Cro Redundancy of Interval Scale Output and Input
More informationSIMON FRASER UNIVERSITY School of Engineering Science ENSC 320 Electric Circuits II. R 4 := 100 kohm
SIMON FRASER UNIVERSITY School of Engineering Science ENSC 320 Electric Circuit II Solution to Aignment 3 February 2003. Cacaded Op Amp [DC&L, problem 4.29] An ideal op amp ha an output impedance of zero,
More informationNo-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 informationA Simple Model of the Linear Speed of a Ground Vehicle under Accelerating and Decelerating Forces
A Siple Model of the Linear Speed of a Ground Vehicle under Accelerating and Decelerating orce Guillero Calderón Meza Kaierlautern Univerity of Technology aculty of Inforatic calderon@inforatik.uni-kl.de
More informationThrottle Actuator Swapping Modularity Design for Idle Speed Control
9 merican ontrol onference Hyatt Regency Riverfront, St. Loui, MO, US June -, 9 ThB.4 Throttle ctuator Swapping Modularity Deign for Idle Speed ontrol Shifang Li, Melih akmakci, Ilya V. Kolmanovky and.
More informationWhat 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 informationTHE PARAMETERIZATION OF ALL TWO-DEGREES-OF-FREEDOM SEMISTRONGLY STABILIZING CONTROLLERS. Tatsuya Hoshikawa, Kou Yamada and Yuko Tatsumi
International Journal of Innovative Computing, Information Control ICIC International c 206 ISSN 349-498 Volume 2, Number 2, April 206 pp. 357 370 THE PARAMETERIZATION OF ALL TWO-DEGREES-OF-FREEDOM SEMISTRONGLY
More informationStability 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 informationPHYSICS 211 MIDTERM II 12 May 2004
PHYSIS IDTER II ay 004 Exa i cloed boo, cloed note. Ue only your forula heet. Write all wor and anwer in exa boolet. The bac of page will not be graded unle you o requet on the front of the page. Show
More informationBasic 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(2011) 34 (3) ISSN
Ceriotti, Matteo and McInne, Colin () Generation of optial trajectorie for Earth hybrid pole itter. Journal of Guidance, Control and Dynaic, 34 (3). pp. 847-859. ISSN 533-3884, http://dx.doi.org/.54/.5935
More informationCONTROL SYSTEMS, ROBOTICS AND AUTOMATION Vol. VIII Decoupling Control - M. Fikar
DECOUPLING CONTROL M. Fikar Department of Proce Control, Faculty of Chemical and Food Technology, Slovak Univerity of Technology in Bratilava, Radlinkého 9, SK-812 37 Bratilava, Slovakia Keyword: Decoupling:
More informationME 375 FINAL EXAM SOLUTIONS Friday December 17, 2004
ME 375 FINAL EXAM SOLUTIONS Friday December 7, 004 Diviion Adam 0:30 / Yao :30 (circle one) Name Intruction () Thi i a cloed book eamination, but you are allowed three 8.5 crib heet. () You have two hour
More informationSimulink Implementation of Induction Machine Model A Modular Approach
Simulink Implementation of Induction Machine Model A Modular Approach Burak Ozpineci burak@ieee.org Oak Ridge National Laboratory P.O. Box 9 Oak Ridge, TN 78-67 Abtract - In thi paper, a modular Simulink
More information15 N 5 N. Chapter 4 Forces and Newton s Laws of Motion. The net force on an object is the vector sum of all forces acting on that object.
Chapter 4 orce and ewton Law of Motion Goal for Chapter 4 to undertand what i force to tudy and apply ewton irt Law to tudy and apply the concept of a and acceleration a coponent of ewton Second Law to
More informationPractice Problem Solutions. Identify the Goal The acceleration of the object Variables and Constants Known Implied Unknown m = 4.
Chapter 5 Newton Law Practice Proble Solution Student Textbook page 163 1. Frae the Proble - Draw a free body diagra of the proble. - The downward force of gravity i balanced by the upward noral force.
More informationTHE BICYCLE RACE ALBERT SCHUELLER
THE BICYCLE RACE ALBERT SCHUELLER. INTRODUCTION We will conider the ituation of a cyclit paing a refrehent tation in a bicycle race and the relative poition of the cyclit and her chaing upport car. The
More informationPHY 171 Practice Test 3 Solutions Fall 2013
PHY 171 Practice et 3 Solution Fall 013 Q1: [4] In a rare eparatene, And a peculiar quietne, hing One and hing wo Lie at ret, relative to the ground And their wacky hairdo. If hing One freeze in Oxford,
More informationChapter 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 informationV2V-Based Vehicle Risk Assessment and Control for Lane-Keeping and Collision Avoidance
VV-Baed Vehicle Rik Aeent and Control for Lane-Keeping and Colliion Avoidance Haze M. Fahy Electronic Departent Geran Univerity in Cairo haze.fahyy9@gail.co Haan Motafa Electronic and Electrical Counication
More informationPOSTER PRESENTATION OF A PAPER BY: Alex Shved, Mark Logillo, Spencer Studley AAPT MEETING, JANUARY, 2002, PHILADELPHIA
POSTER PRESETATIO OF A PAPER BY: Ale Shved, Mar Logillo, Spencer Studley AAPT MEETIG, JAUARY, 00, PHILADELPHIA Daped Haronic Ocillation Uing Air a Drag Force Spencer Studley Ale Shveyd Mar Loguillo Santa
More informationSliding-Mode Bilateral Teleoperation Control Design for Master-Slave Pneumatic Servo Systems
Thi paper appear in Control Engineering Practice, 212. http://dx.doi.org/1.116/j.conengprac.212.2.3 Sliding-Mode Bilateral Teleoperation Control Deign for Mater-Slave Pneuatic Servo Syte R. Moreau 1, M.T.
More informations s 1 s = m s 2 = 0; Δt = 1.75s; a =? mi hr
Flipping Phyic Lecture Note: Introduction to Acceleration with Priu Brake Slaing Exaple Proble a Δv a Δv v f v i & a t f t i Acceleration: & flip the guy and ultiply! Acceleration, jut like Diplaceent
More informationIN SUPERVISING the correct operation of dynamic plants,
1158 IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, VOL. 14, NO. 6, NOVEMBER 2006 Nonlinear Fault Detection and Iolation in a Three-Tank Heating Syte Raffaella Mattone and Aleandro De Luca, Senior Meber,
More informationSMALL-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 informationOpen Access Study of Direct Torque Control Scheme for Induction Motor Based on Torque Angle Closed-Loop Control. Xuande Ji *, Daqing He and Yunwang Ge
Send Order for Reprint to reprint@benthamcience.ae 6 The Open Electrical & Electronic Engineering Journal, 25, 9, 669 Open Acce Study of Direct Torque Control Scheme for Induction Motor Baed on Torque
More informationS_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