Chapter 4. -ry2 ] [ IXll ] -r/2. V ~ -Xl - X2 + r Xl X2 = -

Size: px
Start display at page:

Download "Chapter 4. -ry2 ] [ IXll ] -r/2. V ~ -Xl - X2 + r Xl X2 = -"

Transcription

1 Chapter 4 () asymptotically stable (2) unstable (3) asympto~ica1ly stable (4) unstable (5) stable (6) unstable!. 4.2 Let f(x) = ax'p + g(x). Near the origin, the term ax'p is dominan~. Hence, sign(f(x)) = sign(ax'p). Consider the case when a < 0 and P is odd. With Vex) = ix2 as a Lyapuf~v function candidate, we have V = x[az'p +g(x)] $ azp+l + klxlp+2 Near the origin, the term axp+l is dominant. Hence, Vex) is negative definite and the origin is asymptotically stable. Consider now the case when a > 0 andp is odd. n. the neighbothood of the origin, sign(f(x» =. sign(x). Hence, a trajectory starting near z = 0 will be alwa,ys moving atay from x = O. This shows that the origin is unstable. When p is even, a similar behavior wiu take place n one side of the origin; namely, on the side x > 0 when a > 0 and x < 0 when a < O. Therefore, the ori~ is Let Vex) = (1/2)(xi + xu. i. n the set {lxll2 ~ r2}, we have Xll ~ r. Hence, T i. 2 2 V ~ -Xl - X2 + r Xl X2 = - [ Xll] X21 [ 1 -r/2 -ry2 ] [ Xll ] 11 X21 11 is negative ~efinite for r < 2. Thus, the origin is asymptotically stable.!to investigate global asymptotic stability, note that the solution of the second equation is X2{t) = exp(-t)f2 (O), which when substituted in the first equation yields i Xl = [-1 + exp(-t)x:ho)}xl i i This is a linear time-varying system whose solution does not have a finite e~cape time. After some finite time the coefficient of Xl on the right-hand side will be less than a negative n4mber. Hence, limt -+oo Xl (t) = O. Thus, the origin is globally asymptotically stable.! (2) Let Vex) = (1/2)(xi + x~) V = -(Xl + x2)(1 - Xl - X2) = -2V(1-2f)! n the region Vex) < 1/2, V is negative definite. Hence, the~.'gin is asymptotically stable. For V > 1/2, V is positive. Hence, trajectories starting in the region Vex) >1/2 cannot ~pproach the origin. n fact, they grew unbounded. Thus, the origin is not globally asymptoticcitlly stable. (3) Let Vex) =xt Px =Pllxi + 2P12XlX2 + P22X~, where P is a positive 4efinite symmetric matrix V = -2P12Xl + 2(Pu - P12 - P22)XX2-2CP22 - P12)X2 + ijigher order terms 59

2 60 CHAPTER 4. Near the origin, the quadratic term dominates the higher-order terms. Thus, V will be negative definite in the neighborhood of the origin if the quadratic term is negative definite. Choosing Pl2 = 1, P22 = 2, and Pu = 3 makes Vex) positive definite and ii(x) negative definite. Hence, the origin is asymptotically stable. t is not globally asymptotically stable since the origin is not the unique equilibrium point. The set {x~ = } is an equilibrium set. (4) Let V(x) = xi + (1/2)x~. Hence, the origin is globally asymptotically stable. 4.4 (a) Take V(w) = (1/2)(Jlwf + J2W~ + J3wi) as a Lyapunov function candidate. v = J1Wc:.h + J2W2W2 + J3W3W3 = (J2 - J3)WW2W3 + (Ja - J1 )WW2W3 + (J1 - J2)WW2W3 = 0 The origin is stable. t is not asymptotically stable since V is identically zero. The closed-loop state equation is J1Wl = (h - J3)W2W3 - kw J2W2 = (J3 - Jl )W3W - k2w2 J3W3 = (J1 - J2)WW2 - k3w3 Using the same function V(w) as in part (a), we obtain Thus, the origin is.globally asymptotically stable. 4.5 Let g(x) = VV; gi(x) = OV/OXi. Ogi a ov 0 2 V OXj = OXj {)xi = OXjOXi Similarly Hence ogj a ov {)2v OXi = OXi OXj ~ OXiOXj Alternatively, suppose Define Ogi ogj -;--=-0-, uxj UXi Vi,j=,...,n

3 61 Similarly, it can be shown av - =gi(x), 'Vi ax; To meet the symmetry requirement, take "y =(3. Take 8 = (3. 2 Vex) = -(3Xl + (a - 2(3)XX2 - (3(Xl + x2)h(x + X2) Taking a = 2(3 and (3 > 0 yields which is negative definite for all x E R2. Now g(x) = (3 [i ~] x ~ Px.::} V(x)';" 1% gt(y) dy = ~XTPx where P is positive definite. Thus, Vex) is a radially unbounded Lyapunov function and the origin is globally asymptotically stable. 4.7 (a) Let VV(x) =g(x). Then, V:= _gt(x)q4>(x). Choose g(x) =Px so that Vex) = (lj2)xtpx. We need to choose P = pt > 0 such that V = -xtpq4>(x) is negative definite. Choosing P =Q-l yields V = _xt4>{x) =- L n i=1 xi4>i(xi) V is negative definite in the neighborhood of the origin because y4>(y) > 0 for y ::f: O. Hence, the origin is asymptotically stable. The function Vex) is radially unbounded. The origin will be globally asymptotically stable if V is negative definite for all x. This will be the case if y4>i(y) > 0 for all y ::f: O. (c) The function 4>2 satisfies the condition y4>i(y) > 0 for all y ::f: O. The function 4>1 satisfies the condition only near y = 0 because 4>1 (y) vanishes at y = 1. Thus, we can only show asymptotic stability of the origin using the Lyapunov function Vex) = xtq-1x = x~ + 2X1X2 + 2x~.

4 Vex) = jt(x)pf(x) is positive semidefinite. To show that it is positive definite, we need to show that V == 0 :} x = O. Since P is positive definite, we need to show that f(x) == 0 if and only if x = 0; that is, the origin is the unique equilibrium point. Suppose, to the contrary, that there is p"# 0 such that f(p) = O. Then, 63 which is a contradiction. Hence, the origin is the unique equilibrium point. To show that V is radially unbounded, we note that for any x E Rn xtpf(x) _ 1 T T, 1 xll~ - 21xll~[x Pf(x) + j (x)px]::; -2' 't/ x E R n Suppose now that f(x)12 ::; cas xl Then But this is a contradiction since x T pf(x)12 < x T 121!F12c < 1!F12C -+ as xli xll~ - xll~ - xll2 2 xtpf(x) 1 xll~ ::; - 2' n 't/ x E R Thus, as xll , the magnitude of at least one component of f(x) must approach 00. This shows that Vex) as xll (c) We have shown that V(x) is positive definite and radially unbounded. Since f(x) = 0 :} x = 0, V(x) < 0, for all x ERn, x"# O. Thus, the origin is globally asymptotically stable Since V l (x) is not negative semidefinite, there exists a point Xo arbitrarily close to the origin such that V1(xo) > O. Let U = {x E Br Vi{x) > O}, where Br C D. Since V{x) is positive definite, we have V(x) > 0 for all x E U. Hence, the origin is unstable Since V1(x) is not negative semidefinite, there exists a point Xo arbitrarily close to the origin such that V (xo) > O. Let U = {x E Br Vi(x) > O}, where Br CD. Since W(x) ~ 0 for all xed, we have Hence, the origin is unstable. Vt(x) = W(x) +,\t}{x) > 0, 't/ x E U ~1) Apply Chetaev's theorem with Vex) = (1/2)(x~ - x~). The function V is positive at points arbitrarily close to the origin on the Xl-axis. Vex) = Xl (x~ + X~X2) - X2{-X2 + x~ + XX2 - X~) = (X~ + XX2)2 + x~{1 - X2 - Xl - x~) :For any 0 < c < 1, there is a domain around the origin where Hence, in this domain, we have 1 - X2 - Xl - x~ > c > 0

5 64 CHAPTER 4. 1 Xz Figure 4.1: Exercise 4.13 (2). The right-hand side of the preceding inequality is positive definite; hence all the conditions of Chetaev's theorem are satisfied and the equilibrium point at the origin is unstable. (2) The system Xl = -x~ + X2 =!l(x), X2 = x~ - x~ =hex} has two equilibrium points at (O,O) and (1,1). The set r ={0:5 Xl :5 1} n {X2 ~ xn n {X2 :5 xn is shown in Figure 4.1. On the boundary X2 = x, 12 = 0 and i > 0; hence, all trajectories on this boundary move into r. On the boundary X2 = x~, t = 0 and 12 > 0; hence, all trajectories on this boundary move into r. Thus, r is positively invariant. nside r, both h and h are positive. Thus all trajectories move toward the equilibriwn point (1,1). Since this happens for trajectories starting arbitrarily close to the origin, we conclude that the origin is unstable Therefore, 12:1 12:1 1 o yg(y) dy ~ 0 y dy = 2x~ V() T [1 1] x, ~ 2Xl +XlX2+ x2 = '2x 1 2 X The matrix of the quadratic form is positive definite. Hence, V(x) is positive definite for all x, and radially unbounded. v = Xlg(Xt}Xl + XX2 + X2Xl + 2X2X2 = g(xl)(x1x2 - x~ - XX2-2XX2-2x~) + x~ = -g(xd(x~ + 2XX2 + 2x~} + x~ = _g(xdxtqx + x~ where Q = [~ ;] is positive definite. Since g(xt} 2: 1 and xtqx 2: 0, we have V :5 -(x~ + 2XX2 + 2x~) + x~ = -(x~ + 2XX2 + x~) = -(Xl + X2)2 This shows that "i is negative semidefinite. We need to apply the invariance principle. V = 0 => 0:5 -(Xl +X2)2 => 02: (Xl +X2}2 => Xl +X2 =0

6 71 Hence, there is a unique equilibrium point at (1,1,1). 81 = [~3 ;3 ~:2] = [~ =! ~1] 8x :1:=(1,1,1) Xs - Xs :1:=(1,1,1) The eigenvalues are -1 and (-1 ± jv3)/2. Hence, the origin is asymptotically stable. The third state equation has equilibrium at X3 = O. Starting with the initial condition xs(o) = 0, we have xs(t) == O. Then, Xl = 1 and Xl(t) grows unbounded. Thus, the equilib'tium point is not globally asymptotieally stable (a) 0= Xl! Substitution of Xl = 0 in the second equation yields Hence, the origin is the unique equilibrium point. -x2(1 + x~) = 0 '* X2 = 0 Hence, the origin is asymptotically stable. (c) Let Vex) =XX2 Vex) = Xl%2 + %lx2 = (XX2-1)x1x~ + (XX2-1 + X~)X1X2 - XX2 V(X) = 4x~ > 0. :1:1:1:2=2 which implies that r is a positively invariant set. (d) The origin is not globally asymptotically stable since trajectories starting in r do not converge to the origin. ~ The equilibrium points are the roots of the equ8:tions X2 =3X '* Xl (4 - xn = 0 The equilibrium points are (0,0), (2,6), and (-2, -6). fj = [ 1-3x~,- 1 ] 8x 3-1 The equilibrium point (0,0) is unstable (saddle). fj / _ [1 1] '* ).2-4=0 '*..\=±2 8x :1:=(0,0) {){) = [-i 1!1]- '* ) ,,\ + 8=0'*..\ = x :1:=(2,6) The equilibrium point (2,6) is asymptotically stable (stable node). 811 [-11 1] 8x :1:=(-2,-6) = 3-1

7 72 CHAPTER 4. The equilibrium point (-2,-6) is asymptotically stable (stable node). (c) Let A = [-;1!1] and P be the solution of PA + ATp = -1. Using Matlab, P is found to be P = [~:~~~~ ~:!~~~]. The eigenvalues of Pare,xmoz{P) = and,xmin{p) = To estimate the region of attraction of (2, 6), shift the equilibrium point to the origin via the change of variables The state equation in the new coordinates is given by i l = -llxl + X2-6X~ - x~ i2 = 3Xl-X2 We use V = xt Px as a Lyapunov function candidate. The derivative V is given by V = -xtx - 2(pUXl +Pl2X2){6 + Xl)X~ ::; -lxll~ -12CPllXl + Pl2X2)X~ - 2Pl2Xfx2 ::; -lxll~ + 12VYtl + Yt211xll~ + p12l1xll~ ::; -( - 2.4r r2)lxll~, for xll2 ::; r Taking r = 0.4, we see that V(x) is negative in {lxll2 S r}. Choosing c <,xmin{p)r 2 = , ensures that {Vex) $ c} C xll2 S r because,xmin{p)xlli S V(x). Take c = Thus, the region of attraction is estimated by {xtpx::; 0.007}. The estimate of the region of attraction of (-2, -6) is done similarly and the constant c is chosen to be A less conservative estimate of the region of attraction can be obtained graphically by plotting the contour of Vex) = 0 in the :l:1-z2 plane and then choosing c and plotting the surface V (x) = c, with increasing c, until we obtain the largest c for which the surface V (x) = c is inside the region {Vex) < O}. The constant c is determined to be 0.1. The two estimates of the region of attraction are shown in Figure 4.2. (d) The phase portrait is shown in Figure 4.3 together with the estimates of the region of attraction obtained in part (c). The stable trajectories of the saddle form a separatrix that divides the plane into two halves, with the right half as the region of attraction of (2,6) and the left half the region of attraction of (-2, -6). Notice that the estimates of the regions of attraction are much smaller that the regions themselves (a) The equilibrium points are the roots of the equations There are three equilibrium points at (-f,-i), (0,0), and"'(l, 1). 8j = [ -(1(/4)sec2(1(Zl/2) 1 ] 8:1: 1 -(1(/4) sec1(1(:l:2/2) 811 _ [ -(1(/2) 1 ] 8:1: (-i,-i) - 1 -(1(/2)' Eigenvalues are - (1(/2) ± = [ -(1(/4) 1 ] Eigenvalues are - (1(/4) ± 1 8:1: (0,0) 1 -(1(/4)' 81 1 = [ -(1(/2) 1 ] Eigenvalues are - (1(/2) ± 1 8:1: (t,t) 1 -(1(/2)'

8 74 CHAPTER x"" 0 /" /! -0.5 '-,.,/ x, Figure 4.5: Exercise Phase portrait with esti mates of the regions of attraction. Figure 4.4: Exercise The dotted line is the contour of V(y) = 0 and the solid line is the contour of f(y) = (3) (4) ~e investigate stability of the origin using linearization. (1) - af = [-1 + 2Xl -1 2xs 0] A = - af = [-1 _ 1 ax _2Xl 0 l' ax ",=0 0 0 A has an eigenvalue at 1; hence, the origin is unstable. (2) Near the origin, sat(y) = y which implies that dec ( z = -2xs - sat y) = 2Xl + 5X2-4xs The eigenvalues of A are -1, -1, -2; hence, the origin is asymptotically stable. (3) of [-2+3Xf 0] Ofl [-2 0 -{) = 2Xl -1 0, A = -f) = -1 x -1 x :1:=0 0 0 The eigenvalues of A are -2, -1, -1; hence, the origin is asymptotically stable. (4) The eigenvalues of A are -1, -i ±j!v'3; hence, the origin is asymptotically stable.

9 77 t can be shown that the minimum eigenvalue of P is given by where 2 a=r+ R t can be easily seen that there are positive cqnstants Cl and C2 such that a 2-42:: C and AminCPCt» 2:: C2, for all t 2:: 0, which shows that Vet, x) is positive definite. Suppose t, 6, and R satisfy. 2 [. ( L C) L6 t] 2 Vet x) = R Xl - -2 ( 1 + -LR) x 2, C R2 2 RC R L R2 1 + R (~ _ C) + L6 _ t > C R2 2 RC R LR 1+ R2 2:: C2 for all t 2:: 0, for some positive constants C and C2' Then 2Cl 2 2C2 2 V(t,x) $ - k;x - k;x2 Hence, V(t, x) is negative definite. This shows that the origin is uniformly asymptotically stable. By linearity, it is exponentially stable. Alternatively, we can conclude that the origin is exponentially stable by noting that Vet, x) satisfies the conditions of Theorem ~ (a) Since get} 2:: a > a, Hence 1 + ag(t} - a 2 2:: 1 + aa - a 2 > 1 V(t,x} 2::!(asinx + X2) cos Xl which shows that V is positive definite in the region xl < 211'. Since get) $ (3, Vet, x) $!(asinxl + X2}2 + ( + a(3 + a 2 )11 - cosxd which shows that Vet, x) is decrescent. v = -[get) - acosxl]x~ - asin 2 Xl - a 2 (1- COSX)X2 sin Xl + ag(t)(l- cosxt} < -(a - a)x~ + a1'(l- cosxd - asin 2 Xl + O(lxl 3 ) = -(a - a)x~ - a(2-1')(1 - COS Xl) + a[2(1 - cosxl) - sin2x] + O(lx 3 ) The term [2(1 - cosxd - sin 2 Xl] is O(Xl3). Hence V $ -(a - a)x~ - a(2-1')(1- cosxd + O(l/x13) (c) The preceding inequality shows ~hat V is negative definite, since near the origin the negative definite quadratic term dominates the cubic qrder term. Thus, the origin is uniformly asymptotically stable.

10 Let Vex) ==!(x~ + x~). V = -xi + X1X2 + x1(xi + x~) sin t - X1X2 - x~ + x2(xi + x~) cost = -(xi + x~) + (xi + X~)(X1 sin t + X2 cos t) < -lxll~ + xll~j(sint)2 + (cost)2 == -lxll~ + xll~ < -(1 - r)lxll~, 'if xll2 :s; r, for any r < 1 Hence, by Theorem 4.10, the origin is exponenti~ stable. Since Vex) =!lxll~, can be estimated by the set {lxll2 :s; r} for any r < Use Vex) ==!(xi + x~) as a Lyapunov function candidate. V == xlh(t)x2 - g(t)x~] + x2[-h(t)x1 - g(t)x~] == -g(t)(xf + x~) :s; -k(xt + x~) the region of attraction Hence, the origin is uniformly asymptotically stable. Since all assumptions hold globally and V(x) is radially unbounded, the origin is globally uniformly asymptotically stable, which answers part (c). The conditions of Theorem 4.10 are not satisfied. Let us linearize the system [0 al h(t) ] A(t) = ax (t, 0) = -h(t) 0 Use V(x) ==!(xi + x~) as a Lyapunov function candidate for the linear system. V = x1h(t)x2 - x2h(t)xl == 0 This shows that solutions starting on the surface Vex) =c remain on that surface for all t. Hence, the origin of the linear system is not exponentially stable. This implies that the origin of the nonlinear system is not exponentially stable. (d) No Linearization at the origin yields the matrix all == [-1+3Xi+x~ -1+2X1X2] = [-1-1] ax.,= X1 X2-1 + xi + 3x~.,=0 1-1 whose eigenvalues are -1 ± j. Hence, the matrix is Hurwitz and the origin is exponentially stable. Consequently, it is asymptotically stable Let Vex) =!(bxi + ax~). V == -b</>(t)(x1 - ax2)2 - ac1/l(t)x~ :s; -b</>o(x - ax2)2 - ac1/lox~ ~f -W3(X) t can be verified that W3 (x) is positive definite for all x. Hence, by Theorem 4.9, the origin is globally uniformly asymptotically stable. Linearization at the origin yields the linear system The invertible change of variables results in the system %1 == 0, %2 = </>(t)zl - </>(t)(l + ab)z2 which has the solution Z1(t) == constant. This shows that the linear system is not exponentially stable. Therefore, the origin of the nonlinear system is not exponentially stable.

11 85 E'4.~t follows from Exercise 4.58, but an indepenent solution is given next. Let V(x) = tx4. V = _x 6 + x 3 e-t Starting from any time to, we have e-t ~ e-to for all t ~ to. Hence where 0 < f} < 1. t follows from Theorem 4.18 that there is a finite time tl ~ to such that x(t)1 ~ _to)1/3 ( T ' 'V t ~ tl Given 0 < < 1, take to = n(ljf} 3). Then there exists a finite time T such that x(t)1 ~ for all t ~ T. This shows that x(t) converges to zero as t tends to infinity Applying the non-global version of Theorem 4.18 shows that for any x(to) and any input u(t) such that the solution x(t) exists and satisfies x(t)1 ~,B(lx(to), t - to) + 'Y (;~fo lu(t)), 'V t ~ to Since the solution x(t) depends only on U(T) for to ~ T ~ t, the supremum on the right-hand side can be taken over [to, t], which yields (4.47) (a) Asymptotic stability can be shown by linearization which yields the Hurwitz matrix [of jox](o) = -1. Global asymptotic stability can be shown as follows. First we note that there is no finite escape time because /(x)1 ~ kllxll; see Exercise 3.6. We have X2(t) = e-tx2(o). Therefore, there exists a finite time T > 0 such that Consequently X1Xl ~ -(1-,B)x~, 'V t ~ T => Xl(t) -+ 0 as t The linear system X2 = -X2 +u is input-to-state stable. Hence, for any bounded u(t}, X2(t) is bounded. x,(t) = x, (0) +1.' X,(T) [(sin "~(T»)' -1] dr By Gronwall-Bellman inequality Let T be as defined in part (a). XXl ~ -(1 -,B)x~, 'V t ~ T => Xl (t)1 ~ Xl (T), V t ~ T => Xl (t)1 ~ Xl (O)le T, V t ~ 0

Solution of Additional Exercises for Chapter 4

Solution of Additional Exercises for Chapter 4 1 1. (1) Try V (x) = 1 (x 1 + x ). Solution of Additional Exercises for Chapter 4 V (x) = x 1 ( x 1 + x ) x = x 1 x + x 1 x In the neighborhood of the origin, the term (x 1 + x ) dominates. Hence, the

More information

Nonlinear Control. Nonlinear Control Lecture # 3 Stability of Equilibrium Points

Nonlinear Control. Nonlinear Control Lecture # 3 Stability of Equilibrium Points Nonlinear Control Lecture # 3 Stability of Equilibrium Points The Invariance Principle Definitions Let x(t) be a solution of ẋ = f(x) A point p is a positive limit point of x(t) if there is a sequence

More information

Nonlinear Control. Nonlinear Control Lecture # 8 Time Varying and Perturbed Systems

Nonlinear Control. Nonlinear Control Lecture # 8 Time Varying and Perturbed Systems Nonlinear Control Lecture # 8 Time Varying and Perturbed Systems Time-varying Systems ẋ = f(t,x) f(t,x) is piecewise continuous in t and locally Lipschitz in x for all t 0 and all x D, (0 D). The origin

More information

Nonlinear Control. Nonlinear Control Lecture # 2 Stability of Equilibrium Points

Nonlinear Control. Nonlinear Control Lecture # 2 Stability of Equilibrium Points Nonlinear Control Lecture # 2 Stability of Equilibrium Points Basic Concepts ẋ = f(x) f is locally Lipschitz over a domain D R n Suppose x D is an equilibrium point; that is, f( x) = 0 Characterize and

More information

Nonlinear Systems and Control Lecture # 12 Converse Lyapunov Functions & Time Varying Systems. p. 1/1

Nonlinear Systems and Control Lecture # 12 Converse Lyapunov Functions & Time Varying Systems. p. 1/1 Nonlinear Systems and Control Lecture # 12 Converse Lyapunov Functions & Time Varying Systems p. 1/1 p. 2/1 Converse Lyapunov Theorem Exponential Stability Let x = 0 be an exponentially stable equilibrium

More information

Introduction to Nonlinear Control Lecture # 3 Time-Varying and Perturbed Systems

Introduction to Nonlinear Control Lecture # 3 Time-Varying and Perturbed Systems p. 1/5 Introduction to Nonlinear Control Lecture # 3 Time-Varying and Perturbed Systems p. 2/5 Time-varying Systems ẋ = f(t, x) f(t, x) is piecewise continuous in t and locally Lipschitz in x for all t

More information

Nonlinear Control. Nonlinear Control Lecture # 8 Time Varying and Perturbed Systems

Nonlinear Control. Nonlinear Control Lecture # 8 Time Varying and Perturbed Systems Nonlinear Control Lecture # 8 Time Varying and Perturbed Systems Time-varying Systems ẋ = f(t,x) f(t,x) is piecewise continuous in t and locally Lipschitz in x for all t 0 and all x D, (0 D). The origin

More information

Prof. Krstic Nonlinear Systems MAE281A Homework set 1 Linearization & phase portrait

Prof. Krstic Nonlinear Systems MAE281A Homework set 1 Linearization & phase portrait Prof. Krstic Nonlinear Systems MAE28A Homework set Linearization & phase portrait. For each of the following systems, find all equilibrium points and determine the type of each isolated equilibrium. Use

More information

Lyapunov stability ORDINARY DIFFERENTIAL EQUATIONS

Lyapunov stability ORDINARY DIFFERENTIAL EQUATIONS Lyapunov stability ORDINARY DIFFERENTIAL EQUATIONS An ordinary differential equation is a mathematical model of a continuous state continuous time system: X = < n state space f: < n! < n vector field (assigns

More information

MCE/EEC 647/747: Robot Dynamics and Control. Lecture 8: Basic Lyapunov Stability Theory

MCE/EEC 647/747: Robot Dynamics and Control. Lecture 8: Basic Lyapunov Stability Theory MCE/EEC 647/747: Robot Dynamics and Control Lecture 8: Basic Lyapunov Stability Theory Reading: SHV Appendix Mechanical Engineering Hanz Richter, PhD MCE503 p.1/17 Stability in the sense of Lyapunov A

More information

Lecture 4. Chapter 4: Lyapunov Stability. Eugenio Schuster. Mechanical Engineering and Mechanics Lehigh University.

Lecture 4. Chapter 4: Lyapunov Stability. Eugenio Schuster. Mechanical Engineering and Mechanics Lehigh University. Lecture 4 Chapter 4: Lyapunov Stability Eugenio Schuster schuster@lehigh.edu Mechanical Engineering and Mechanics Lehigh University Lecture 4 p. 1/86 Autonomous Systems Consider the autonomous system ẋ

More information

MCE693/793: Analysis and Control of Nonlinear Systems

MCE693/793: Analysis and Control of Nonlinear Systems MCE693/793: Analysis and Control of Nonlinear Systems Lyapunov Stability - I Hanz Richter Mechanical Engineering Department Cleveland State University Definition of Stability - Lyapunov Sense Lyapunov

More information

Converse Lyapunov theorem and Input-to-State Stability

Converse Lyapunov theorem and Input-to-State Stability Converse Lyapunov theorem and Input-to-State Stability April 6, 2014 1 Converse Lyapunov theorem In the previous lecture, we have discussed few examples of nonlinear control systems and stability concepts

More information

Topic # /31 Feedback Control Systems. Analysis of Nonlinear Systems Lyapunov Stability Analysis

Topic # /31 Feedback Control Systems. Analysis of Nonlinear Systems Lyapunov Stability Analysis Topic # 16.30/31 Feedback Control Systems Analysis of Nonlinear Systems Lyapunov Stability Analysis Fall 010 16.30/31 Lyapunov Stability Analysis Very general method to prove (or disprove) stability of

More information

Practice Problems for Final Exam

Practice Problems for Final Exam Math 1280 Spring 2016 Practice Problems for Final Exam Part 2 (Sections 6.6, 6.7, 6.8, and chapter 7) S o l u t i o n s 1. Show that the given system has a nonlinear center at the origin. ẋ = 9y 5y 5,

More information

Stability in the sense of Lyapunov

Stability in the sense of Lyapunov CHAPTER 5 Stability in the sense of Lyapunov Stability is one of the most important properties characterizing a system s qualitative behavior. There are a number of stability concepts used in the study

More information

Modeling and Analysis of Dynamic Systems

Modeling and Analysis of Dynamic Systems Modeling and Analysis of Dynamic Systems Dr. Guillaume Ducard Fall 2017 Institute for Dynamic Systems and Control ETH Zurich, Switzerland G. Ducard c 1 / 57 Outline 1 Lecture 13: Linear System - Stability

More information

Chapter #4 EEE8086-EEE8115. Robust and Adaptive Control Systems

Chapter #4 EEE8086-EEE8115. Robust and Adaptive Control Systems Chapter #4 Robust and Adaptive Control Systems Nonlinear Dynamics.... Linear Combination.... Equilibrium points... 3 3. Linearisation... 5 4. Limit cycles... 3 5. Bifurcations... 4 6. Stability... 6 7.

More information

EN Nonlinear Control and Planning in Robotics Lecture 3: Stability February 4, 2015

EN Nonlinear Control and Planning in Robotics Lecture 3: Stability February 4, 2015 EN530.678 Nonlinear Control and Planning in Robotics Lecture 3: Stability February 4, 2015 Prof: Marin Kobilarov 0.1 Model prerequisites Consider ẋ = f(t, x). We will make the following basic assumptions

More information

Half of Final Exam Name: Practice Problems October 28, 2014

Half of Final Exam Name: Practice Problems October 28, 2014 Math 54. Treibergs Half of Final Exam Name: Practice Problems October 28, 24 Half of the final will be over material since the last midterm exam, such as the practice problems given here. The other half

More information

2 Lyapunov Stability. x(0) x 0 < δ x(t) x 0 < ɛ

2 Lyapunov Stability. x(0) x 0 < δ x(t) x 0 < ɛ 1 2 Lyapunov Stability Whereas I/O stability is concerned with the effect of inputs on outputs, Lyapunov stability deals with unforced systems: ẋ = f(x, t) (1) where x R n, t R +, and f : R n R + R n.

More information

LMI Methods in Optimal and Robust Control

LMI Methods in Optimal and Robust Control LMI Methods in Optimal and Robust Control Matthew M. Peet Arizona State University Lecture 15: Nonlinear Systems and Lyapunov Functions Overview Our next goal is to extend LMI s and optimization to nonlinear

More information

Stability lectures. Stability of Linear Systems. Stability of Linear Systems. Stability of Continuous Systems. EECE 571M/491M, Spring 2008 Lecture 5

Stability lectures. Stability of Linear Systems. Stability of Linear Systems. Stability of Continuous Systems. EECE 571M/491M, Spring 2008 Lecture 5 EECE 571M/491M, Spring 2008 Lecture 5 Stability of Continuous Systems http://courses.ece.ubc.ca/491m moishi@ece.ubc.ca Dr. Meeko Oishi Electrical and Computer Engineering University of British Columbia,

More information

Hybrid Systems - Lecture n. 3 Lyapunov stability

Hybrid Systems - Lecture n. 3 Lyapunov stability OUTLINE Focus: stability of equilibrium point Hybrid Systems - Lecture n. 3 Lyapunov stability Maria Prandini DEI - Politecnico di Milano E-mail: prandini@elet.polimi.it continuous systems decribed by

More information

Lyapunov Stability Analysis: Open Loop

Lyapunov Stability Analysis: Open Loop Copyright F.L. Lewis 008 All rights reserved Updated: hursday, August 8, 008 Lyapunov Stability Analysis: Open Loop We know that the stability of linear time-invariant (LI) dynamical systems can be determined

More information

Hybrid Systems Course Lyapunov stability

Hybrid Systems Course Lyapunov stability Hybrid Systems Course Lyapunov stability OUTLINE Focus: stability of an equilibrium point continuous systems decribed by ordinary differential equations (brief review) hybrid automata OUTLINE Focus: stability

More information

. 2' 22 2xsint. v = xx =- x + --< -2v + 1 l+x2. u= -2u + 1, u(o) = 2. Ix(t)1 = vv(t) $ 2. l~txtxl $ 2I/xIl2I1f(t,x)1I2 $ 2Lllxll~

. 2' 22 2xsint. v = xx =- x + --< -2v + 1 l+x2. u= -2u + 1, u(o) = 2. Ix(t)1 = vv(t) $ 2. l~txtxl $ 2I/xIl2I1f(t,x)1I2 $ 2Lllxll~ 52 CHAPTER 3. o 3.16 Let v = x2 let u(t) be the solution ofthe differential equation. 2' 22 2xsint v = xx =- x + --< -2v + 1 l+x2 u= -2u + 1, u(o) = 2 Then Thus ft 1 + 3e-2t vet) $ u(t) = 2e- 2t + 10 e-

More information

Modeling & Control of Hybrid Systems Chapter 4 Stability

Modeling & Control of Hybrid Systems Chapter 4 Stability Modeling & Control of Hybrid Systems Chapter 4 Stability Overview 1. Switched systems 2. Lyapunov theory for smooth and linear systems 3. Stability for any switching signal 4. Stability for given switching

More information

Classification of Phase Portraits at Equilibria for u (t) = f( u(t))

Classification of Phase Portraits at Equilibria for u (t) = f( u(t)) Classification of Phase Portraits at Equilibria for u t = f ut Transfer of Local Linearized Phase Portrait Transfer of Local Linearized Stability How to Classify Linear Equilibria Justification of the

More information

Math 331 Homework Assignment Chapter 7 Page 1 of 9

Math 331 Homework Assignment Chapter 7 Page 1 of 9 Math Homework Assignment Chapter 7 Page of 9 Instructions: Please make sure to demonstrate every step in your calculations. Return your answers including this homework sheet back to the instructor as a

More information

Lyapunov Stability Theory

Lyapunov Stability Theory Lyapunov Stability Theory Peter Al Hokayem and Eduardo Gallestey March 16, 2015 1 Introduction In this lecture we consider the stability of equilibrium points of autonomous nonlinear systems, both in continuous

More information

Stability of Stochastic Differential Equations

Stability of Stochastic Differential Equations Lyapunov stability theory for ODEs s Stability of Stochastic Differential Equations Part 1: Introduction Department of Mathematics and Statistics University of Strathclyde Glasgow, G1 1XH December 2010

More information

7.1 Linear Systems Stability Consider the Continuous-Time (CT) Linear Time-Invariant (LTI) system

7.1 Linear Systems Stability Consider the Continuous-Time (CT) Linear Time-Invariant (LTI) system 7 Stability 7.1 Linear Systems Stability Consider the Continuous-Time (CT) Linear Time-Invariant (LTI) system ẋ(t) = A x(t), x(0) = x 0, A R n n, x 0 R n. (14) The origin x = 0 is a globally asymptotically

More information

Stability and hybrid synchronization of a time-delay financial hyperchaotic system

Stability and hybrid synchronization of a time-delay financial hyperchaotic system ISSN 76-7659 England UK Journal of Information and Computing Science Vol. No. 5 pp. 89-98 Stability and hybrid synchronization of a time-delay financial hyperchaotic system Lingling Zhang Guoliang Cai

More information

1. Find the solution of the following uncontrolled linear system. 2 α 1 1

1. Find the solution of the following uncontrolled linear system. 2 α 1 1 Appendix B Revision Problems 1. Find the solution of the following uncontrolled linear system 0 1 1 ẋ = x, x(0) =. 2 3 1 Class test, August 1998 2. Given the linear system described by 2 α 1 1 ẋ = x +

More information

Chapter III. Stability of Linear Systems

Chapter III. Stability of Linear Systems 1 Chapter III Stability of Linear Systems 1. Stability and state transition matrix 2. Time-varying (non-autonomous) systems 3. Time-invariant systems 1 STABILITY AND STATE TRANSITION MATRIX 2 In this chapter,

More information

(308 ) EXAMPLES. 1. FIND the quotient and remainder when. II. 1. Find a root of the equation x* = +J Find a root of the equation x 6 = ^ - 1.

(308 ) EXAMPLES. 1. FIND the quotient and remainder when. II. 1. Find a root of the equation x* = +J Find a root of the equation x 6 = ^ - 1. (308 ) EXAMPLES. N 1. FIND the quotient and remainder when is divided by x 4. I. x 5 + 7x* + 3a; 3 + 17a 2 + 10* - 14 2. Expand (a + bx) n in powers of x, and then obtain the first derived function of

More information

Nonlinear Control Lecture 4: Stability Analysis I

Nonlinear Control Lecture 4: Stability Analysis I Nonlinear Control Lecture 4: Stability Analysis I Farzaneh Abdollahi Department of Electrical Engineering Amirkabir University of Technology Fall 2010 Farzaneh Abdollahi Nonlinear Control Lecture 4 1/70

More information

EG4321/EG7040. Nonlinear Control. Dr. Matt Turner

EG4321/EG7040. Nonlinear Control. Dr. Matt Turner EG4321/EG7040 Nonlinear Control Dr. Matt Turner EG4321/EG7040 [An introduction to] Nonlinear Control Dr. Matt Turner EG4321/EG7040 [An introduction to] Nonlinear [System Analysis] and Control Dr. Matt

More information

ẋ = f(x, y), ẏ = g(x, y), (x, y) D, can only have periodic solutions if (f,g) changes sign in D or if (f,g)=0in D.

ẋ = f(x, y), ẏ = g(x, y), (x, y) D, can only have periodic solutions if (f,g) changes sign in D or if (f,g)=0in D. 4 Periodic Solutions We have shown that in the case of an autonomous equation the periodic solutions correspond with closed orbits in phase-space. Autonomous two-dimensional systems with phase-space R

More information

EE363 homework 7 solutions

EE363 homework 7 solutions EE363 Prof. S. Boyd EE363 homework 7 solutions 1. Gain margin for a linear quadratic regulator. Let K be the optimal state feedback gain for the LQR problem with system ẋ = Ax + Bu, state cost matrix Q,

More information

E209A: Analysis and Control of Nonlinear Systems Problem Set 6 Solutions

E209A: Analysis and Control of Nonlinear Systems Problem Set 6 Solutions E9A: Analysis and Control of Nonlinear Systems Problem Set 6 Solutions Michael Vitus Gabe Hoffmann Stanford University Winter 7 Problem 1 The governing equations are: ẋ 1 = x 1 + x 1 x ẋ = x + x 3 Using

More information

Solution of Linear State-space Systems

Solution of Linear State-space Systems Solution of Linear State-space Systems Homogeneous (u=0) LTV systems first Theorem (Peano-Baker series) The unique solution to x(t) = (t, )x 0 where The matrix function is given by is called the state

More information

Nonlinear systems. Lyapunov stability theory. G. Ferrari Trecate

Nonlinear systems. Lyapunov stability theory. G. Ferrari Trecate Nonlinear systems Lyapunov stability theory G. Ferrari Trecate Dipartimento di Ingegneria Industriale e dell Informazione Università degli Studi di Pavia Advanced automation and control Ferrari Trecate

More information

CDS Solutions to the Midterm Exam

CDS Solutions to the Midterm Exam CDS 22 - Solutions to the Midterm Exam Instructor: Danielle C. Tarraf November 6, 27 Problem (a) Recall that the H norm of a transfer function is time-delay invariant. Hence: ( ) Ĝ(s) = s + a = sup /2

More information

1 Lyapunov theory of stability

1 Lyapunov theory of stability M.Kawski, APM 581 Diff Equns Intro to Lyapunov theory. November 15, 29 1 1 Lyapunov theory of stability Introduction. Lyapunov s second (or direct) method provides tools for studying (asymptotic) stability

More information

B5.6 Nonlinear Systems

B5.6 Nonlinear Systems B5.6 Nonlinear Systems 4. Bifurcations Alain Goriely 2018 Mathematical Institute, University of Oxford Table of contents 1. Local bifurcations for vector fields 1.1 The problem 1.2 The extended centre

More information

154 Chapter 9 Hints, Answers, and Solutions The particular trajectories are highlighted in the phase portraits below.

154 Chapter 9 Hints, Answers, and Solutions The particular trajectories are highlighted in the phase portraits below. 54 Chapter 9 Hints, Answers, and Solutions 9. The Phase Plane 9.. 4. The particular trajectories are highlighted in the phase portraits below... 3. 4. 9..5. Shown below is one possibility with x(t) and

More information

Stability of Nonlinear Systems An Introduction

Stability of Nonlinear Systems An Introduction Stability of Nonlinear Systems An Introduction Michael Baldea Department of Chemical Engineering The University of Texas at Austin April 3, 2012 The Concept of Stability Consider the generic nonlinear

More information

Sample Solutions of Assignment 10 for MAT3270B

Sample Solutions of Assignment 10 for MAT3270B Sample Solutions of Assignment 1 for MAT327B 1. For the following ODEs, (a) determine all critical points; (b) find the corresponding linear system near each critical point; (c) find the eigenvalues of

More information

2.10 Saddles, Nodes, Foci and Centers

2.10 Saddles, Nodes, Foci and Centers 2.10 Saddles, Nodes, Foci and Centers In Section 1.5, a linear system (1 where x R 2 was said to have a saddle, node, focus or center at the origin if its phase portrait was linearly equivalent to one

More information

Output Feedback and State Feedback. EL2620 Nonlinear Control. Nonlinear Observers. Nonlinear Controllers. ẋ = f(x,u), y = h(x)

Output Feedback and State Feedback. EL2620 Nonlinear Control. Nonlinear Observers. Nonlinear Controllers. ẋ = f(x,u), y = h(x) Output Feedback and State Feedback EL2620 Nonlinear Control Lecture 10 Exact feedback linearization Input-output linearization Lyapunov-based control design methods ẋ = f(x,u) y = h(x) Output feedback:

More information

One Dimensional Dynamical Systems

One Dimensional Dynamical Systems 16 CHAPTER 2 One Dimensional Dynamical Systems We begin by analyzing some dynamical systems with one-dimensional phase spaces, and in particular their bifurcations. All equations in this Chapter are scalar

More information

Nonlinear Control Lecture 5: Stability Analysis II

Nonlinear Control Lecture 5: Stability Analysis II Nonlinear Control Lecture 5: Stability Analysis II Farzaneh Abdollahi Department of Electrical Engineering Amirkabir University of Technology Fall 2010 Farzaneh Abdollahi Nonlinear Control Lecture 5 1/41

More information

STABILITY. Phase portraits and local stability

STABILITY. Phase portraits and local stability MAS271 Methods for differential equations Dr. R. Jain STABILITY Phase portraits and local stability We are interested in system of ordinary differential equations of the form ẋ = f(x, y), ẏ = g(x, y),

More information

Lecture 8. Chapter 5: Input-Output Stability Chapter 6: Passivity Chapter 14: Passivity-Based Control. Eugenio Schuster.

Lecture 8. Chapter 5: Input-Output Stability Chapter 6: Passivity Chapter 14: Passivity-Based Control. Eugenio Schuster. Lecture 8 Chapter 5: Input-Output Stability Chapter 6: Passivity Chapter 14: Passivity-Based Control Eugenio Schuster schuster@lehigh.edu Mechanical Engineering and Mechanics Lehigh University Lecture

More information

Nonlinear Control Systems

Nonlinear Control Systems Nonlinear Control Systems António Pedro Aguiar pedro@isr.ist.utl.pt 3. Fundamental properties IST-DEEC PhD Course http://users.isr.ist.utl.pt/%7epedro/ncs2012/ 2012 1 Example Consider the system ẋ = f

More information

Dynamical Systems & Lyapunov Stability

Dynamical Systems & Lyapunov Stability Dynamical Systems & Lyapunov Stability Harry G. Kwatny Department of Mechanical Engineering & Mechanics Drexel University Outline Ordinary Differential Equations Existence & uniqueness Continuous dependence

More information

Hello everyone, Best, Josh

Hello everyone, Best, Josh Hello everyone, As promised, the chart mentioned in class about what kind of critical points you get with different types of eigenvalues are included on the following pages (The pages are an ecerpt from

More information

Solutions to Final Exam Sample Problems, Math 246, Spring 2011

Solutions to Final Exam Sample Problems, Math 246, Spring 2011 Solutions to Final Exam Sample Problems, Math 246, Spring 2 () Consider the differential equation dy dt = (9 y2 )y 2 (a) Identify its equilibrium (stationary) points and classify their stability (b) Sketch

More information

Chapter 3. f(x) == [. k 1 =? - == k

Chapter 3. f(x) == [. k 1 =? - == k Chapter 3 3.1 (1) The term Ixl is not continuously differentiable at x == 0, but it is globally Lipschitz. The term x2 is continuously differentiable, but its partial derivative is not globally bounded.

More information

Formula Sheet for Optimal Control

Formula Sheet for Optimal Control Formula Sheet for Optimal Control Division of Optimization and Systems Theory Royal Institute of Technology 144 Stockholm, Sweden 23 December 1, 29 1 Dynamic Programming 11 Discrete Dynamic Programming

More information

8 Periodic Linear Di erential Equations - Floquet Theory

8 Periodic Linear Di erential Equations - Floquet Theory 8 Periodic Linear Di erential Equations - Floquet Theory The general theory of time varying linear di erential equations _x(t) = A(t)x(t) is still amazingly incomplete. Only for certain classes of functions

More information

CHAPTER 2 POLYNOMIALS KEY POINTS

CHAPTER 2 POLYNOMIALS KEY POINTS CHAPTER POLYNOMIALS KEY POINTS 1. Polynomials of degrees 1, and 3 are called linear, quadratic and cubic polynomials respectively.. A quadratic polynomial in x with real coefficient is of the form a x

More information

Boulder School for Condensed Matter and Materials Physics. Laurette Tuckerman PMMH-ESPCI-CNRS

Boulder School for Condensed Matter and Materials Physics. Laurette Tuckerman PMMH-ESPCI-CNRS Boulder School for Condensed Matter and Materials Physics Laurette Tuckerman PMMH-ESPCI-CNRS laurette@pmmh.espci.fr Dynamical Systems: A Basic Primer 1 1 Basic bifurcations 1.1 Fixed points and linear

More information

Chapter 13 Internal (Lyapunov) Stability 13.1 Introduction We have already seen some examples of both stable and unstable systems. The objective of th

Chapter 13 Internal (Lyapunov) Stability 13.1 Introduction We have already seen some examples of both stable and unstable systems. The objective of th Lectures on Dynamic Systems and Control Mohammed Dahleh Munther A. Dahleh George Verghese Department of Electrical Engineering and Computer Science Massachuasetts Institute of Technology 1 1 c Chapter

More information

+ i. cos(t) + 2 sin(t) + c 2.

+ i. cos(t) + 2 sin(t) + c 2. MATH HOMEWORK #7 PART A SOLUTIONS Problem 7.6.. Consider the system x = 5 x. a Express the general solution of the given system of equations in terms of realvalued functions. b Draw a direction field,

More information

(a) Write down the value of q and of r. (2) Write down the equation of the axis of symmetry. (1) (c) Find the value of p. (3) (Total 6 marks)

(a) Write down the value of q and of r. (2) Write down the equation of the axis of symmetry. (1) (c) Find the value of p. (3) (Total 6 marks) 1. Let f(x) = p(x q)(x r). Part of the graph of f is shown below. The graph passes through the points ( 2, 0), (0, 4) and (4, 0). (a) Write down the value of q and of r. (b) Write down the equation of

More information

Handout 2: Invariant Sets and Stability

Handout 2: Invariant Sets and Stability Engineering Tripos Part IIB Nonlinear Systems and Control Module 4F2 1 Invariant Sets Handout 2: Invariant Sets and Stability Consider again the autonomous dynamical system ẋ = f(x), x() = x (1) with state

More information

3 Applications of partial differentiation

3 Applications of partial differentiation Advanced Calculus Chapter 3 Applications of partial differentiation 37 3 Applications of partial differentiation 3.1 Stationary points Higher derivatives Let U R 2 and f : U R. The partial derivatives

More information

Nonlinear Systems Theory

Nonlinear Systems Theory Nonlinear Systems Theory Matthew M. Peet Arizona State University Lecture 2: Nonlinear Systems Theory Overview Our next goal is to extend LMI s and optimization to nonlinear systems analysis. Today we

More information

ON THE AVERAGE NUMBER OF REAL ROOTS OF A RANDOM ALGEBRAIC EQUATION

ON THE AVERAGE NUMBER OF REAL ROOTS OF A RANDOM ALGEBRAIC EQUATION ON THE AVERAGE NUMBER OF REAL ROOTS OF A RANDOM ALGEBRAIC EQUATION M. KAC 1. Introduction. Consider the algebraic equation (1) Xo + X x x + X 2 x 2 + + In-i^" 1 = 0, where the X's are independent random

More information

There is a more global concept that is related to this circle of ideas that we discuss somewhat informally. Namely, a region R R n with a (smooth)

There is a more global concept that is related to this circle of ideas that we discuss somewhat informally. Namely, a region R R n with a (smooth) 82 Introduction Liapunov Functions Besides the Liapunov spectral theorem, there is another basic method of proving stability that is a generalization of the energy method we have seen in the introductory

More information

or - CHAPTER 7 Applications of Integration Section 7.1 Area of a Region Between Two Curves 1. A= ~2[0- (x :2-6x)] dr=-~2(x 2-6x) dr

or - CHAPTER 7 Applications of Integration Section 7.1 Area of a Region Between Two Curves 1. A= ~2[0- (x :2-6x)] dr=-~2(x 2-6x) dr CHAPTER 7 Applications of Integration Section 7.1 Area of a Region Between Two Curves 1. A= ~[0- (x : 6x)] dr=-~(x 6x) dr 6~ 1356 or - 6. A: ~[(x- 1) 3 -(x-1)]dx 11. [~/3 ( - see x) dx 5- - 3 - I 1 3 5

More information

MATH 425, FINAL EXAM SOLUTIONS

MATH 425, FINAL EXAM SOLUTIONS MATH 425, FINAL EXAM SOLUTIONS Each exercise is worth 50 points. Exercise. a The operator L is defined on smooth functions of (x, y by: Is the operator L linear? Prove your answer. L (u := arctan(xy u

More information

LECTURE 16 GAUSS QUADRATURE In general for Newton-Cotes (equispaced interpolation points/ data points/ integration points/ nodes).

LECTURE 16 GAUSS QUADRATURE In general for Newton-Cotes (equispaced interpolation points/ data points/ integration points/ nodes). CE 025 - Lecture 6 LECTURE 6 GAUSS QUADRATURE In general for ewton-cotes (equispaced interpolation points/ data points/ integration points/ nodes). x E x S fx dx hw' o f o + w' f + + w' f + E 84 f 0 f

More information

Georgia Institute of Technology Nonlinear Controls Theory Primer ME 6402

Georgia Institute of Technology Nonlinear Controls Theory Primer ME 6402 Georgia Institute of Technology Nonlinear Controls Theory Primer ME 640 Ajeya Karajgikar April 6, 011 Definition Stability (Lyapunov): The equilibrium state x = 0 is said to be stable if, for any R > 0,

More information

Problem set 7 Math 207A, Fall 2011 Solutions

Problem set 7 Math 207A, Fall 2011 Solutions Problem set 7 Math 207A, Fall 2011 s 1. Classify the equilibrium (x, y) = (0, 0) of the system x t = x, y t = y + x 2. Is the equilibrium hyperbolic? Find an equation for the trajectories in (x, y)- phase

More information

Sturm-Liouville Theory

Sturm-Liouville Theory More on Ryan C. Trinity University Partial Differential Equations April 19, 2012 Recall: A Sturm-Liouville (S-L) problem consists of A Sturm-Liouville equation on an interval: (p(x)y ) + (q(x) + λr(x))y

More information

S(x) Section 1.5 infinite Limits. lim f(x)=-m x --," -3 + Jkx) - x ~

S(x) Section 1.5 infinite Limits. lim f(x)=-m x --, -3 + Jkx) - x ~ 8 Chapter Limits and Their Properties Section.5 infinite Limits -. f(x)- (x-) As x approaches from the left, x - is a small negative number. So, lim f(x) : -m As x approaches from the right, x - is a small

More information

CDS 101 Precourse Phase Plane Analysis and Stability

CDS 101 Precourse Phase Plane Analysis and Stability CDS 101 Precourse Phase Plane Analysis and Stability Melvin Leok Control and Dynamical Systems California Institute of Technology Pasadena, CA, 26 September, 2002. mleok@cds.caltech.edu http://www.cds.caltech.edu/

More information

LB 220 Homework 4 Solutions

LB 220 Homework 4 Solutions LB 220 Homework 4 Solutions Section 11.4, # 40: This problem was solved in class on Feb. 03. Section 11.4, # 42: This problem was also solved in class on Feb. 03. Section 11.4, # 43: Also solved in class

More information

Hybrid Control and Switched Systems. Lecture #11 Stability of switched system: Arbitrary switching

Hybrid Control and Switched Systems. Lecture #11 Stability of switched system: Arbitrary switching Hybrid Control and Switched Systems Lecture #11 Stability of switched system: Arbitrary switching João P. Hespanha University of California at Santa Barbara Stability under arbitrary switching Instability

More information

MAC 1147 Final Exam Review

MAC 1147 Final Exam Review MAC 1147 Final Exam Review nstructions: The final exam will consist of 15 questions plu::; a bonus problem. Some questions will have multiple parts and others will not. Some questions will be multiple

More information

Optimal Control. Quadratic Functions. Single variable quadratic function: Multi-variable quadratic function:

Optimal Control. Quadratic Functions. Single variable quadratic function: Multi-variable quadratic function: Optimal Control Control design based on pole-placement has non unique solutions Best locations for eigenvalues are sometimes difficult to determine Linear Quadratic LQ) Optimal control minimizes a quadratic

More information

ALGEBRAIC GEOMETRY HOMEWORK 3

ALGEBRAIC GEOMETRY HOMEWORK 3 ALGEBRAIC GEOMETRY HOMEWORK 3 (1) Consider the curve Y 2 = X 2 (X + 1). (a) Sketch the curve. (b) Determine the singular point P on C. (c) For all lines through P, determine the intersection multiplicity

More information

First order Partial Differential equations

First order Partial Differential equations First order Partial Differential equations 0.1 Introduction Definition 0.1.1 A Partial Deferential equation is called linear if the dependent variable and all its derivatives have degree one and not multiple

More information

Math 266: Phase Plane Portrait

Math 266: Phase Plane Portrait Math 266: Phase Plane Portrait Long Jin Purdue, Spring 2018 Review: Phase line for an autonomous equation For a single autonomous equation y = f (y) we used a phase line to illustrate the equilibrium solutions

More information

Math 308 Final Exam Practice Problems

Math 308 Final Exam Practice Problems Math 308 Final Exam Practice Problems This review should not be used as your sole source for preparation for the exam You should also re-work all examples given in lecture and all suggested homework problems

More information

High-Gain Observers in Nonlinear Feedback Control

High-Gain Observers in Nonlinear Feedback Control High-Gain Observers in Nonlinear Feedback Control Lecture # 1 Introduction & Stabilization High-Gain ObserversinNonlinear Feedback ControlLecture # 1Introduction & Stabilization p. 1/4 Brief History Linear

More information

Math 216 Final Exam 24 April, 2017

Math 216 Final Exam 24 April, 2017 Math 216 Final Exam 24 April, 2017 This sample exam is provided to serve as one component of your studying for this exam in this course. Please note that it is not guaranteed to cover the material that

More information

3 Stability and Lyapunov Functions

3 Stability and Lyapunov Functions CDS140a Nonlinear Systems: Local Theory 02/01/2011 3 Stability and Lyapunov Functions 3.1 Lyapunov Stability Denition: An equilibrium point x 0 of (1) is stable if for all ɛ > 0, there exists a δ > 0 such

More information

ON THE CAUCHY EQUATION ON SPHERES

ON THE CAUCHY EQUATION ON SPHERES Annales Mathematicae Silesianae 11. Katowice 1997, 89-99 Prace Naukowe Uniwersytetu Śląskiego nr 1665 ON THE CAUCHY EQUATION ON SPHERES ROMAN GER AND JUSTYNA SIKORSKA Abstract. We deal with a conditional

More information

Control of Mobile Robots

Control of Mobile Robots Control of Mobile Robots Regulation and trajectory tracking Prof. Luca Bascetta (luca.bascetta@polimi.it) Politecnico di Milano Dipartimento di Elettronica, Informazione e Bioingegneria Organization and

More information

Redacted for Privacy

Redacted for Privacy AN ABSTRACT OF THE THESIS OF NAMKIAT CHUANKRERKKLTL for the (Name) Electrical and in Electronics Engineering presented on (Major) MASTER OF SCIENCE (Degree) Aulu 5(-- I, Fc? (Date) Title: THE APPLICATION

More information

Math 3301 Homework Set Points ( ) ( ) I ll leave it to you to verify that the eigenvalues and eigenvectors for this matrix are, ( ) ( ) ( ) ( )

Math 3301 Homework Set Points ( ) ( ) I ll leave it to you to verify that the eigenvalues and eigenvectors for this matrix are, ( ) ( ) ( ) ( ) #7. ( pts) I ll leave it to you to verify that the eigenvalues and eigenvectors for this matrix are, λ 5 λ 7 t t ce The general solution is then : 5 7 c c c x( 0) c c 9 9 c+ c c t 5t 7 e + e A sketch of

More information

MATH 32A: MIDTERM 2 REVIEW. sin 2 u du z(t) = sin 2 t + cos 2 2

MATH 32A: MIDTERM 2 REVIEW. sin 2 u du z(t) = sin 2 t + cos 2 2 MATH 3A: MIDTERM REVIEW JOE HUGHES 1. Curvature 1. Consider the curve r(t) = x(t), y(t), z(t), where x(t) = t Find the curvature κ(t). 0 cos(u) sin(u) du y(t) = Solution: The formula for curvature is t

More information

Nonlinear Control Lecture 7: Passivity

Nonlinear Control Lecture 7: Passivity Nonlinear Control Lecture 7: Passivity Farzaneh Abdollahi Department of Electrical Engineering Amirkabir University of Technology Fall 2011 Farzaneh Abdollahi Nonlinear Control Lecture 7 1/26 Passivity

More information

3. Fundamentals of Lyapunov Theory

3. Fundamentals of Lyapunov Theory Applied Nonlinear Control Nguyen an ien -.. Fundamentals of Lyapunov heory he objective of this chapter is to present Lyapunov stability theorem and illustrate its use in the analysis and the design of

More information