Reactive Power Compensation in Mechanical Systems

Size: px
Start display at page:

Download "Reactive Power Compensation in Mechanical Systems"

Transcription

1 Reactive Power Compensation in Mechanical Systems Carlos Rengifo, Bassel Kaar, Yannick Aoustin, Christine Chevallereau To cite this version: Carlos Rengifo, Bassel Kaar, Yannick Aoustin, Christine Chevallereau. Reactive Power Compensation in Mechanical Systems. The 2n Joint International Conference on Multiboy System Dynamics - IMSD212, May 212, Stuttgart, Germany. <hal > HAL I: hal Submitte on 11 Oct 212 HAL is a multi-isciplinary open access archive for the eposit an issemination of scientific research ocuments, whether they are publishe or not. The ocuments may come from teaching an research institutions in France or abroa, or from public or private research centers. L archive ouverte pluriisciplinaire HAL, est estinée au épôt et à la iffusion e ocuments scientifiques e niveau recherche, publiés ou non, émanant es établissements enseignement et e recherche français ou étrangers, es laboratoires publics ou privés.

2 The 2 n Joint International Conference on Multiboy System Dynamics May 29 June 1, 212, Stuttgart, Germany Reactive Power Compensation in Mechanical Systems Rengifo Carlos, Kaar Bassel, Aoustin Yannick, Chevallereau Christine Faculty of Electronical Engineering Universia el Cauca Calle 5 No 4-7, Popayan, Colombia caferen@unicauca.eu.co L UNAM, IRCCyN, UMR, CNRS 6597 CNRS, École Centrale e Nantes 1, rue e la Noë, BP 9211, 44321, Nantes, France [firstname.lastname]@irrcyn.ec-nantes.fr ABSTRACT In this paper the problem of energy consumption in mechanical systems is approache from an electrical engineering point of view. To achieve this objective classical concepts in electrical networks theory like apparent power, reactive power an power factor have been extene to mechanical systems. This paper focus on the role of springs in mechanical systems to avoi power oscillations between joint actuators an loas. Such oscillations are a major problem because they unnecessarily increases the mean-square value of joint torques an by consequence Joule effect losses in the actuators. The minimization of these oscillations is known as "reactive power compensation". The main points illustrate in this paper are the funamental limitations on reactive power compensation an the negative effect on the energy consumption of the harmonic content of the reference trajectory. 1 Introuction In rotational mechanical systems like robot joints, the instantaneous power elivere by a motion actuator is given by the prouct between the joint torque an the joint velocity. If the mechanical loa introuces a phase shift between these two variables, the sign of the instantaneous power is not constant. As a consequence the flow of energy between the actuator an the loa is biirectional. For a passive loa, it implies that a part of the receive energy is store an subsequently forware to the actuator. This phenomenon entails two main problems. The first one is that most actuators o not have energy recovery capabilities so this forware energy is lost by Joule effect. The secon one is that the mean-square value of the torque require to prouce a given motion is unnecessarily incremente because of the aitional transfer of energy from the actuator to the loa. In the same way as in electrical networks capacitors are use to compensate phase shifts between voltage an current create by inuctive loas, we show that springs play the same role in mechanical systems. Thus, in both electrical an mechanical systems, phase shift compensation between inputs an outputs is a funamental issue for the improvement of the energy transfer between a source an a loa. Despite of this similarity, efficient power transmission in mechanical systems is far from being evient. The main ifficulties arise from the non-sinusoial nature of joint robotic motions an the non linear ynamics present in most mechanical systems. It is important to note that in the case of nonlinear systems, phase shift compensation between torque an velocity oes not necessarily guarantee an uniirectional flow of energy. Moreover, only in the case of linear systems excite with sinusoial inputs, phase-shift compensation guarantees an efficient energy transfer between source an loa [2]. The objective of this paper is to show the applicability of recent theoretical avances [3], [5], [6] in powerfactor compensation of nonlinear electrical networks excite with non-sinusoial signals for the minimization of energy consumption in mechanical systems. To achieve this objective it has been necessary to generalize classical concepts in electrical engineering like power factor, apparent power an reactive power. This paper is organize as follows. In section 2 the problem statement an the assumptions for the rest of the paper are presente. In section 3 mathematical operators for the root-mean-square value of a perioical signal an for the active power are introuce. In section 4 reactive power compensation is formulate as an optimization problem using two criteria, the mean-square value of the joint torque an the so-calle "power

3 factor". In section 5 a geometrical interpretation of the power factor is given. In section 6 an optimality conition vali for the two criteria is euce. In section 7 two numerical examples are presente. One of them illustrates the funamental limitations on reactive power compensation an the other one shows the negative effect it can have the harmonic content of the reference trajectory in energy consumption. Last Section is evote to conclusions an perspectives. 2 Problem statement The problem aresse in this paper is how to optimize the energy transfer between a motion actuator an a mechanical loa. In robotic systems, for example, the loa correspons to the mechanical structure of the robot an the motion actuator to an electric, hyraulic, pneumatic or any other type of evice suppling the joint torque necessary to prouce the esire motion. The compensator system can be a torsional spring or any other elastic element capable of storing energy. The mechanical loa is suppose to be functioning as the feeback system presente in Figure 1. q a(t) is the esire motion for the actuate joints, Σ l is the ynamical system representing the mechanical loa, Σ c (θ) is a non-issipative passive system calle mechanical compensator an Ω is a given close loop controller Γ c Compensator Σ c q a(t) + Ω Γ + Γ l Σ l q a (t) Controller Loa Figure 1. Close loop mechanical system. For the close loop system of Figure 1 the following assumptions will be mae A1: The reference perioic motion q a(t) is a vector of smooth signals with a common perio. A2: The controller Ω ensures the convergence of q a (t) to q a(t). A3: The close loop system is consiere to be functioning for a long time before t =. For t, q a (t) is consiere to be converge to q a(t). In such a case, it is sai that the system has reache the steay state. A4: The mechanical loa Σ l is suppose to be a passive ynamical system [7]. Uner the assumptions A1 an A2 passivity implies that the average power elivere by the actuator in a cycle is nonnegative 1 To Γ T l (t) q a(t) t (1) A5: The mechanical compensator is compose by non-issipative passive elements. Uner the assumptions A1 an A2, it implies 1 To Γ T c (t) q a (t) t = (2) 3 Mathematical notation Given two perioical vector value signals x(t) IR n an y(t) IR n with a common funamental perio, the application of the binary operator <, > to x(t) an y(t) gives a real quantity efine as x(t), y(t) 1 To x T (t) y(t) t (3)

4 Using this operator, assumptions A4 an A5 can be written as Γ l (t), q a(t) an Γ c (t), q a(t) =. The value x(t), x(t) correspons to the mean-square value of the vector signal x(t) x(t), x(t) = 1 To x T (t) x(t) t, (4) an by consequence x(t), x(t) is the root-mean-square (rms) value of x(t) IR n. In the sake of simplicity, instea of x(t), x(t), the rms value is enote as follows x(t) x(t), x(t) (5) 4 Optimization criteria In this section two ifferent criteria for the minimization of steay state energy consumption are presente. Optimization will be mae with respect to θ, a vector containing the parameters of the compensator system Σ. For example, if Σ is a torsional spring, θ is its stiffness. The first criterion is given by Γ 2 1 To Γ T (t) Γ(t) t (6) Despite of the wiesprea utilization of (6) as a performance inex for trajectory generation in robotic systems, its main inconvenient is the ifficulty to assert when a given Γ 2 is small enough for a given motion. A particular value of Γ 2 coul be consiere small for certain motions but not for others. This fact oes not allow a proper comparison between motions with ifferent. It woul be "unfair" to compare slow an fast motions just in terms of Γ 2 even if they are applie to the same system. The other criterion we present in this section is known in electrical engineering as power factor [4]. The equivalent of the efinition presente in [4] for mechanical systems is p f = P S (7) with P Γ, q a n S Γ i q a i Γ i an q a i being the i-th component of the vectors Γ IR n an q a IR n. The scalar quantities P an S, respectively known as active power an apparent power [2], satisfy the Cauchy-Schwarz inequality As Γ = Γ l + Γ c (see Figure 1), active power can be rewritten as P = Γ l, q a + Γc, q a S P S (9) Uner the assumption A4 the term Γ c, q a is zero an by consequence active power P oes not epen on the compensator system P = Γ l, q a (11) Uner the assumption A5 the term Γ l, q a is a nonnegative quantity. By consequence the inequality (9) becomes P S (12) The above inequality implies that power factor is a quantity between an 1. The main avantage of powerfactor is that is a normalize quantity. When this quantity is close to zero, most part of the energy transfere to the loa is store an subsequently forware to the actuator. This phenomenon entails two main problems. The first one is that most actuators o not have energy recovery capabilities so this forware energy is lost by Joule effect. The secon one is that the mean-square value of the torque require to prouce a given motion is unnecessarily incremente. Conversely, an unitary power factor implies that for all time t power goes from the actuator to the loa. These aspects will be explaine in the next section. (8) (1)

5 Apparent power S Reactive power Q α Active power P Figure 2. Power factor is the cosine of α. When reactive power is zeroe, then power factor equals to one. 5 Unerstaning power factor Power factor can be unerstoo through the right-angle triangle presente in Figure 2. The hypotenuse represents the apparent power, the horizontal cathetus the active power an the cosine of the angle between them is the power factor. The vertical cathetus is known as reactive power. From Figure 2 it can be seen that a reuction in the reactive power leas to an improvement of the power factor. To illustrate this iea, the close loop system presente in Figure 1 will be consiere. The mechanical loa Ω l is suppose to be a linear single actuate system Γ l = J q + f v q (J an f v being the inertia moment an the viscous friction coefficient). The compensator is suppose to be a torsional spring escribe by Γ c = k q. Uner the assumption A3, the close system can be escribe as For this system active an apparent power are given by Γ = J q a + f v q a + k qa (13) }{{}}{{} Γ l Γ c P =< J q a + f v q a + k q a, q a > S = J q a + f v q a + k q a q a Using Fourier series it can be prove that terms < q a, q a > an < q a, q a > are zero for any perioic signal q a(t). In such a case the expressions for P an S can be simplifie as with P = f v q a 2 S = J 2 q a 2 + fv 2 q a 2 + k 2 qa J k < q a, qa > q a = fv 2 q a 2 + J q a + k qa 2 q a = ( f v q a 2 ) 2 + ( J q a + k qa q a ) 2 = P 2 + Q 2 (14) (15) Q = J q a + k q a q a (16) Depening on the harmonic content of q a(t), a positive constant k minimizing Q can be foun. If k is such that J q a + k q a = for all t, then Q is zeroe an by consequence the power factor becomes unitary. In such a case, the compensate mechanical loa is Γ = f v q a, which is equivalent to a pure viscous friction element. Γ = f v q a implies that instantaneous power remains non negative for all time t an that energy flows in one irection, from the actuator to the loa. 6 Optimality conitions Firstly, we euce a conition for the maximization of the power factor with respect to θ (a vector containing the parameters of the compensator Σ). Equation (11) shows that the active power P is inepenent of θ.

6 By consequence, the minimization of the apparent power S leas to the maximization of the quotient P/S, which is efine as the power factor. Apparent power can be written in the following way S = = = = n Γ i q a i n Γ li + Γ ci q a i n Γli + Γ ci 2 q a i n Γli 2 + Γ ci Γ li, Γ ci q a i (17) Conversely, the apparent power for the uncompensate system (Γ c (t) ) is given by S u = n Γli 2 q a i (18) If we compare the expressions for S an S u, it can be conclue that the following conition guarantees S < S u, Γ ci Γ li, Γ ci < i {1,..., n}, (19) If the above inequalities are satisfie for all i, then apparent power of each actuator is ecrease an so the total apparent power S. Conition (19), however, is sufficient but not necessary. The total apparent power S coul be ecrease even if the above inequalities are satisfie for some (but not all) values of i. In the case of a single-actuate system (n = 1) conition (19) becomes both necessary an sufficient. Now we euce a necessary an sufficient conition for the minimization of the mean-square joint torque. The joint torque supplie by the actuator is ecompose as the sum of Γ l an Γ c (see Figure 1) Γ 2 = 1 To [Γ l (t) + Γ c (t)] T [Γ l (t) + Γ c (t)] t = 1 To Γ T l (t) Γ l (t) + Γ T c (t) Γ c (t) + 2Γ T l (t) Γ c (t)t Using the operators. an <, > the above equation can be rewritten as (2) If the following inequality is satisfie or equivalently Γ 2 = Γ l 2 + Γ c Γ l, Γ c (21) Γ c Γ l, Γ c <, (22) n Γ ci Γ li, Γ ci <, (23) then Γ 2 < Γ l 2. In such a case, the mechanical compensator leas to a less energy consumption in the sense of the criterion (6). Criteria (19) an (23) are equivalent only for single-actuate systems. 7 Numerical simulations In this section two numerical examples are presente. The first one illustrates the funamental limitations on reactive power compensation an the other one shows the negative effect that can have the harmonic content of the reference trajectory in energy consumption.

7 25 Minimal amplitue for Ko > [egrees] Normalize Frequency Figure 3. Amplitue-Frequency optimality conition. Minimal motion amplitue require to obtain a positive optimal spring constant. Frequency is normalize with respect to the natural frequency of the penulum. Example 1 Consier the close-loop mechanical system presente in Figure 1 an suppose that Σ l is a single penulum system, Σ c is a series torsional spring an Ω a control law satisfying the assumption A3. The parameters of the penulum in the international units (MKS) are J =.981 (inertia), m =.1 (mass), l = 1 (length), f v =.1 (viscous friction) an g = 9.81 is the gravity force. The objective is to maximize the power factor by optimizing the stiffness of the spring. The esire motion is suppose to be given by The steay state close loop ynamics can be escribe as follows q a(t) = A sin (ω o t) (24) Γ l = J q a + m g l sin ( q a) + fv q a Γ c = k q a (25) For small motion amplitue sin ( q a) can be approximate by q a. Uner this assumption it can be shown that the optimality conition (19) leas to k < 2 ( J ω 2 o m g l ) (26) The above inequality implies that power factor can be improve using a torsional spring only when frequency motion is greater than the natural frequency of the penulum ω n = m g l/j, otherwise problem is infeasible because a negative k is require. If the reference motion oes not allow to approximate sin ( ) qa by qa the optimality conition (19) gives an upper limit for k epening on A an ω o. Unfortunately, an expression in a close form like (26) cannot be obtaine in that case. The graph presente in Figure 3 shows the minimal value of A require to obtain a non-negative upper limit for k for a given frequency ω o. If the pair (A, ω o ) is below the curve, the optimality conition (19) cannot be satisfie for any positive value of k. If (A, ω o ) is above the curve, there exist a set of positive values of k leaing to an improvement of the power factor. It is interesting to note that for frequencies higher than the natural frequency, optimization is possible for all amplitues. As seen in Section 4 if the compensate mechanical loa is seen by the actuator as pure viscous friction element, then the power factor becomes unitary. Using the equation (25) it can be conclue that Γ = f v q a can be obtaine, if an only if, there exist a constant value of k satisfying J q a + m g l sin ( q a) + k q a =, t (27)

8 1.9 Optimal Power Factor Wn 1.Wn 2.Wn 5.Wn Motion amplitue [egrees] Figure 4. Maximal power factor in a single penulum system when the reference motion is a sinusoial signal of given amplitue. The above equation can be satisfie for a constant k only if the amplitue of the esire motion is small. In such a case, k is given by k = Jω 2 o m g l. If sin ( q a) cannot be approximate by q a then an unitary optimal power factor cannot be obtaine. Figure 4 shows the maximal power factor as a function of the amplitue an frequency. From this figure it can be observe that for a fixe frequency if the amplitue of the esire motion is augmente then the maximal power factor that can be obtaine ecreases. Conversely, for a motion of fixe amplitue, greater is the frequency, greater is the maximal power factor. Example 2 Reference motion in robotic systems is often inicate by using only initial an final conitions on joint positions an velocities. This implies that an infinite number of time functions satisfying such conitions can be generate. For example, for the system of the previous example, the two perioic motions presente in Figure 5 satisfy the conitions q() = 2 o, q(t/2) = 2 o, q() =, q(t/2) =. Both reference motions have a funamental frequency equal to ω o = 1 ra/seg which is ten times the natural frequency of the penulum (ω n = m g l/j). One of the motions is efine as a single frequency sinusoial signal an the other one is obtaine by concatenating two polynomials of thir orer. Sinusoial motion: q a(t) = A sin (ω o t) (28) Polynomial motion: a 3 t 3 + a 2 t 2 + a 1 t + a, qa(t) = b 3 t 3 + b 2 t 2 + b 1 t + b, t < To 2 2 t < (29) As motions are almost ientical it coul be expecte that the joint torque curves for the polynomial an the sinusoial references be also quite similar. However, this is not always true. It epens on the transfer function Γ(s)/q a(s). If Γ(s)/q a(s) has a strong gain at high frequencies, some of the high-orer harmonic components of the polynomial motion coul have a more important gain that the funamental component. In such a case, the torques coul be quite ifferent even if motions are very similar. If the high frequency gain of Γ(s)/q a(s) is limite, the convergence of q a (t) towars q a(t) can be seriously affecte. In summary, there is trae-off between tracking an energy consumption. To illustrate this point a linearize version of

9 2 Joint position Degrees Time [sec] Joint velocity 2 Degrees/sec Time [sec] Figure 5. Reference motions for the example 2. One of them is efine as a single frequency sinusoial signal (soli line) an the secon one by concatenating two polynomials of thir orer (ashe line). the penulum system will be consiere Γ = J q a + f v q a + (m g l + k) q a (3) By taking the Laplace transform of the last equation, the following transfer function is obtaine Γ(s) q a(s) = J s2 + f v s + (m g l + k) (31) This transfer function is unrealistic because the resulting steay-state gain increases inefinitely as frequency increases. In practice, close-loop steay-state gain is limite by the actuator ynamics. To obtain a more convincing transfer function the following consierations will be mae Actuator is suppose to be moele as a low-pass filter with a cutoff frequency of 1ω o (ω o being the funamental frequency of the reference motion) G a (s) = 1 (.1s + 1) 2 (32) Controller Ω (see Figure 1) is represente by a classical lea compensator [1] G c (s) = 5 1.1s + 1.1s + 1 (33) With the above consierations the steay-state gain of the transfer function Γ(s)/q a(s) ecreases as frequency increases when ω > 1ω o. (Figure (6)). For frequencies between ω o an 1ω o the gain increases as frequency increases. From this figure it can be seen that harmonic components with frequencies between 2ω o an 1ω o have a gain more than ten times larger than the gain of the funamental harmonic ω o. As consequence, even if the two motions presente in Figure 5 are very similar, the corresponing instantaneous power curves are very ifferent (see Figure 7). From this Figure it can be seen that for the sinusoial motion instantaneous power remains non-negative, an for the polynomial motion power oscillations are important. For the sinusoial motion power factor is unitary an Γ 2 =.369, for the polynomial motion power factor is.4569 an Γ 2 =.1769.

10 1 3 Steay state gain Normalize frequency [ω/ω ] o Figure 6. Steay state gain of the close loop transfer function Γ(jω)/q a(jω) when actuator ynamics is consiere. 2 Steay state power Power [J/s] Time [sec] Figure 7. Instantaneous power for the sinusoial motion (soli line) an for the polynomial motion (ashe line).

11 8 Conclusions an perspectives The problem of the steay state reactive power compensation in close loop mechanical system subject to perioic motion has been presente. Compensation is one by using non-issipative passive elements like torsional springs. Parameter selection for these elements is formulate as an optimization problem. Two ifferent performance inex are presente. One of them is the classical mean-square value of the torque an the other one, inspire from the electrical networks theory, is known as power factor. This latter is a normalize quantity between an 1 which epens on the torque an on the esire motion. It has the avantage to allow the comparison between systems with ifferent motions. Base on the iea of optimization of power factor by the use of capacitors in electrical system, the use of springs is propose to optimize the "energy" consumption in mechanical system. Since the stiffness is a positive coefficient the efficiency of this approach epens on the esire trajectory. In the example 1, the positiveness of the spring stiffness epens on the amplitue an the frequency of the motion. An unitary power factor can be obtaine when the compensate mechanical loa is seen by the actuator as a linear viscous friction element of the form Γ = f v q a. In such a case instantaneous power remains on-negative for all time t an energy flows in one irection, from the actuator to the loa. Another aspect stuie in the paper is the effect of the harmonic content of the reference motion in the power factor of the system. In the Example 2, it is shown that very similar reference motions can prouce very ifferent power factors. In the cite example, this phenomenon is explaine by the amplification of the high orer harmonic components of the reference motion. The feeback system presente in Figure 1, allows to inclue springs only in active joints. Our main perspective is then to evelop a conceptual framework allowing to stuy more general interconnections between mechanical systems an passive compensators. It woul be interest, for example, to unerstan the effect of passive arms in the energy consume by a bipeal robot. Acknowlegements Carlos F. Rengifo woul like to acknowlege an express his sincere gratitue to Universia el Cauca for the financial support given to him uring this project. REFERENCES [1] Y. Chen. Replacing a PID controller by a lag-lea compensator for a robot - A frequency-response approach. IEEE Transactions on Robotics an Automation, 5(2): , apr [2] E. Garcia-Canseco, R. Grino, R. Ortega, M. Salichs, an A.M. Stankovic. Power-factor compensation of electrical circuits. IEEE Control Systems Magazine, 27(2):46 59, April 27. [3] Dimitri Jeltsema. Moeling an Control of Nonlinear Networks: A Power-Base Perspective. PhD thesis, Delft University of Technology, 25. [4] G Kassakian, M.F Schlecht, an G.C Verghese. Principles of power electronics. Reaing MA: Aison- Wesley, [5] H. Lev-Ari an A.M. Stankovic. Hilbert space techniques for moeling an compensation of reactive power in energy processing systems. IEEE Transactions on Circuits an Systems I: Funamental Theory an Applications, 5(4):54 556, april 23. [6] R. Ortega, D. Jeltsema, an J.M.A. Scherpen. Power shaping: a new paraigm for stabilization of nonlinear RLC circuits. IEEE Transactions on Automatic Control, 48(1): , oct. 23. [7] Romeo Ortega, Julio Antonio Loría Perez, Per Johan Nicklasson, an Hebertt J. Sira-Ramirez. Passivity-base control of Euler-Lagrange systems: mechanical, electrical, an electromechanical applications. Springer, 1998.

Adaptive Control of the Boost DC-AC Converter

Adaptive Control of the Boost DC-AC Converter Aaptive Control of the Boost DC-AC Converter Carolina Albea-Sanchez, Carlos Canuas De Wit, Francisco Gorillo Alvarez To cite this version: Carolina Albea-Sanchez, Carlos Canuas De Wit, Francisco Gorillo

More information

u t v t v t c a u t b a v t u t v t b a

u t v t v t c a u t b a v t u t v t b a Nonlinear Dynamical Systems In orer to iscuss nonlinear ynamical systems, we must first consier linear ynamical systems. Linear ynamical systems are just systems of linear equations like we have been stuying

More information

The Principle of Least Action

The Principle of Least Action Chapter 7. The Principle of Least Action 7.1 Force Methos vs. Energy Methos We have so far stuie two istinct ways of analyzing physics problems: force methos, basically consisting of the application of

More information

Total Energy Shaping of a Class of Underactuated Port-Hamiltonian Systems using a New Set of Closed-Loop Potential Shape Variables*

Total Energy Shaping of a Class of Underactuated Port-Hamiltonian Systems using a New Set of Closed-Loop Potential Shape Variables* 51st IEEE Conference on Decision an Control December 1-13 212. Maui Hawaii USA Total Energy Shaping of a Class of Uneractuate Port-Hamiltonian Systems using a New Set of Close-Loop Potential Shape Variables*

More information

Chapter 31: RLC Circuits. PHY2049: Chapter 31 1

Chapter 31: RLC Circuits. PHY2049: Chapter 31 1 Chapter 31: RLC Circuits PHY049: Chapter 31 1 LC Oscillations Conservation of energy Topics Dampe oscillations in RLC circuits Energy loss AC current RMS quantities Force oscillations Resistance, reactance,

More information

Experimental Robustness Study of a Second-Order Sliding Mode Controller

Experimental Robustness Study of a Second-Order Sliding Mode Controller Experimental Robustness Stuy of a Secon-Orer Sliing Moe Controller Anré Blom, Bram e Jager Einhoven University of Technology Department of Mechanical Engineering P.O. Box 513, 5600 MB Einhoven, The Netherlans

More information

Applications of First Order Equations

Applications of First Order Equations Applications of First Orer Equations Viscous Friction Consier a small mass that has been roppe into a thin vertical tube of viscous flui lie oil. The mass falls, ue to the force of gravity, but falls more

More information

Harmonic Modelling of Thyristor Bridges using a Simplified Time Domain Method

Harmonic Modelling of Thyristor Bridges using a Simplified Time Domain Method 1 Harmonic Moelling of Thyristor Briges using a Simplifie Time Domain Metho P. W. Lehn, Senior Member IEEE, an G. Ebner Abstract The paper presents time omain methos for harmonic analysis of a 6-pulse

More information

An inductance lookup table application for analysis of reluctance stepper motor model

An inductance lookup table application for analysis of reluctance stepper motor model ARCHIVES OF ELECTRICAL ENGINEERING VOL. 60(), pp. 5- (0) DOI 0.478/ v07-0-000-y An inuctance lookup table application for analysis of reluctance stepper motor moel JAKUB BERNAT, JAKUB KOŁOTA, SŁAWOMIR

More information

Sequential Multiplier with Sub-linear Gate Complexity

Sequential Multiplier with Sub-linear Gate Complexity Sequential Multiplier with Sub-linear Gate Complexity Anwar Hasan, Christophe Negre To cite this version: Anwar Hasan, Christophe Negre. Sequential Multiplier with Sub-linear Gate Complexity. [Research

More information

Optimal Variable-Structure Control Tracking of Spacecraft Maneuvers

Optimal Variable-Structure Control Tracking of Spacecraft Maneuvers Optimal Variable-Structure Control racking of Spacecraft Maneuvers John L. Crassiis 1 Srinivas R. Vaali F. Lanis Markley 3 Introuction In recent years, much effort has been evote to the close-loop esign

More information

Differentiability, Computing Derivatives, Trig Review. Goals:

Differentiability, Computing Derivatives, Trig Review. Goals: Secants vs. Derivatives - Unit #3 : Goals: Differentiability, Computing Derivatives, Trig Review Determine when a function is ifferentiable at a point Relate the erivative graph to the the graph of an

More information

Chapter 6. Electromagnetic Oscillations and Alternating Current

Chapter 6. Electromagnetic Oscillations and Alternating Current hapter 6 Electromagnetic Oscillations an Alternating urrent hapter 6: Electromagnetic Oscillations an Alternating urrent (hapter 31, 3 in textbook) 6.1. Oscillations 6.. The Electrical Mechanical Analogy

More information

Arithmetic Distributions of Convergents Arising from Jacobi-Perron Algorithm

Arithmetic Distributions of Convergents Arising from Jacobi-Perron Algorithm Arithmetic Distributions of Convergents Arising from Jacobi-Perron Algorithm Valerie Berthe, H Nakaa, R Natsui To cite this version: Valerie Berthe, H Nakaa, R Natsui Arithmetic Distributions of Convergents

More information

Table of Common Derivatives By David Abraham

Table of Common Derivatives By David Abraham Prouct an Quotient Rules: Table of Common Derivatives By Davi Abraham [ f ( g( ] = [ f ( ] g( + f ( [ g( ] f ( = g( [ f ( ] g( g( f ( [ g( ] Trigonometric Functions: sin( = cos( cos( = sin( tan( = sec

More information

Role of parameters in the stochastic dynamics of a stick-slip oscillator

Role of parameters in the stochastic dynamics of a stick-slip oscillator Proceeing Series of the Brazilian Society of Applie an Computational Mathematics, v. 6, n. 1, 218. Trabalho apresentao no XXXVII CNMAC, S.J. os Campos - SP, 217. Proceeing Series of the Brazilian Society

More information

A Novel Decoupled Iterative Method for Deep-Submicron MOSFET RF Circuit Simulation

A Novel Decoupled Iterative Method for Deep-Submicron MOSFET RF Circuit Simulation A Novel ecouple Iterative Metho for eep-submicron MOSFET RF Circuit Simulation CHUAN-SHENG WANG an YIMING LI epartment of Mathematics, National Tsing Hua University, National Nano evice Laboratories, an

More information

Closed loop observer-based parameter estimation of quantum systems with a single population measurement

Closed loop observer-based parameter estimation of quantum systems with a single population measurement Close loop observer-base parameter estimation of quantum systems with a single population measurement Zaki Leghtas To cite this version: Zaki Leghtas. Close loop observer-base parameter estimation of quantum

More information

Differentiability, Computing Derivatives, Trig Review

Differentiability, Computing Derivatives, Trig Review Unit #3 : Differentiability, Computing Derivatives, Trig Review Goals: Determine when a function is ifferentiable at a point Relate the erivative graph to the the graph of an original function Compute

More information

Optimization of a point-mass walking model using direct collocation and sequential quadratic programming

Optimization of a point-mass walking model using direct collocation and sequential quadratic programming Optimization of a point-mass walking moel using irect collocation an sequential quaratic programming Chris Dembia June 5, 5 Telescoping actuator y Stance leg Point-mass boy m (x,y) Swing leg x Leg uring

More information

AN INTRODUCTION TO AIRCRAFT WING FLUTTER Revision A

AN INTRODUCTION TO AIRCRAFT WING FLUTTER Revision A AN INTRODUCTION TO AIRCRAFT WIN FLUTTER Revision A By Tom Irvine Email: tomirvine@aol.com January 8, 000 Introuction Certain aircraft wings have experience violent oscillations uring high spee flight.

More information

19 Eigenvalues, Eigenvectors, Ordinary Differential Equations, and Control

19 Eigenvalues, Eigenvectors, Ordinary Differential Equations, and Control 19 Eigenvalues, Eigenvectors, Orinary Differential Equations, an Control This section introuces eigenvalues an eigenvectors of a matrix, an iscusses the role of the eigenvalues in etermining the behavior

More information

6.003 Homework #7 Solutions

6.003 Homework #7 Solutions 6.003 Homework #7 Solutions Problems. Secon-orer systems The impulse response of a secon-orer CT system has the form h(t) = e σt cos(ω t + φ)u(t) where the parameters σ, ω, an φ are relate to the parameters

More information

The canonical controllers and regular interconnection

The canonical controllers and regular interconnection Systems & Control Letters ( www.elsevier.com/locate/sysconle The canonical controllers an regular interconnection A.A. Julius a,, J.C. Willems b, M.N. Belur c, H.L. Trentelman a Department of Applie Mathematics,

More information

Lecture 2 Lagrangian formulation of classical mechanics Mechanics

Lecture 2 Lagrangian formulation of classical mechanics Mechanics Lecture Lagrangian formulation of classical mechanics 70.00 Mechanics Principle of stationary action MATH-GA To specify a motion uniquely in classical mechanics, it suffices to give, at some time t 0,

More information

PES 1120 Spring 2014, Spendier Lecture 36/Page 1

PES 1120 Spring 2014, Spendier Lecture 36/Page 1 PES 0 Spring 04, Spenier ecture 36/Page Toay: chapter 3 - R circuits: Dampe Oscillation - Driven series R circuit - HW 9 ue Wenesay - FQs Wenesay ast time you stuie the circuit (no resistance) The total

More information

Stator/Rotor Interface Analysis for Piezoelectric Motors

Stator/Rotor Interface Analysis for Piezoelectric Motors Stator/Rotor Interface Analysis for Piezoelectric Motors K Harmouch, Yves Bernard, Laurent Daniel To cite this version: K Harmouch, Yves Bernard, Laurent Daniel. Stator/Rotor Interface Analysis for Piezoelectric

More information

Exponential Tracking Control of Nonlinear Systems with Actuator Nonlinearity

Exponential Tracking Control of Nonlinear Systems with Actuator Nonlinearity Preprints of the 9th Worl Congress The International Feeration of Automatic Control Cape Town, South Africa. August -9, Exponential Tracking Control of Nonlinear Systems with Actuator Nonlinearity Zhengqiang

More information

NON-SMOOTH DYNAMICS USING DIFFERENTIAL-ALGEBRAIC EQUATIONS PERSPECTIVE: MODELING AND NUMERICAL SOLUTIONS. A Thesis PRIYANKA GOTIKA

NON-SMOOTH DYNAMICS USING DIFFERENTIAL-ALGEBRAIC EQUATIONS PERSPECTIVE: MODELING AND NUMERICAL SOLUTIONS. A Thesis PRIYANKA GOTIKA NON-SMOOTH DYNAMICS USING DIFFERENTIAL-ALGEBRAIC EQUATIONS PERSPECTIVE: MODELING AND NUMERICAL SOLUTIONS A Thesis by PRIYANKA GOTIKA Submitte to the Office of Grauate Stuies of Texas A&M University in

More information

'HVLJQ &RQVLGHUDWLRQ LQ 0DWHULDO 6HOHFWLRQ 'HVLJQ 6HQVLWLYLW\,1752'8&7,21

'HVLJQ &RQVLGHUDWLRQ LQ 0DWHULDO 6HOHFWLRQ 'HVLJQ 6HQVLWLYLW\,1752'8&7,21 Large amping in a structural material may be either esirable or unesirable, epening on the engineering application at han. For example, amping is a esirable property to the esigner concerne with limiting

More information

Local well-posedness of nonlocal Burgers equations

Local well-posedness of nonlocal Burgers equations Local well-poseness of nonlocal Burgers equations Sylvie Benzoni-Gavage To cite this version: Sylvie Benzoni-Gavage. Local well-poseness of nonlocal Burgers equations. Differential Integral Equations,

More information

Lecture 6: Control of Three-Phase Inverters

Lecture 6: Control of Three-Phase Inverters Yoash Levron The Anrew an Erna Viterbi Faculty of Electrical Engineering, Technion Israel Institute of Technology, Haifa 323, Israel yoashl@ee.technion.ac.il Juri Belikov Department of Computer Systems,

More information

TRAJECTORY TRACKING FOR FULLY ACTUATED MECHANICAL SYSTEMS

TRAJECTORY TRACKING FOR FULLY ACTUATED MECHANICAL SYSTEMS TRAJECTORY TRACKING FOR FULLY ACTUATED MECHANICAL SYSTEMS Francesco Bullo Richar M. Murray Control an Dynamical Systems California Institute of Technology Pasaena, CA 91125 Fax : + 1-818-796-8914 email

More information

Predictive control of synchronous generator: a multiciterial optimization approach

Predictive control of synchronous generator: a multiciterial optimization approach Preictive control of synchronous generator: a multiciterial optimization approach Marián Mrosko, Eva Miklovičová, Ján Murgaš Abstract The paper eals with the preictive control esign for nonlinear systems.

More information

Modeling time-varying storage components in PSpice

Modeling time-varying storage components in PSpice Moeling time-varying storage components in PSpice Dalibor Biolek, Zenek Kolka, Viera Biolkova Dept. of EE, FMT, University of Defence Brno, Czech Republic Dept. of Microelectronics/Raioelectronics, FEEC,

More information

THE VAN KAMPEN EXPANSION FOR LINKED DUFFING LINEAR OSCILLATORS EXCITED BY COLORED NOISE

THE VAN KAMPEN EXPANSION FOR LINKED DUFFING LINEAR OSCILLATORS EXCITED BY COLORED NOISE Journal of Soun an Vibration (1996) 191(3), 397 414 THE VAN KAMPEN EXPANSION FOR LINKED DUFFING LINEAR OSCILLATORS EXCITED BY COLORED NOISE E. M. WEINSTEIN Galaxy Scientific Corporation, 2500 English Creek

More information

Switching Time Optimization in Discretized Hybrid Dynamical Systems

Switching Time Optimization in Discretized Hybrid Dynamical Systems Switching Time Optimization in Discretize Hybri Dynamical Systems Kathrin Flaßkamp, To Murphey, an Sina Ober-Blöbaum Abstract Switching time optimization (STO) arises in systems that have a finite set

More information

Chapter 2 Lagrangian Modeling

Chapter 2 Lagrangian Modeling Chapter 2 Lagrangian Moeling The basic laws of physics are use to moel every system whether it is electrical, mechanical, hyraulic, or any other energy omain. In mechanics, Newton s laws of motion provie

More information

Math 1B, lecture 8: Integration by parts

Math 1B, lecture 8: Integration by parts Math B, lecture 8: Integration by parts Nathan Pflueger 23 September 2 Introuction Integration by parts, similarly to integration by substitution, reverses a well-known technique of ifferentiation an explores

More information

Dynamics of the synchronous machine

Dynamics of the synchronous machine ELEC0047 - Power system ynamics, control an stability Dynamics of the synchronous machine Thierry Van Cutsem t.vancutsem@ulg.ac.be www.montefiore.ulg.ac.be/~vct These slies follow those presente in course

More information

VIRTUAL STRUCTURE BASED SPACECRAFT FORMATION CONTROL WITH FORMATION FEEDBACK

VIRTUAL STRUCTURE BASED SPACECRAFT FORMATION CONTROL WITH FORMATION FEEDBACK AIAA Guiance, Navigation, an Control Conference an Exhibit 5-8 August, Monterey, California AIAA -9 VIRTUAL STRUCTURE BASED SPACECRAT ORMATION CONTROL WITH ORMATION EEDBACK Wei Ren Ranal W. Bear Department

More information

Simple Electromagnetic Motor Model for Torsional Analysis of Variable Speed Drives with an Induction Motor

Simple Electromagnetic Motor Model for Torsional Analysis of Variable Speed Drives with an Induction Motor DOI: 10.24352/UB.OVGU-2017-110 TECHNISCHE MECHANIK, 37, 2-5, (2017), 347-357 submitte: June 15, 2017 Simple Electromagnetic Motor Moel for Torsional Analysis of Variable Spee Drives with an Inuction Motor

More information

Module 2. DC Circuit. Version 2 EE IIT, Kharagpur

Module 2. DC Circuit. Version 2 EE IIT, Kharagpur Moule 2 DC Circuit Lesson 9 Analysis of c resistive network in presence of one non-linear element Objectives To unerstan the volt (V ) ampere ( A ) characteristics of linear an nonlinear elements. Concept

More information

A Simple Model for the Calculation of Plasma Impedance in Atmospheric Radio Frequency Discharges

A Simple Model for the Calculation of Plasma Impedance in Atmospheric Radio Frequency Discharges Plasma Science an Technology, Vol.16, No.1, Oct. 214 A Simple Moel for the Calculation of Plasma Impeance in Atmospheric Raio Frequency Discharges GE Lei ( ) an ZHANG Yuantao ( ) Shanong Provincial Key

More information

Local Input-to-State Stabilization of 1-D Linear Reaction-Diffusion Equation with Bounded Feedback

Local Input-to-State Stabilization of 1-D Linear Reaction-Diffusion Equation with Bounded Feedback Local Input-to-State Stabilization of -D Linear Reaction-Diffusion Equation with Boune Feeback Aneel Tanwani, Swann Marx, Christophe Prieur To cite this version: Aneel Tanwani, Swann Marx, Christophe Prieur.

More information

On Using Unstable Electrohydraulic Valves for Control

On Using Unstable Electrohydraulic Valves for Control Kailash Krishnaswamy Perry Y. Li Department of Mechanical Engineering, University of Minnesota, 111 Church St. SE, Minneapolis, MN 55455 e-mail: kk,pli @me.umn.eu On Using Unstable Electrohyraulic Valves

More information

Nearly finite Chacon Transformation

Nearly finite Chacon Transformation Nearly finite hacon Transformation Élise Janvresse, Emmanuel Roy, Thierry De La Rue To cite this version: Élise Janvresse, Emmanuel Roy, Thierry De La Rue Nearly finite hacon Transformation 2018

More information

THE RELAXATION SPEED IN THE CASE THE FLOW SATISFIES EXPONENTIAL DECAY OF CORRELATIONS

THE RELAXATION SPEED IN THE CASE THE FLOW SATISFIES EXPONENTIAL DECAY OF CORRELATIONS HE RELAXAIO SPEED I HE CASE HE FLOW SAISFIES EXPOEIAL DECAY OF CORRELAIOS Brice Franke, hi-hien guyen o cite this version: Brice Franke, hi-hien guyen HE RELAXAIO SPEED I HE CASE HE FLOW SAISFIES EXPOEIAL

More information

The effect of nonvertical shear on turbulence in a stably stratified medium

The effect of nonvertical shear on turbulence in a stably stratified medium The effect of nonvertical shear on turbulence in a stably stratifie meium Frank G. Jacobitz an Sutanu Sarkar Citation: Physics of Fluis (1994-present) 10, 1158 (1998); oi: 10.1063/1.869640 View online:

More information

Chapter 14: Vibration Generations Mechanisms: Self Excited Vibration

Chapter 14: Vibration Generations Mechanisms: Self Excited Vibration hapter 14: ibration Generations echanisms: Self Ecite ibration Introuction: Self-ecite systems begin to vibrate of their own accor spontaneously, the amplitue increasing until some nonlinear effect limits

More information

Lagrangian and Hamiltonian Mechanics

Lagrangian and Hamiltonian Mechanics Lagrangian an Hamiltonian Mechanics.G. Simpson, Ph.. epartment of Physical Sciences an Engineering Prince George s Community College ecember 5, 007 Introuction In this course we have been stuying classical

More information

Advanced Partial Differential Equations with Applications

Advanced Partial Differential Equations with Applications MIT OpenCourseWare http://ocw.mit.eu 18.306 Avance Partial Differential Equations with Applications Fall 2009 For information about citing these materials or our Terms of Use, visit: http://ocw.mit.eu/terms.

More information

Examining Geometric Integration for Propagating Orbit Trajectories with Non-Conservative Forcing

Examining Geometric Integration for Propagating Orbit Trajectories with Non-Conservative Forcing Examining Geometric Integration for Propagating Orbit Trajectories with Non-Conservative Forcing Course Project for CDS 05 - Geometric Mechanics John M. Carson III California Institute of Technology June

More information

Laplacian Cooperative Attitude Control of Multiple Rigid Bodies

Laplacian Cooperative Attitude Control of Multiple Rigid Bodies Laplacian Cooperative Attitue Control of Multiple Rigi Boies Dimos V. Dimarogonas, Panagiotis Tsiotras an Kostas J. Kyriakopoulos Abstract Motivate by the fact that linear controllers can stabilize the

More information

Interpolated Rigid-Body Motions and Robotics

Interpolated Rigid-Body Motions and Robotics Interpolate Rigi-Boy Motions an Robotics J.M. Selig Faculty of Business, Computing an Info. Management. Lonon South Bank University, Lonon SE AA, U.K. seligjm@lsbu.ac.uk Yaunquing Wu Dept. Mechanical Engineering.

More information

NOTES ON EULER-BOOLE SUMMATION (1) f (l 1) (n) f (l 1) (m) + ( 1)k 1 k! B k (y) f (k) (y) dy,

NOTES ON EULER-BOOLE SUMMATION (1) f (l 1) (n) f (l 1) (m) + ( 1)k 1 k! B k (y) f (k) (y) dy, NOTES ON EULER-BOOLE SUMMATION JONATHAN M BORWEIN, NEIL J CALKIN, AND DANTE MANNA Abstract We stuy a connection between Euler-MacLaurin Summation an Boole Summation suggeste in an AMM note from 196, which

More information

State Space Analysis of Power System Stability Enhancement with Used the STATCOM

State Space Analysis of Power System Stability Enhancement with Used the STATCOM tate pace Analysis of Power ystem tability Enhancement with Use the ACOM M. Mahavian () - G. hahgholian () () Department of Electrical Engineering, Islamic Aza University, Naein Branch, Esfahan, Iran ()

More information

Free rotation of a rigid body 1 D. E. Soper 2 University of Oregon Physics 611, Theoretical Mechanics 5 November 2012

Free rotation of a rigid body 1 D. E. Soper 2 University of Oregon Physics 611, Theoretical Mechanics 5 November 2012 Free rotation of a rigi boy 1 D. E. Soper 2 University of Oregon Physics 611, Theoretical Mechanics 5 November 2012 1 Introuction In this section, we escribe the motion of a rigi boy that is free to rotate

More information

12.11 Laplace s Equation in Cylindrical and

12.11 Laplace s Equation in Cylindrical and SEC. 2. Laplace s Equation in Cylinrical an Spherical Coorinates. Potential 593 2. Laplace s Equation in Cylinrical an Spherical Coorinates. Potential One of the most important PDEs in physics an engineering

More information

Math 342 Partial Differential Equations «Viktor Grigoryan

Math 342 Partial Differential Equations «Viktor Grigoryan Math 342 Partial Differential Equations «Viktor Grigoryan 6 Wave equation: solution In this lecture we will solve the wave equation on the entire real line x R. This correspons to a string of infinite

More information

On state representations of time-varying nonlinear systems

On state representations of time-varying nonlinear systems On state representations of time-varying nonlinear systems Paulo Sérgio Pereira a Silva a, Simone Batista a, a University of São Paulo, Escola Politécnicca PTC Av. Luciano Gualberto trav. 03, 158, 05508-900

More information

Impact of DFIG based Wind Energy Conversion System on Fault Studies and Power Swings

Impact of DFIG based Wind Energy Conversion System on Fault Studies and Power Swings Impact of DFIG base Win Energy Conversion System on Fault Stuies an Power Swings Likin Simon Electrical Engineering Department Inian Institute of Technology, Maras Email: ee133@ee.iitm.ac.in K Shanti Swarup

More information

Robust Tracking Control of Robot Manipulator Using Dissipativity Theory

Robust Tracking Control of Robot Manipulator Using Dissipativity Theory Moern Applie Science July 008 Robust racking Control of Robot Manipulator Using Dissipativity heory Hongrui Wang Key Lab of Inustrial Computer Control Engineering of Hebei Province Yanshan University Qinhuangao

More information

Transmission Line Matrix (TLM) network analogues of reversible trapping processes Part B: scaling and consistency

Transmission Line Matrix (TLM) network analogues of reversible trapping processes Part B: scaling and consistency Transmission Line Matrix (TLM network analogues of reversible trapping processes Part B: scaling an consistency Donar e Cogan * ANC Eucation, 308-310.A. De Mel Mawatha, Colombo 3, Sri Lanka * onarecogan@gmail.com

More information

Lower Bounds for the Smoothed Number of Pareto optimal Solutions

Lower Bounds for the Smoothed Number of Pareto optimal Solutions Lower Bouns for the Smoothe Number of Pareto optimal Solutions Tobias Brunsch an Heiko Röglin Department of Computer Science, University of Bonn, Germany brunsch@cs.uni-bonn.e, heiko@roeglin.org Abstract.

More information

Design and Application of Fault Current Limiter in Iran Power System Utility

Design and Application of Fault Current Limiter in Iran Power System Utility Australian Journal of Basic an Applie Sciences, 7(): 76-8, 13 ISSN 1991-8178 Design an Application of Fault Current Limiter in Iran Power System Utility M. Najafi, M. Hoseynpoor Department of Electrical

More information

G j dq i + G j. q i. = a jt. and

G j dq i + G j. q i. = a jt. and Lagrange Multipliers Wenesay, 8 September 011 Sometimes it is convenient to use reunant coorinates, an to effect the variation of the action consistent with the constraints via the metho of Lagrange unetermine

More information

Time scaling control for an underactuated biped robot

Time scaling control for an underactuated biped robot Time scaling control for an underactuated biped robot Christine Chevallereau To cite this version: Christine Chevallereau. Time scaling control for an underactuated biped robot. IEEE Transactions on Robotics

More information

Determine Power Transfer Limits of An SMIB System through Linear System Analysis with Nonlinear Simulation Validation

Determine Power Transfer Limits of An SMIB System through Linear System Analysis with Nonlinear Simulation Validation Determine Power Transfer Limits of An SMIB System through Linear System Analysis with Nonlinear Simulation Valiation Yin Li, Stuent Member, IEEE, Lingling Fan, Senior Member, IEEE Abstract This paper extens

More information

arxiv: v1 [cond-mat.stat-mech] 9 Jan 2012

arxiv: v1 [cond-mat.stat-mech] 9 Jan 2012 arxiv:1201.1836v1 [con-mat.stat-mech] 9 Jan 2012 Externally riven one-imensional Ising moel Amir Aghamohammai a 1, Cina Aghamohammai b 2, & Mohamma Khorrami a 3 a Department of Physics, Alzahra University,

More information

Mechatronics by Analogy and Application to Legged Locomotion

Mechatronics by Analogy and Application to Legged Locomotion Mechatronics by Analogy an Application to Legge Locomotion by Victor Ragusila A thesis submitte in conformity with the requirements for the egree of Doctor of Philosophy Grauate Department of Aerospace

More information

RE-CENTERING CAPABILITY EVALUATION OF SEISMIC ISOLATION SYSTEMS BASED ON ENERGY CONCEPTS

RE-CENTERING CAPABILITY EVALUATION OF SEISMIC ISOLATION SYSTEMS BASED ON ENERGY CONCEPTS 3 th Worl Conference on Earthquake Engineering Vancouver, B.C., Canaa August -6, 004 Paper No. 306 RE-CENTERING CAPABILITY EVALUATION OF SEISMIC ISOLATION SYSTEMS BASED ON ENERGY CONCEPTS Renzo MEDEOT

More information

ORDINARY DIFFERENTIAL EQUATIONS AND SINGULAR INTEGRALS. Gianluca Crippa

ORDINARY DIFFERENTIAL EQUATIONS AND SINGULAR INTEGRALS. Gianluca Crippa Manuscript submitte to AIMS Journals Volume X, Number 0X, XX 200X Website: http://aimsciences.org pp. X XX ORDINARY DIFFERENTIAL EQUATIONS AND SINGULAR INTEGRALS Gianluca Crippa Departement Mathematik

More information

ECE 422 Power System Operations & Planning 7 Transient Stability

ECE 422 Power System Operations & Planning 7 Transient Stability ECE 4 Power System Operations & Planning 7 Transient Stability Spring 5 Instructor: Kai Sun References Saaat s Chapter.5 ~. EPRI Tutorial s Chapter 7 Kunur s Chapter 3 Transient Stability The ability of

More information

Nested Saturation with Guaranteed Real Poles 1

Nested Saturation with Guaranteed Real Poles 1 Neste Saturation with Guarantee Real Poles Eric N Johnson 2 an Suresh K Kannan 3 School of Aerospace Engineering Georgia Institute of Technology, Atlanta, GA 3332 Abstract The global stabilization of asymptotically

More information

Calculus in the AP Physics C Course The Derivative

Calculus in the AP Physics C Course The Derivative Limits an Derivatives Calculus in the AP Physics C Course The Derivative In physics, the ieas of the rate change of a quantity (along with the slope of a tangent line) an the area uner a curve are essential.

More information

Linear First-Order Equations

Linear First-Order Equations 5 Linear First-Orer Equations Linear first-orer ifferential equations make up another important class of ifferential equations that commonly arise in applications an are relatively easy to solve (in theory)

More information

A Note on Exact Solutions to Linear Differential Equations by the Matrix Exponential

A Note on Exact Solutions to Linear Differential Equations by the Matrix Exponential Avances in Applie Mathematics an Mechanics Av. Appl. Math. Mech. Vol. 1 No. 4 pp. 573-580 DOI: 10.4208/aamm.09-m0946 August 2009 A Note on Exact Solutions to Linear Differential Equations by the Matrix

More information

6 Wave equation in spherical polar coordinates

6 Wave equation in spherical polar coordinates 6 Wave equation in spherical polar coorinates We now look at solving problems involving the Laplacian in spherical polar coorinates. The angular epenence of the solutions will be escribe by spherical harmonics.

More information

Stabilization of a Class of Underactuated Mechanical Systems via Interconnection and Damping Assignment

Stabilization of a Class of Underactuated Mechanical Systems via Interconnection and Damping Assignment Stabilization of a Class of Uneractuate Mechanical Systems via Interconnection an Damping Assignment Romeo Ortega Lab. es Signaux et Systèmes CNRS-SUPELEC Gif sur Yvette 99 FRANCE tel. no:(33)--69-85-7-65

More information

Chapter 11: Feedback and PID Control Theory

Chapter 11: Feedback and PID Control Theory Chapter 11: Feeback an D Control Theory Chapter 11: Feeback an D Control Theory. ntrouction Feeback is a mechanism for regulating a physical system so that it maintains a certain state. Feeback works by

More information

MATHEMATICAL ANALYSIS OF A PARABOLIC-ELLIPTIC MODEL FOR BRAIN LACTATE KINETICS

MATHEMATICAL ANALYSIS OF A PARABOLIC-ELLIPTIC MODEL FOR BRAIN LACTATE KINETICS MATHEMATICAL ANALYSIS OF A PARABOLIC-ELLIPTIC MODEL FOR BRAIN LACTATE KINETICS Alain Miranville To cite this version: Alain Miranville. MATHEMATICAL ANALYSIS OF A PARABOLIC-ELLIPTIC MODEL FOR BRAIN LACTATE

More information

Conservation laws a simple application to the telegraph equation

Conservation laws a simple application to the telegraph equation J Comput Electron 2008 7: 47 51 DOI 10.1007/s10825-008-0250-2 Conservation laws a simple application to the telegraph equation Uwe Norbrock Reinhol Kienzler Publishe online: 1 May 2008 Springer Scienceusiness

More information

4. CONTROL OF ZERO-SEQUENCE CURRENT IN PARALLEL THREE-PHASE CURRENT-BIDIRECTIONAL CONVERTERS

4. CONTROL OF ZERO-SEQUENCE CURRENT IN PARALLEL THREE-PHASE CURRENT-BIDIRECTIONAL CONVERTERS 4. CONRO OF ZERO-SEQUENCE CURREN IN PARAE HREE-PHASE CURREN-BIDIRECIONA CONVERERS 4. A NOVE ZERO-SEQUENCE CURREN CONRO 4.. Zero-Sequence Dynamics he parallel boost rectifier moel in Figure.4 an the parallel

More information

Generalization of the persistent random walk to dimensions greater than 1

Generalization of the persistent random walk to dimensions greater than 1 PHYSICAL REVIEW E VOLUME 58, NUMBER 6 DECEMBER 1998 Generalization of the persistent ranom walk to imensions greater than 1 Marián Boguñá, Josep M. Porrà, an Jaume Masoliver Departament e Física Fonamental,

More information

The derivative of a function f(x) is another function, defined in terms of a limiting expression: f(x + δx) f(x)

The derivative of a function f(x) is another function, defined in terms of a limiting expression: f(x + δx) f(x) Y. D. Chong (2016) MH2801: Complex Methos for the Sciences 1. Derivatives The erivative of a function f(x) is another function, efine in terms of a limiting expression: f (x) f (x) lim x δx 0 f(x + δx)

More information

ELEC3114 Control Systems 1

ELEC3114 Control Systems 1 ELEC34 Control Systems Linear Systems - Moelling - Some Issues Session 2, 2007 Introuction Linear systems may be represente in a number of ifferent ways. Figure shows the relationship between various representations.

More information

LATTICE-BASED D-OPTIMUM DESIGN FOR FOURIER REGRESSION

LATTICE-BASED D-OPTIMUM DESIGN FOR FOURIER REGRESSION The Annals of Statistics 1997, Vol. 25, No. 6, 2313 2327 LATTICE-BASED D-OPTIMUM DESIGN FOR FOURIER REGRESSION By Eva Riccomagno, 1 Rainer Schwabe 2 an Henry P. Wynn 1 University of Warwick, Technische

More information

OPTIMAL CONTROL OF A PRODUCTION SYSTEM WITH INVENTORY-LEVEL-DEPENDENT DEMAND

OPTIMAL CONTROL OF A PRODUCTION SYSTEM WITH INVENTORY-LEVEL-DEPENDENT DEMAND Applie Mathematics E-Notes, 5(005), 36-43 c ISSN 1607-510 Available free at mirror sites of http://www.math.nthu.eu.tw/ amen/ OPTIMAL CONTROL OF A PRODUCTION SYSTEM WITH INVENTORY-LEVEL-DEPENDENT DEMAND

More information

TRACKING CONTROL OF MULTIPLE MOBILE ROBOTS: A CASE STUDY OF INTER-ROBOT COLLISION-FREE PROBLEM

TRACKING CONTROL OF MULTIPLE MOBILE ROBOTS: A CASE STUDY OF INTER-ROBOT COLLISION-FREE PROBLEM 265 Asian Journal of Control, Vol. 4, No. 3, pp. 265-273, September 22 TRACKING CONTROL OF MULTIPLE MOBILE ROBOTS: A CASE STUDY OF INTER-ROBOT COLLISION-FREE PROBLEM Jurachart Jongusuk an Tsutomu Mita

More information

THE USE OF KIRCHOFF S CURRENT LAW AND CUT-SET EQUATIONS IN THE ANALYSIS OF BRIDGES AND TRUSSES

THE USE OF KIRCHOFF S CURRENT LAW AND CUT-SET EQUATIONS IN THE ANALYSIS OF BRIDGES AND TRUSSES Session TH US O KIRCHO S CURRNT LAW AND CUT-ST QUATIONS IN TH ANALYSIS O BRIDGS AND TRUSSS Ravi P. Ramachanran an V. Ramachanran. Department of lectrical an Computer ngineering, Rowan University, Glassboro,

More information

Closed and Open Loop Optimal Control of Buffer and Energy of a Wireless Device

Closed and Open Loop Optimal Control of Buffer and Energy of a Wireless Device Close an Open Loop Optimal Control of Buffer an Energy of a Wireless Device V. S. Borkar School of Technology an Computer Science TIFR, umbai, Inia. borkar@tifr.res.in A. A. Kherani B. J. Prabhu INRIA

More information

Widely Linear Estimation with Complex Data

Widely Linear Estimation with Complex Data Widely Linear Estimation with Complex Data Bernard Picinbono, Pascal Chevalier To cite this version: Bernard Picinbono, Pascal Chevalier. Widely Linear Estimation with Complex Data. IEEE Transactions on

More information

arxiv: v1 [physics.flu-dyn] 8 May 2014

arxiv: v1 [physics.flu-dyn] 8 May 2014 Energetics of a flui uner the Boussinesq approximation arxiv:1405.1921v1 [physics.flu-yn] 8 May 2014 Kiyoshi Maruyama Department of Earth an Ocean Sciences, National Defense Acaemy, Yokosuka, Kanagawa

More information

Nonlinear Adaptive Ship Course Tracking Control Based on Backstepping and Nussbaum Gain

Nonlinear Adaptive Ship Course Tracking Control Based on Backstepping and Nussbaum Gain Nonlinear Aaptive Ship Course Tracking Control Base on Backstepping an Nussbaum Gain Jialu Du, Chen Guo Abstract A nonlinear aaptive controller combining aaptive Backstepping algorithm with Nussbaum gain

More information

Placement and tuning of resonance dampers on footbridges

Placement and tuning of resonance dampers on footbridges Downloae from orbit.tu.k on: Jan 17, 19 Placement an tuning of resonance ampers on footbriges Krenk, Steen; Brønen, Aners; Kristensen, Aners Publishe in: Footbrige 5 Publication ate: 5 Document Version

More information

and from it produce the action integral whose variation we set to zero:

and from it produce the action integral whose variation we set to zero: Lagrange Multipliers Monay, 6 September 01 Sometimes it is convenient to use reunant coorinates, an to effect the variation of the action consistent with the constraints via the metho of Lagrange unetermine

More information

Situation awareness of power system based on static voltage security region

Situation awareness of power system based on static voltage security region The 6th International Conference on Renewable Power Generation (RPG) 19 20 October 2017 Situation awareness of power system base on static voltage security region Fei Xiao, Zi-Qing Jiang, Qian Ai, Ran

More information

Laplace s Equation in Cylindrical Coordinates and Bessel s Equation (II)

Laplace s Equation in Cylindrical Coordinates and Bessel s Equation (II) Laplace s Equation in Cylinrical Coorinates an Bessel s Equation (II Qualitative properties of Bessel functions of first an secon kin In the last lecture we foun the expression for the general solution

More information

Approximate reduction of dynamic systems

Approximate reduction of dynamic systems Systems & Control Letters 57 2008 538 545 www.elsevier.com/locate/sysconle Approximate reuction of ynamic systems Paulo Tabuaa a,, Aaron D. Ames b, Agung Julius c, George J. Pappas c a Department of Electrical

More information