2 Simulation exercise 2

Size: px
Start display at page:

Download "2 Simulation exercise 2"

Transcription

1 Smulaton exercse. Descrton of a dynamc system One of the man tasks n the course on CAD of automatc control system s to model, to smulate and to carry out control acton for some knd of dynamc system(s). One way or another, the dynamc system s descrbed as a mathematcal model that reresents a hyscal realty, wth a set of varables and a set of logcal and quanttatve relatonshs between them. Even though the model may make exlct assumtons that are known to be false (or ncomlete) n some detal, t has to carry out the essence of the hyscal rocess(es). Modern techncal systems are consdered to be comlex (comosed of many comonents) and cover mult-doman (electrcal, mechancal, thermal ). Over and over agan t s not trval to go from hyscal rocess to mathematcal model and comromse beng fast and accurate (what to model and what to exclude, nclude relevant hyscs, use arorate concets ). A model s always aroxmate and a good model s smle, yet catures the essentals! There can be dfferent methodologes how to gras the essentals or an effcent aroach to (buld a) model of a dynamc system of nterest. There mght be a few stes between establshng a hyscal understandng and defnng a mathematcal model: How does the system work? Understandng, defnton of urose, structurng nto subsystems and nteractons between them, once more understandng of hyscal realty Whch asects of the system are we nterested n and whch quanttes are mortant for descrbng the rocesses? Understandng, try to reflect logcal relatons, hyscal rncles, cause-and-effect, force-and-reacton relatonshs, controllablty, measurablty How do reflect the essence of the hyscal rocesses and how the quanttes of mortance nfluence each other? Organze varables and equatons, valdate and smlfy model o Mathematcal models are often based on balance equatons (nflow outflow = volume, energy etc change er tme unt, ower n ower out = accumulated energy er tme unt, sum of all currents enterng a node = 0) and consttutve relatons (statc relatons between quanttes Ohm s Law) o Focus modellng effort on dynamcs whose tme constants are relevant for the ntended urose of the model subsystems wth fast dynamcs aroxmated as statc relatons and varables that vary slowly are aroxmated by constants In the frst home assgnment a geometrc shae of a system.e. nductor was gven and the assgnment was to descrbe the system by a set of equatons that s also reflected from the block dagram. Fgure. A smle smulnk block dagram descrbng the nductor

2 ψ ψ = ( u R) dt = f = em (.) L The system s consdered to be nonlnear not only because of L = f ( B) f n B but also because of, whch s not ncluded n the revous exressons. There s assumed that L=const. Furthermore, when consderng knetcs of the nductor yoke (electromagnet yoke) then L=f(B,x) where x corresond to a dslacement of the yoke. As a matter of fact, the oosng nduced voltage can be ether a transformer voltage or/and a motonal voltage, whch s resectvely generated ether by the change of current or by the change of nductance generated by moton. d d d dl d dx dl e = ψ = L = L + = L + (.) dt dt dt dt dt dt dx At the moment, there s no further nvestgaton on the nonlnear system of the nductor or the electromagnet rather than to study a lnear tme nvarant (LTI) system. u S y=s(u) The system S s lnear f ( ku) ks( u) S ( u u ) = S( u ) + S( ) S = scalng + sueroston u A system s tme-nvarant f delayng the nut results n a delayed outut: y ( t τ ) = S( u( t τ )) Lnear tme-nvarant systems are easy to analyze Local stablty = global stablty: Egenvalues of the system matrx A (= oles of G(s)) n left half lane regardless of ntal ostons The transent resonse of a lnear system s comosed of the natural modes of the system: Sueroston, enough to know ste (or mulse) resonse Frequency analyss ossble: Snusodal nuts gve snusodal oututs The man tasks of ths home assgnments s to recall knowledge or become famlar wth Dfferent ways of descrbng a dynamc system Tme and frequency resonse characterzaton of a dynamc system Analyss of the automatc control system References to course lterature Automatc Control by Raul Naadel are gven n the arentheses {Eest keeles}. Each ste of solvng an assgnment corresonds to certan amount of credts gven n brackets (0). Use the and mrove the m-fle (Ch.7) to carry out your work

3 . Electrcal machne wth ermanent magnet exctaton The second smulaton exercse focus on a seed controlled electrcal machne n an electrc drve system. The frst task s to establsh a hyscal understandng of the electromechancal energy converson. An electrc motor s a machne whch converts electrcal energy nto mechancal energy. The oeraton of a most of electrcal motors s based on the rncle that when a current-carryng conductor s laced n a magnetc feld, t exerences a mechancal force whose drecton s gven by Flemng's Left-hand rule. I I E M M B ψ ω F jωψ I rotaton axs Fgure. a smlfed constructon of a ermanent magnet excted electrcal machne. We can assume that ermanent magnet exctaton gves a constant feld and the rotaton occurs n the drecton and seed ω. The moton of col s a subject of lnkng wth feld lnes and nducng feld E nsde the col. There are 4 waveforms n Fgure.3 that mght be ether flux or nduced voltage and your task s to select and motvate s flux and emf that corresond to the machne n Fgure.. The dmensons can be recalculated from the student dentfcaton number: n=[n n n 3 n 4 n 5 n 6 ] accordng to the formulaton n.7 (m-scrt). waveform, A (t) [-] A (t) relatve erod, T [-] waveform, A (t) [-] A (t) relatve erod, T [-] waveform, A 3 (t) [-] A 3 (t) relatve erod, T [-] waveform, A 4 (t) [-] A 4 (t) relatve erod, T [-] Fgure.3 Normalsed waveforms of a hyscal quantty A over a erod T.. Pck correct flux waveform () and motvate your choce (3).. Pck correct emf waveform () and motvate your choce (3).

4 .3 Frst order system Study the electromechancal resonse of a dc machne wthout consderng the knetcs of the system.e. the rotatonal seed Ω=0 rad/s. The SISO has voltage as an nut and electromagnetc torque as an outut. 3. Descrton of the system. Gve arametrc exressons and check t numercally by hel of Matlab. a. Block dagram {Struktuurskeem..4} reresentaton (and reducton). Draw structure block dagram accordng to Fgure. n smulnk and use In and Out blocks to secfy nut and outut and gve a name to the model e.g. AutRP mdl () b. Wrte (a sngle) dfferental equaton {Dfferentsaalvõrrand.}of the system () c. State varable model. Descrbe the system by state equaton {Olekuvõrrand.3}. (). Choose state varables. Exress tme dervatves of states n terms of states and nuts. Exress oututs n terms of states and nuts v. Use MATLAB command n work sace [A,B,C,D] = lnmod('autrp mdl') and comare the results d. Transfer functon {ülekandefunktsoon..} () 4. resonse of the system. Use MATLAB command n work sace [num,den] = lnmod('autrp mdl'); tf(num,den) and comare the results e. tme resonse durng t=0:e-4:0.05. ste resonse {ühkhüe.4.}. Use MATLAB command n work sace y=ste(num,den,t); lot the results and characterse the resonse (show the tme constant of the frst order ste resonse) (). ste resonse {ühkmulss.4.}. Use MATLAB command n work sace y=mulse(num,den,t); lot the results and characterse the resonse () f. frequency resonse. Bode dagram {Bode dagramm..3}. Use MATLAB command n work sace y=bode(num,den); lot the results and characterse the resonse (show the bandwdth of the frst order frequency resonse) (). Nyqust dagram {Nyqust dagramm 3...4}. Use MATLAB command n work sace y=nyqust(num,den); lot the results and characterse the resonse (show the tme constant of the frst order ste resonse) () 5. Estmate the stablty of the system g. Accordng to egenvalues of the system matrx A {tunnusvõrrand lahendd 3...}. Use MATLAB command n work sace eg(a) and characterse the results. () h. Stablty accordng to Nyqust and Bode dagrams {3...4 ja 3...5} ()

5 .4 Second order system Include knematcs to the revously derved system. 6. Reeat revous exercses (3, 4, 5) wth the renewed system (0). 7. How behaves the system f the back emf feedback E=m*Ω s not ncluded, how ths can be exlaned n the sense of hyscal energy converson rocesses (5). 8. Include load momentum of nerta Jload=0.0 kgm and characterse system behavour (5). Note that you can nclude more than sngle outut when studyng the dynamcs of the system e.g. one outut for the mechancal seed, the other for the machne current..5 Seed control Prevously an electrc drve system has been derved that nut voltage u(t) nfluences the outut Ω(t). The am of the control system s to acheve a desred resonse of a system and not just to affect the outut smlar to dsturbances or load varatons. The am here s to carry out the seed control for the electrcal drve The control loos n electrcal drve are usually always connected n cascade Cascaded control concet does only work f the bandwdth ncreases from the outer to the nner loos. It s assumed that torque control acton s erformed erfectly wthout affectng the desgn of the seed control loo. The system resonse wth PI controller has a good steady state erformance e.g. t can acheve the zero steady-state error. The control acton of a PI-controller bases on the control error e(t), whch s the dfference between the reference y*(t) and the measured value y(t). e () t = y * () t y() t The control outut s roortonal to the error and to the ntegral of the error. In the leftmost exresson of u(t) the controller gan can be changed wthout changng the tme constant. u = + dt T () t e() t + e() t dt = e() t e() t The breakont n Bode dagram /T wll be unchanged (shown from the exressons of transfer functons). From the rghtmost exressons can be seen that the gan and the breakont wll be affected by both and. u + st st () s = e() s = + e() s st By assumng that the torque source s nfntely fast the transfer functon of the closed seed controlled system can be wrtten Ω * Ω () s () s ( + st ) = s JT + s T + the oles for the system are (.3) (.4) (.5) (.6)

6 oles = ± J 4J JT (.7) Ths exresson shows that the oles of the system can be laced arbtrarly wth and T. Practcally, f s too large then the assumton that the torque loo s nfntely fast s not vald. The realstc assumton for the torque resonse corresonds to a low ass flter wth a tme constant equal to the samlng erod n the torque control loo. () s = () s + stc T (.8) * T By consderng the realstc aroxmate resonse of the torque controlled electrcal machne, the oen loo transfer functon for the system can be wrtten W + st ω = (.9) st + st sj ( j ) c Your assgnment s to draw an oen loo block dagram and to study frequency resonse. Fgure.4 oen loo of a seed controlled electrcal drve 9. Draw the block dagram shown Fgure.4, select Tc=0.00 seconds, T>Tc, = and study the frequency resonse from Bode dagram (4). 0. Wrte on Bode dagram the breakng frequences /T, /Tc and the frequency ω0 = where the maxmum hase aears (4). T T c.6 Symmetrc otmum The PI controller arameters are selected accordng to symmetrc otmum crteron. An dea behnd that s to select the cross-over frequency n the ont where the hase margnal s the largest. Ths wll gve the best damng for the closed system. The condton W(jω) = at ω 0 gves the frst equaton: T = a T where a > as T > T c c (.0) By relacng Tc n eq.0 wth T accordng to eq. gves the next relaton a J = (.) T In accordance wth the closed seed loo Ω * Ω () s () s c ( + st ) = 3 s JT T + s JT + s T + the characterstc equaton can be wrtten (.)

7 3 T a s + s T + + = 0 sa (.3) a T where one root s T a s = ω 0 = (.4) Polynomal dvson of the characterstc olynomal (eg.4) gves T a s + s T + = 0 (.5) a a where the other roots can be calculated analytcally. We assume that they are comlex conjugates, where ( ξ ± ) s (.6),3 = ω0 ξ ξ = a (.7) s seen as the relatve damng for the oles to the system. The arameter T can now be selected to lace the oles n a sutable way. If the relatve damng s selected to ξ =, then a=.4. Ths gves drectly value on T as a functon of Tc. If we on the other hand assume that no comlex oles are to exst n the seed control system then ξ = and a=3. All three oles wll thus be equal to - ω 0. Your task s to choose PI seed controller arameters accordng to symmetrc otmum crteron.. Select PI controller arameters accordng to Tc=0.00 sec and a=3. Analyse the system wthout and wth load momentum of nerta Jload=0.0 kgm and characterse system behavour accordng to tme resonse and frequency resonse (8).. Use dfferent and T n the PI regulator and characterse system behavour and stablty accordng to tme resonse and frequency resonse (0). 3. Study the torque resonse wth the new nerta and estmate the motor current accordng to your motor (4). 4. Add a low ass flter nto the seed feedback as n ractcal cases t s consdered that the seed sensor s subjected to nose that needs to be fltered out to some extent. As you see the system becomes 4-th order system. In order to solve the roblem the flter tme constant s selected at least one order of magntude longer comared to torque loo. Thereafter the flter tme constant wll be bass to desgn PI seed controller accordng to symmetrc otmum. Snce the torque dynamcs s one order of magntude faster than the flter dynamcs t can be omtted. Reeat analyss accordng to onts and (0).

8 .7 M-fle Ths s the m-fle that you should use n your home assgnment n order to get the ntal data for an electrcal machne. Take an advantage of the scrt to carry out effcently all the assgnments! % Home assgnment on CAD of Automatc Control Systems % machne descrton % the ermanent magnet machne s assumed to have rotor dameter of D, % stator dameter of D and machne length l. Magnetc ga s D/4, wndng % heght D/4 and fll factor over the crcular cross-secton s 0.5. % suly voltage V, ga flux densty s assumed 0.8T and allowed current % densty 3A/mm wthn the thermal lmt. Mass densty of the machne s % 7000 kg/m3 rjuta sa oma martkl number jättes numbrte vahele tühkud % arametersaton n = [ ]; % student dentfcaton number mu0 = 4**e-7; D = (n(6) + 0)*e-3; l = (n(5) + 40)*e-3; Un = ; n = 4000; Ph = 0.5**D*l * 0.8; [Vs] % magnetc ermeablty n vacuum % rotor dameter [m] % length of machne [m] % suly voltage [V] % nomnal seed [rm] % maxmum magnetc Bga=0.8T N = 0.5*((D-D/4)^-(D/)^)* * 0.5*3e+6; % magnetomotve Jm=3e+6A/m [Aturns] dph= Ph/(/); Tn = N*dPh; Pn = Tn*n/60**; N = cel(un/(dph*n/60**)); In = N/N; m = dph*n; M = *D^*l * 7000; % dph/dtheta [V/(rad/s)] % electromagnetc torque [Nm] % electromagnetc ower [W] % number of turns [turns] % rated current [A] % machne constant [Nm/A=Vs/rad] % mass of the machne [kg] R =.4e-8**(l+.6*D)/(0.5*((D-D/4)^-(D/)^)*)*N^; % resstance [Ohm] L = /(/mu0*d/4/(0.5**d*l))*n^; % armature nductance [H]

9 J = /4*7000*l**(D/)^*((D/)^); % rotor momentum of nerta [kg*m^] Dm = J/0.*0; % mechancal damng %J=J+0.0; Tc=0.00; % torque resonse tme, sec Tflt=0.05; % seed flter tme constant, sec %Tflt=Tc; % PI seed controller arameters a=3; % otmum control Tw=a^*Tflt; % ntegral tme constant w=j*a/tw; % roortonal gan w=/tw; % ntegral gan % Smulatons %oen('autrp_a_mdl.mdl') [A,B,C,D] = lnmod('autrp mdl'); [num,den]=lnmod('autrp mdl'); t=0:e-4:0.05; fgure(); clf; scrsz = get(0,'screensze'); set(gcf,'poston',[5 scrsz(4)/0 scrsz(3)-0 scrsz(4)/],'color',[ ],'Name','Tme Doman'); % ste resonse y=ste(num,den,t); %y=y./(ones(length(y),)*max(y)); sublot(,,); hold on; grd on; lot(t,y); ttle(['ste resonse']); xlabel('tme, t [sec]'); ylabel('outut'); % mulse resonse y=mulse(num,den,t); sublot(,,); hold on; grd on; lot(t,y) ttle(['mulse resonse']); xlabel('tme, t [sec]'); ylabel('outut'); fgure(66); nyqust(num,den) fgure(67); bode(num,den)

Lesson 16: Basic Control Modes

Lesson 16: Basic Control Modes 0/8/05 Lesson 6: Basc Control Modes ET 438a Automatc Control Systems Technology lesson6et438a.tx Learnng Objectves Ater ths resentaton you wll be able to: Descrbe the common control modes used n analog

More information

Digital PI Controller Equations

Digital PI Controller Equations Ver. 4, 9 th March 7 Dgtal PI Controller Equatons Probably the most common tye of controller n ndustral ower electroncs s the PI (Proortonal - Integral) controller. In feld orented motor control, PI controllers

More information

THE EFFECT OF TORSIONAL RIGIDITY BETWEEN ELEMENTS ON FREE VIBRATIONS OF A TELESCOPIC HYDRAULIC CYLINDER SUBJECTED TO EULER S LOAD

THE EFFECT OF TORSIONAL RIGIDITY BETWEEN ELEMENTS ON FREE VIBRATIONS OF A TELESCOPIC HYDRAULIC CYLINDER SUBJECTED TO EULER S LOAD Journal of Appled Mathematcs and Computatonal Mechancs 7, 6(3), 7- www.amcm.pcz.pl p-issn 99-9965 DOI:.75/jamcm.7.3. e-issn 353-588 THE EFFECT OF TORSIONAL RIGIDITY BETWEEN ELEMENTS ON FREE VIBRATIONS

More information

Mechanics Physics 151

Mechanics Physics 151 Mechancs hyscs 151 Lecture Canoncal Transformatons (Chater 9) What We Dd Last Tme Drect Condtons Q j Q j = = j, Q, j, Q, Necessary and suffcent j j for Canoncal Transf. = = j Q, Q, j Q, Q, Infntesmal CT

More information

The Decibel and its Usage

The Decibel and its Usage The Decbel and ts Usage Consder a two-stage amlfer system, as shown n Fg.. Each amlfer rodes an ncrease of the sgnal ower. Ths effect s referred to as the ower gan,, of the amlfer. Ths means that the sgnal

More information

A Quadratic Cumulative Production Model for the Material Balance of Abnormally-Pressured Gas Reservoirs F.E. Gonzalez M.S.

A Quadratic Cumulative Production Model for the Material Balance of Abnormally-Pressured Gas Reservoirs F.E. Gonzalez M.S. Natural as Engneerng A Quadratc Cumulatve Producton Model for the Materal Balance of Abnormally-Pressured as Reservors F.E. onale M.S. Thess (2003) T.A. Blasngame, Texas A&M U. Deartment of Petroleum Engneerng

More information

6. Hamilton s Equations

6. Hamilton s Equations 6. Hamlton s Equatons Mchael Fowler A Dynamcal System s Path n Confguraton Sace and n State Sace The story so far: For a mechancal system wth n degrees of freedom, the satal confguraton at some nstant

More information

A Quadratic Cumulative Production Model for the Material Balance of Abnormally-Pressured Gas Reservoirs F.E. Gonzalez M.S.

A Quadratic Cumulative Production Model for the Material Balance of Abnormally-Pressured Gas Reservoirs F.E. Gonzalez M.S. Formaton Evaluaton and the Analyss of Reservor Performance A Quadratc Cumulatve Producton Model for the Materal Balance of Abnormally-Pressured as Reservors F.E. onale M.S. Thess (2003) T.A. Blasngame,

More information

Transfer Functions. Convenient representation of a linear, dynamic model. A transfer function (TF) relates one input and one output: ( ) system

Transfer Functions. Convenient representation of a linear, dynamic model. A transfer function (TF) relates one input and one output: ( ) system Transfer Functons Convenent representaton of a lnear, dynamc model. A transfer functon (TF) relates one nput and one output: x t X s y t system Y s The followng termnology s used: x y nput output forcng

More information

PHYS 705: Classical Mechanics. Newtonian Mechanics

PHYS 705: Classical Mechanics. Newtonian Mechanics 1 PHYS 705: Classcal Mechancs Newtonan Mechancs Quck Revew of Newtonan Mechancs Basc Descrpton: -An dealzed pont partcle or a system of pont partcles n an nertal reference frame [Rgd bodes (ch. 5 later)]

More information

Translational Equations of Motion for A Body Translational equations of motion (centroidal) for a body are m r = f.

Translational Equations of Motion for A Body Translational equations of motion (centroidal) for a body are m r = f. Lesson 12: Equatons o Moton Newton s Laws Frst Law: A artcle remans at rest or contnues to move n a straght lne wth constant seed there s no orce actng on t Second Law: The acceleraton o a artcle s roortonal

More information

Confidence intervals for weighted polynomial calibrations

Confidence intervals for weighted polynomial calibrations Confdence ntervals for weghted olynomal calbratons Sergey Maltsev, Amersand Ltd., Moscow, Russa; ur Kalambet, Amersand Internatonal, Inc., Beachwood, OH e-mal: kalambet@amersand-ntl.com htt://www.chromandsec.com

More information

PHYSICS - CLUTCH CH 28: INDUCTION AND INDUCTANCE.

PHYSICS - CLUTCH CH 28: INDUCTION AND INDUCTANCE. !! www.clutchprep.com CONCEPT: ELECTROMAGNETIC INDUCTION A col of wre wth a VOLTAGE across each end wll have a current n t - Wre doesn t HAVE to have voltage source, voltage can be INDUCED V Common ways

More information

Mechanics Physics 151

Mechanics Physics 151 Mechancs Physcs 151 Lecture 22 Canoncal Transformatons (Chater 9) What We Dd Last Tme Drect Condtons Q j Q j = = j P, Q, P j, P Q, P Necessary and suffcent P j P j for Canoncal Transf. = = j Q, Q, P j

More information

Week3, Chapter 4. Position and Displacement. Motion in Two Dimensions. Instantaneous Velocity. Average Velocity

Week3, Chapter 4. Position and Displacement. Motion in Two Dimensions. Instantaneous Velocity. Average Velocity Week3, Chapter 4 Moton n Two Dmensons Lecture Quz A partcle confned to moton along the x axs moves wth constant acceleraton from x =.0 m to x = 8.0 m durng a 1-s tme nterval. The velocty of the partcle

More information

Week 9 Chapter 10 Section 1-5

Week 9 Chapter 10 Section 1-5 Week 9 Chapter 10 Secton 1-5 Rotaton Rgd Object A rgd object s one that s nondeformable The relatve locatons of all partcles makng up the object reman constant All real objects are deformable to some extent,

More information

PHYSICS - CLUTCH 1E CH 28: INDUCTION AND INDUCTANCE.

PHYSICS - CLUTCH 1E CH 28: INDUCTION AND INDUCTANCE. !! www.clutchprep.com CONCEPT: ELECTROMAGNETIC INDUCTION A col of wre wth a VOLTAGE across each end wll have a current n t - Wre doesn t HAVE to have voltage source, voltage can be INDUCED V Common ways

More information

THERMODYNAMICS. Temperature

THERMODYNAMICS. Temperature HERMODYNMICS hermodynamcs s the henomenologcal scence whch descrbes the behavor of macroscoc objects n terms of a small number of macroscoc arameters. s an examle, to descrbe a gas n terms of volume ressure

More information

Chapter 6 Electrical Systems and Electromechanical Systems

Chapter 6 Electrical Systems and Electromechanical Systems ME 43 Systems Dynamcs & Control Chapter 6: Electrcal Systems and Electromechancal Systems Chapter 6 Electrcal Systems and Electromechancal Systems 6. INTODUCTION A. Bazoune The majorty of engneerng systems

More information

CHAPTER 5 NUMERICAL EVALUATION OF DYNAMIC RESPONSE

CHAPTER 5 NUMERICAL EVALUATION OF DYNAMIC RESPONSE CHAPTER 5 NUMERICAL EVALUATION OF DYNAMIC RESPONSE Analytcal soluton s usually not possble when exctaton vares arbtrarly wth tme or f the system s nonlnear. Such problems can be solved by numercal tmesteppng

More information

A particle in a state of uniform motion remain in that state of motion unless acted upon by external force.

A particle in a state of uniform motion remain in that state of motion unless acted upon by external force. The fundamental prncples of classcal mechancs were lad down by Galleo and Newton n the 16th and 17th centures. In 1686, Newton wrote the Prncpa where he gave us three laws of moton, one law of gravty,

More information

Model Reference Adaptive Temperature Control of the Electromagnetic Oven Process in Manufacturing Process

Model Reference Adaptive Temperature Control of the Electromagnetic Oven Process in Manufacturing Process RECENT ADVANCES n SIGNAL PROCESSING, ROBOTICS and AUTOMATION Model Reference Adatve Temerature Control of the Electromagnetc Oven Process n Manufacturng Process JIRAPHON SRISERTPOL SUPOT PHUNGPHIMAI School

More information

Physics 1202: Lecture 11 Today s Agenda

Physics 1202: Lecture 11 Today s Agenda Physcs 122: Lecture 11 Today s Agenda Announcements: Team problems start ths Thursday Team 1: Hend Ouda, Mke Glnsk, Stephane Auger Team 2: Analese Bruder, Krsten Dean, Alson Smth Offce hours: Monday 2:3-3:3

More information

PHY2049 Exam 2 solutions Fall 2016 Solution:

PHY2049 Exam 2 solutions Fall 2016 Solution: PHY2049 Exam 2 solutons Fall 2016 General strategy: Fnd two resstors, one par at a tme, that are connected ether n SERIES or n PARALLEL; replace these two resstors wth one of an equvalent resstance. Now

More information

Advanced Circuits Topics - Part 1 by Dr. Colton (Fall 2017)

Advanced Circuits Topics - Part 1 by Dr. Colton (Fall 2017) Advanced rcuts Topcs - Part by Dr. olton (Fall 07) Part : Some thngs you should already know from Physcs 0 and 45 These are all thngs that you should have learned n Physcs 0 and/or 45. Ths secton s organzed

More information

PID Controller Design Based on Second Order Model Approximation by Using Stability Boundary Locus Fitting

PID Controller Design Based on Second Order Model Approximation by Using Stability Boundary Locus Fitting PID Controller Desgn Based on Second Order Model Aroxmaton by Usng Stablty Boundary Locus Fttng Furkan Nur Denz, Bars Baykant Alagoz and Nusret Tan Inonu Unversty, Deartment of Electrcal and Electroncs

More information

Inductance Calculation for Conductors of Arbitrary Shape

Inductance Calculation for Conductors of Arbitrary Shape CRYO/02/028 Aprl 5, 2002 Inductance Calculaton for Conductors of Arbtrary Shape L. Bottura Dstrbuton: Internal Summary In ths note we descrbe a method for the numercal calculaton of nductances among conductors

More information

Dr. Shalabh Department of Mathematics and Statistics Indian Institute of Technology Kanpur

Dr. Shalabh Department of Mathematics and Statistics Indian Institute of Technology Kanpur Analyss of Varance and Desgn of Exerments-I MODULE III LECTURE - 2 EXPERIMENTAL DESIGN MODELS Dr. Shalabh Deartment of Mathematcs and Statstcs Indan Insttute of Technology Kanur 2 We consder the models

More information

Moments of Inertia. and reminds us of the analogous equation for linear momentum p= mv, which is of the form. The kinetic energy of the body is.

Moments of Inertia. and reminds us of the analogous equation for linear momentum p= mv, which is of the form. The kinetic energy of the body is. Moments of Inerta Suppose a body s movng on a crcular path wth constant speed Let s consder two quanttes: the body s angular momentum L about the center of the crcle, and ts knetc energy T How are these

More information

Topology optimization of plate structures subject to initial excitations for minimum dynamic performance index

Topology optimization of plate structures subject to initial excitations for minimum dynamic performance index th World Congress on Structural and Multdsclnary Otmsaton 7 th -2 th, June 25, Sydney Australa oology otmzaton of late structures subject to ntal exctatons for mnmum dynamc erformance ndex Kun Yan, Gengdong

More information

Finite Element Modelling of truss/cable structures

Finite Element Modelling of truss/cable structures Pet Schreurs Endhoven Unversty of echnology Department of Mechancal Engneerng Materals echnology November 3, 214 Fnte Element Modellng of truss/cable structures 1 Fnte Element Analyss of prestressed structures

More information

Hidden Markov Model Cheat Sheet

Hidden Markov Model Cheat Sheet Hdden Markov Model Cheat Sheet (GIT ID: dc2f391536d67ed5847290d5250d4baae103487e) Ths document s a cheat sheet on Hdden Markov Models (HMMs). It resembles lecture notes, excet that t cuts to the chase

More information

Computational Modelling of the Unbalanced Magnetic Pull by Finite Element Method

Computational Modelling of the Unbalanced Magnetic Pull by Finite Element Method Avalable onlne at www.scencedrect.com Proceda Engneerng 48 (2012 ) 83 89 MMaMS 2012 Computatonal Modellng of the Unbalanced Magnetc Pull by Fnte Element Method Martn Donát a * a Brno Unversty of Technology,

More information

The Bellman Equation

The Bellman Equation The Bellman Eqaton Reza Shadmehr In ths docment I wll rovde an elanaton of the Bellman eqaton, whch s a method for otmzng a cost fncton and arrvng at a control olcy.. Eamle of a game Sose that or states

More information

Research on Co-simulation for Mechatronic System of Parallel Robot

Research on Co-simulation for Mechatronic System of Parallel Robot Research on Co-smulaton for Mechatronc System of Parallel Robot Lu Yongxan School of Mechancal Engneerng and Automaton, Northeastern Unversty, Wenhua Road -, Heng Dstrct, Shenyang 0004, P.R. Chna, Zhu

More information

χ x B E (c) Figure 2.1.1: (a) a material particle in a body, (b) a place in space, (c) a configuration of the body

χ x B E (c) Figure 2.1.1: (a) a material particle in a body, (b) a place in space, (c) a configuration of the body Secton.. Moton.. The Materal Body and Moton hyscal materals n the real world are modeled usng an abstract mathematcal entty called a body. Ths body conssts of an nfnte number of materal partcles. Shown

More information

Temperature. Chapter Heat Engine

Temperature. Chapter Heat Engine Chapter 3 Temperature In prevous chapters of these notes we ntroduced the Prncple of Maxmum ntropy as a technque for estmatng probablty dstrbutons consstent wth constrants. In Chapter 9 we dscussed the

More information

Solutions to Exercises in Astrophysical Gas Dynamics

Solutions to Exercises in Astrophysical Gas Dynamics 1 Solutons to Exercses n Astrophyscal Gas Dynamcs 1. (a). Snce u 1, v are vectors then, under an orthogonal transformaton, u = a j u j v = a k u k Therefore, u v = a j a k u j v k = δ jk u j v k = u j

More information

Turbulence classification of load data by the frequency and severity of wind gusts. Oscar Moñux, DEWI GmbH Kevin Bleibler, DEWI GmbH

Turbulence classification of load data by the frequency and severity of wind gusts. Oscar Moñux, DEWI GmbH Kevin Bleibler, DEWI GmbH Turbulence classfcaton of load data by the frequency and severty of wnd gusts Introducton Oscar Moñux, DEWI GmbH Kevn Blebler, DEWI GmbH Durng the wnd turbne developng process, one of the most mportant

More information

Note 10. Modeling and Simulation of Dynamic Systems

Note 10. Modeling and Simulation of Dynamic Systems Lecture Notes of ME 475: Introducton to Mechatroncs Note 0 Modelng and Smulaton of Dynamc Systems Department of Mechancal Engneerng, Unversty Of Saskatchewan, 57 Campus Drve, Saskatoon, SK S7N 5A9, Canada

More information

PHYS 705: Classical Mechanics. Calculus of Variations II

PHYS 705: Classical Mechanics. Calculus of Variations II 1 PHYS 705: Classcal Mechancs Calculus of Varatons II 2 Calculus of Varatons: Generalzaton (no constrant yet) Suppose now that F depends on several dependent varables : We need to fnd such that has a statonary

More information

Using Genetic Algorithms in System Identification

Using Genetic Algorithms in System Identification Usng Genetc Algorthms n System Identfcaton Ecaterna Vladu Deartment of Electrcal Engneerng and Informaton Technology, Unversty of Oradea, Unverstat, 410087 Oradea, Româna Phone: +40259408435, Fax: +40259408408,

More information

Advanced Topics in Optimization. Piecewise Linear Approximation of a Nonlinear Function

Advanced Topics in Optimization. Piecewise Linear Approximation of a Nonlinear Function Advanced Tocs n Otmzaton Pecewse Lnear Aroxmaton of a Nonlnear Functon Otmzaton Methods: M8L Introducton and Objectves Introducton There exsts no general algorthm for nonlnear rogrammng due to ts rregular

More information

Non-Ideality Through Fugacity and Activity

Non-Ideality Through Fugacity and Activity Non-Idealty Through Fugacty and Actvty S. Patel Deartment of Chemstry and Bochemstry, Unversty of Delaware, Newark, Delaware 19716, USA Corresondng author. E-mal: saatel@udel.edu 1 I. FUGACITY In ths dscusson,

More information

6.3.7 Example with Runga Kutta 4 th order method

6.3.7 Example with Runga Kutta 4 th order method 6.3.7 Example wth Runga Kutta 4 th order method Agan, as an example, 3 machne, 9 bus system shown n Fg. 6.4 s agan consdered. Intally, the dampng of the generators are neglected (.e. d = 0 for = 1, 2,

More information

Physics 4B. Question and 3 tie (clockwise), then 2 and 5 tie (zero), then 4 and 6 tie (counterclockwise) B i. ( T / s) = 1.74 V.

Physics 4B. Question and 3 tie (clockwise), then 2 and 5 tie (zero), then 4 and 6 tie (counterclockwise) B i. ( T / s) = 1.74 V. Physcs 4 Solutons to Chapter 3 HW Chapter 3: Questons:, 4, 1 Problems:, 15, 19, 7, 33, 41, 45, 54, 65 Queston 3-1 and 3 te (clockwse), then and 5 te (zero), then 4 and 6 te (counterclockwse) Queston 3-4

More information

The Dirac Equation for a One-electron atom. In this section we will derive the Dirac equation for a one-electron atom.

The Dirac Equation for a One-electron atom. In this section we will derive the Dirac equation for a one-electron atom. The Drac Equaton for a One-electron atom In ths secton we wll derve the Drac equaton for a one-electron atom. Accordng to Ensten the energy of a artcle wth rest mass m movng wth a velocty V s gven by E

More information

Appendix B. The Finite Difference Scheme

Appendix B. The Finite Difference Scheme 140 APPENDIXES Appendx B. The Fnte Dfference Scheme In ths appendx we present numercal technques whch are used to approxmate solutons of system 3.1 3.3. A comprehensve treatment of theoretcal and mplementaton

More information

Electrical Circuits 2.1 INTRODUCTION CHAPTER

Electrical Circuits 2.1 INTRODUCTION CHAPTER CHAPTE Electrcal Crcuts. INTODUCTION In ths chapter, we brefly revew the three types of basc passve electrcal elements: resstor, nductor and capactor. esstance Elements: Ohm s Law: The voltage drop across

More information

Equivalent Circuit Analysis of Interior Permanent Magnet Synchronous Motor Considering Magnetic saturation

Equivalent Circuit Analysis of Interior Permanent Magnet Synchronous Motor Considering Magnetic saturation Page 0114 World Electrc Vehcle Journal Vol. 3 - ISSN 2032-6653 - 2009 AVERE EVS24 Stavanger, Norway, May 13-16, 2009 Euvalent Crcut Analyss of Interor Permanent Magnet Synchronous Motor Consderng Magnetc

More information

Spin-rotation coupling of the angularly accelerated rigid body

Spin-rotation coupling of the angularly accelerated rigid body Spn-rotaton couplng of the angularly accelerated rgd body Loua Hassan Elzen Basher Khartoum, Sudan. Postal code:11123 E-mal: louaelzen@gmal.com November 1, 2017 All Rghts Reserved. Abstract Ths paper s

More information

Solution Set #3

Solution Set #3 5-55-7 Soluton Set #. Te varaton of refractve ndex wt wavelengt for a transarent substance (suc as glass) may be aroxmately reresented by te emrcal equaton due to Caucy: n [] A + were A and are emrcally

More information

Numerical Heat and Mass Transfer

Numerical Heat and Mass Transfer Master degree n Mechancal Engneerng Numercal Heat and Mass Transfer 06-Fnte-Dfference Method (One-dmensonal, steady state heat conducton) Fausto Arpno f.arpno@uncas.t Introducton Why we use models and

More information

Lecture 10 Support Vector Machines II

Lecture 10 Support Vector Machines II Lecture 10 Support Vector Machnes II 22 February 2016 Taylor B. Arnold Yale Statstcs STAT 365/665 1/28 Notes: Problem 3 s posted and due ths upcomng Frday There was an early bug n the fake-test data; fxed

More information

Field computation with finite element method applied for diagnosis eccentricity fault in induction machine

Field computation with finite element method applied for diagnosis eccentricity fault in induction machine Proceedngs of the Internatonal Conference on Recent Advances n Electrcal Systems, Tunsa, 216 Feld computaton wth fnte element method appled for dagnoss eccentrcty fault n nducton machne Moufd Mohammed,

More information

Chapter 11: Angular Momentum

Chapter 11: Angular Momentum Chapter 11: ngular Momentum Statc Equlbrum In Chap. 4 we studed the equlbrum of pontobjects (mass m) wth the applcaton of Newton s aws F 0 F x y, 0 Therefore, no lnear (translatonal) acceleraton, a0 For

More information

Physics 181. Particle Systems

Physics 181. Particle Systems Physcs 181 Partcle Systems Overvew In these notes we dscuss the varables approprate to the descrpton of systems of partcles, ther defntons, ther relatons, and ther conservatons laws. We consder a system

More information

2 Finite difference basics

2 Finite difference basics Numersche Methoden 1, WS 11/12 B.J.P. Kaus 2 Fnte dfference bascs Consder the one- The bascs of the fnte dfference method are best understood wth an example. dmensonal transent heat conducton equaton T

More information

2.3 Nilpotent endomorphisms

2.3 Nilpotent endomorphisms s a block dagonal matrx, wth A Mat dm U (C) In fact, we can assume that B = B 1 B k, wth B an ordered bass of U, and that A = [f U ] B, where f U : U U s the restrcton of f to U 40 23 Nlpotent endomorphsms

More information

Priority Queuing with Finite Buffer Size and Randomized Push-out Mechanism

Priority Queuing with Finite Buffer Size and Randomized Push-out Mechanism ICN 00 Prorty Queung wth Fnte Buffer Sze and Randomzed Push-out Mechansm Vladmr Zaborovsy, Oleg Zayats, Vladmr Muluha Polytechncal Unversty, Sant-Petersburg, Russa Arl 4, 00 Content I. Introducton II.

More information

coordinates. Then, the position vectors are described by

coordinates. Then, the position vectors are described by Revewng, what we have dscussed so far: Generalzed coordnates Any number of varables (say, n) suffcent to specfy the confguraton of the system at each nstant to tme (need not be the mnmum number). In general,

More information

ENGN 40 Dynamics and Vibrations Homework # 7 Due: Friday, April 15

ENGN 40 Dynamics and Vibrations Homework # 7 Due: Friday, April 15 NGN 40 ynamcs and Vbratons Homework # 7 ue: Frday, Aprl 15 1. Consder a concal hostng drum used n the mnng ndustry to host a mass up/down. A cable of dameter d has the mass connected at one end and s wound/unwound

More information

Canonical transformations

Canonical transformations Canoncal transformatons November 23, 2014 Recall that we have defned a symplectc transformaton to be any lnear transformaton M A B leavng the symplectc form nvarant, Ω AB M A CM B DΩ CD Coordnate transformatons,

More information

Analysis of the Magnetomotive Force of a Three-Phase Winding with Concentrated Coils and Different Symmetry Features

Analysis of the Magnetomotive Force of a Three-Phase Winding with Concentrated Coils and Different Symmetry Features Analyss of the Magnetomotve Force of a Three-Phase Wndng wth Concentrated Cols and Dfferent Symmetry Features Deter Gerlng Unversty of Federal Defense Munch, Neubberg, 85579, Germany Emal: Deter.Gerlng@unbw.de

More information

Rigid body simulation

Rigid body simulation Rgd bod smulaton Rgd bod smulaton Once we consder an object wth spacal etent, partcle sstem smulaton s no longer suffcent Problems Problems Unconstraned sstem rotatonal moton torques and angular momentum

More information

Mechanics Physics 151

Mechanics Physics 151 Mechancs Physcs 5 Lecture 7 Specal Relatvty (Chapter 7) What We Dd Last Tme Worked on relatvstc knematcs Essental tool for epermental physcs Basc technques are easy: Defne all 4 vectors Calculate c-o-m

More information

ELASTIC WAVE PROPAGATION IN A CONTINUOUS MEDIUM

ELASTIC WAVE PROPAGATION IN A CONTINUOUS MEDIUM ELASTIC WAVE PROPAGATION IN A CONTINUOUS MEDIUM An elastc wave s a deformaton of the body that travels throughout the body n all drectons. We can examne the deformaton over a perod of tme by fxng our look

More information

Indeterminate pin-jointed frames (trusses)

Indeterminate pin-jointed frames (trusses) Indetermnate pn-jonted frames (trusses) Calculaton of member forces usng force method I. Statcal determnacy. The degree of freedom of any truss can be derved as: w= k d a =, where k s the number of all

More information

EMF induced in a coil by moving a bar magnet. Induced EMF: Faraday s Law. Induction and Oscillations. Electromagnetic Induction.

EMF induced in a coil by moving a bar magnet. Induced EMF: Faraday s Law. Induction and Oscillations. Electromagnetic Induction. Inducton and Oscllatons Ch. 3: Faraday s Law Ch. 3: AC Crcuts Induced EMF: Faraday s Law Tme-dependent B creates nduced E In partcular: A changng magnetc flux creates an emf n a crcut: Ammeter or voltmeter.

More information

DO NOT DO HOMEWORK UNTIL IT IS ASSIGNED. THE ASSIGNMENTS MAY CHANGE UNTIL ANNOUNCED.

DO NOT DO HOMEWORK UNTIL IT IS ASSIGNED. THE ASSIGNMENTS MAY CHANGE UNTIL ANNOUNCED. EE 539 Homeworks Sprng 08 Updated: Tuesday, Aprl 7, 08 DO NOT DO HOMEWORK UNTIL IT IS ASSIGNED. THE ASSIGNMENTS MAY CHANGE UNTIL ANNOUNCED. For full credt, show all work. Some problems requre hand calculatons.

More information

Lecture 8 Modal Analysis

Lecture 8 Modal Analysis Lecture 8 Modal Analyss 16.0 Release Introducton to ANSYS Mechancal 1 2015 ANSYS, Inc. February 27, 2015 Chapter Overvew In ths chapter free vbraton as well as pre-stressed vbraton analyses n Mechancal

More information

AGC Introduction

AGC Introduction . Introducton AGC 3 The prmary controller response to a load/generaton mbalance results n generaton adjustment so as to mantan load/generaton balance. However, due to droop, t also results n a non-zero

More information

CHAPTER 6. LAGRANGE S EQUATIONS (Analytical Mechanics)

CHAPTER 6. LAGRANGE S EQUATIONS (Analytical Mechanics) CHAPTER 6 LAGRANGE S EQUATIONS (Analytcal Mechancs) 1 Ex. 1: Consder a partcle movng on a fxed horzontal surface. r P Let, be the poston and F be the total force on the partcle. The FBD s: -mgk F 1 x O

More information

Physics 5153 Classical Mechanics. Principle of Virtual Work-1

Physics 5153 Classical Mechanics. Principle of Virtual Work-1 P. Guterrez 1 Introducton Physcs 5153 Classcal Mechancs Prncple of Vrtual Work The frst varatonal prncple we encounter n mechancs s the prncple of vrtual work. It establshes the equlbrum condton of a mechancal

More information

Physics 2102 Spring 2007 Lecture 10 Current and Resistance

Physics 2102 Spring 2007 Lecture 10 Current and Resistance esstance Is Futle! Physcs 0 Sprng 007 Jonathan Dowlng Physcs 0 Sprng 007 Lecture 0 Current and esstance Georg Smon Ohm (789-854) What are we gong to learn? A road map lectrc charge lectrc force on other

More information

EP523 Introduction to QFT I

EP523 Introduction to QFT I EP523 Introducton to QFT I Toc 0 INTRODUCTION TO COURSE Deartment of Engneerng Physcs Unversty of Gazante Setember 2011 Sayfa 1 Content Introducton Revew of SR, QM, RQM and EMT Lagrangan Feld Theory An

More information

Lectures on Multivariable Feedback Control

Lectures on Multivariable Feedback Control Lectures on Multvarable Feedback Control Al Karmpour Department of Electrcal Engneerng, Faculty of Engneerng, Ferdows Unversty of Mashhad June 200) Chapter 9: Quanttatve feedback theory Lecture Notes of

More information

Spring 2002 Lecture #13

Spring 2002 Lecture #13 44-50 Sprng 00 ecture # Dr. Jaehoon Yu. Rotatonal Energy. Computaton of oments of nerta. Parallel-as Theorem 4. Torque & Angular Acceleraton 5. Work, Power, & Energy of Rotatonal otons Remember the md-term

More information

Module 1 : The equation of continuity. Lecture 1: Equation of Continuity

Module 1 : The equation of continuity. Lecture 1: Equation of Continuity 1 Module 1 : The equaton of contnuty Lecture 1: Equaton of Contnuty 2 Advanced Heat and Mass Transfer: Modules 1. THE EQUATION OF CONTINUITY : Lectures 1-6 () () () (v) (v) Overall Mass Balance Momentum

More information

Part C Dynamics and Statics of Rigid Body. Chapter 5 Rotation of a Rigid Body About a Fixed Axis

Part C Dynamics and Statics of Rigid Body. Chapter 5 Rotation of a Rigid Body About a Fixed Axis Part C Dynamcs and Statcs of Rgd Body Chapter 5 Rotaton of a Rgd Body About a Fxed Axs 5.. Rotatonal Varables 5.. Rotaton wth Constant Angular Acceleraton 5.3. Knetc Energy of Rotaton, Rotatonal Inerta

More information

First Law: A body at rest remains at rest, a body in motion continues to move at constant velocity, unless acted upon by an external force.

First Law: A body at rest remains at rest, a body in motion continues to move at constant velocity, unless acted upon by an external force. Secton 1. Dynamcs (Newton s Laws of Moton) Two approaches: 1) Gven all the forces actng on a body, predct the subsequent (changes n) moton. 2) Gven the (changes n) moton of a body, nfer what forces act

More information

COMPOSITE BEAM WITH WEAK SHEAR CONNECTION SUBJECTED TO THERMAL LOAD

COMPOSITE BEAM WITH WEAK SHEAR CONNECTION SUBJECTED TO THERMAL LOAD COMPOSITE BEAM WITH WEAK SHEAR CONNECTION SUBJECTED TO THERMAL LOAD Ákos Jósef Lengyel, István Ecsed Assstant Lecturer, Professor of Mechancs, Insttute of Appled Mechancs, Unversty of Mskolc, Mskolc-Egyetemváros,

More information

8. THE CONTACT DYNAMICS METHOD

8. THE CONTACT DYNAMICS METHOD 8 THE CONTACT DYNAMICS METHOD 8 Introducton The Contact Dynamcs ( CD ) method was ntroduced at the begnnng of the 990es by M Jean and JJ Moreau (Jean és Moreau, 992; Jean, 999) The method turned out to

More information

Module 3: Element Properties Lecture 1: Natural Coordinates

Module 3: Element Properties Lecture 1: Natural Coordinates Module 3: Element Propertes Lecture : Natural Coordnates Natural coordnate system s bascally a local coordnate system whch allows the specfcaton of a pont wthn the element by a set of dmensonless numbers

More information

Modeling of Dynamic Systems

Modeling of Dynamic Systems Modelng of Dynamc Systems Ref: Control System Engneerng Norman Nse : Chapters & 3 Chapter objectves : Revew the Laplace transform Learn how to fnd a mathematcal model, called a transfer functon Learn how

More information

Errors for Linear Systems

Errors for Linear Systems Errors for Lnear Systems When we solve a lnear system Ax b we often do not know A and b exactly, but have only approxmatons  and ˆb avalable. Then the best thng we can do s to solve ˆx ˆb exactly whch

More information

The equation of motion of a dynamical system is given by a set of differential equations. That is (1)

The equation of motion of a dynamical system is given by a set of differential equations. That is (1) Dynamcal Systems Many engneerng and natural systems are dynamcal systems. For example a pendulum s a dynamcal system. State l The state of the dynamcal system specfes t condtons. For a pendulum n the absence

More information

PHYS 1101 Practice problem set 12, Chapter 32: 21, 22, 24, 57, 61, 83 Chapter 33: 7, 12, 32, 38, 44, 49, 76

PHYS 1101 Practice problem set 12, Chapter 32: 21, 22, 24, 57, 61, 83 Chapter 33: 7, 12, 32, 38, 44, 49, 76 PHYS 1101 Practce problem set 1, Chapter 3: 1,, 4, 57, 61, 83 Chapter 33: 7, 1, 3, 38, 44, 49, 76 3.1. Vsualze: Please reer to Fgure Ex3.1. Solve: Because B s n the same drecton as the ntegraton path s

More information

Mechanics Physics 151

Mechanics Physics 151 Mechancs Physcs 5 Lecture 0 Canoncal Transformatons (Chapter 9) What We Dd Last Tme Hamlton s Prncple n the Hamltonan formalsm Dervaton was smple δi δ p H(, p, t) = 0 Adonal end-pont constrants δ t ( )

More information

EN40: Dynamics and Vibrations. Homework 4: Work, Energy and Linear Momentum Due Friday March 1 st

EN40: Dynamics and Vibrations. Homework 4: Work, Energy and Linear Momentum Due Friday March 1 st EN40: Dynamcs and bratons Homework 4: Work, Energy and Lnear Momentum Due Frday March 1 st School of Engneerng Brown Unversty 1. The fgure (from ths publcaton) shows the energy per unt area requred to

More information

Lecture # 02: Pressure measurements and Measurement Uncertainties

Lecture # 02: Pressure measurements and Measurement Uncertainties AerE 3L & AerE343L Lecture Notes Lecture # 0: Pressure measurements and Measurement Uncertantes Dr. Hu H Hu Deartment of Aerosace Engneerng Iowa State Unversty Ames, Iowa 500, U.S.A Mechancal Pressure

More information

Formal solvers of the RT equation

Formal solvers of the RT equation Formal solvers of the RT equaton Formal RT solvers Runge- Kutta (reference solver) Pskunov N.: 979, Master Thess Long characterstcs (Feautrer scheme) Cannon C.J.: 970, ApJ 6, 55 Short characterstcs (Hermtan

More information

12. The Hamilton-Jacobi Equation Michael Fowler

12. The Hamilton-Jacobi Equation Michael Fowler 1. The Hamlton-Jacob Equaton Mchael Fowler Back to Confguraton Space We ve establshed that the acton, regarded as a functon of ts coordnate endponts and tme, satsfes ( ) ( ) S q, t / t+ H qpt,, = 0, and

More information

DC Circuits. Crossing the emf in this direction +ΔV

DC Circuits. Crossing the emf in this direction +ΔV DC Crcuts Delverng a steady flow of electrc charge to a crcut requres an emf devce such as a battery, solar cell or electrc generator for example. mf stands for electromotve force, but an emf devce transforms

More information

DECOUPLING THEORY HW2

DECOUPLING THEORY HW2 8.8 DECOUPLIG THEORY HW2 DOGHAO WAG DATE:OCT. 3 207 Problem We shall start by reformulatng the problem. Denote by δ S n the delta functon that s evenly dstrbuted at the n ) dmensonal unt sphere. As a temporal

More information

Chapter 12. Ordinary Differential Equation Boundary Value (BV) Problems

Chapter 12. Ordinary Differential Equation Boundary Value (BV) Problems Chapter. Ordnar Dfferental Equaton Boundar Value (BV) Problems In ths chapter we wll learn how to solve ODE boundar value problem. BV ODE s usuall gven wth x beng the ndependent space varable. p( x) q(

More information

Algorithms for factoring

Algorithms for factoring CSA E0 235: Crytograhy Arl 9,2015 Instructor: Arta Patra Algorthms for factorng Submtted by: Jay Oza, Nranjan Sngh Introducton Factorsaton of large ntegers has been a wdely studed toc manly because of

More information

EN40: Dynamics and Vibrations. Homework 7: Rigid Body Kinematics

EN40: Dynamics and Vibrations. Homework 7: Rigid Body Kinematics N40: ynamcs and Vbratons Homewor 7: Rgd Body Knematcs School of ngneerng Brown Unversty 1. In the fgure below, bar AB rotates counterclocwse at 4 rad/s. What are the angular veloctes of bars BC and C?.

More information

U.C. Berkeley CS294: Beyond Worst-Case Analysis Luca Trevisan September 5, 2017

U.C. Berkeley CS294: Beyond Worst-Case Analysis Luca Trevisan September 5, 2017 U.C. Berkeley CS94: Beyond Worst-Case Analyss Handout 4s Luca Trevsan September 5, 07 Summary of Lecture 4 In whch we ntroduce semdefnte programmng and apply t to Max Cut. Semdefnte Programmng Recall that

More information

Chapter - 2. Distribution System Power Flow Analysis

Chapter - 2. Distribution System Power Flow Analysis Chapter - 2 Dstrbuton System Power Flow Analyss CHAPTER - 2 Radal Dstrbuton System Load Flow 2.1 Introducton Load flow s an mportant tool [66] for analyzng electrcal power system network performance. Load

More information