where u(t) and y(t) are the input and output, re-

Size: px
Start display at page:

Download "where u(t) and y(t) are the input and output, re-"

Transcription

1 Proceedings of the 35th FMil 2:lO Conference on Decision and Control Kobe, Japan December 1996 Robustness of Discrete Periodically Time Varying Control Under Different Model Perturbations * Jingxin Zhang Cishen Zhang* School of Electrical Engineering, University of South Australia, Whyalla Norrie, SA 5608 Cooperative Research Centre for Sensor Signal and Information Processing, Technology Park Adelaide, Australia Fax: $ j.zhang@unisa.edu.au Department of Electrical and Electronic Engineering, University of Melbourne, Parkville, Vic. 3052, Australia Abstract: This paper presents a quantitative analysis on the robustness of discrete linear periodically time varying (LPTV) control under different perturbations in comparison with linear time invariant control. For unstructured perturbations, it is shown that the system stability margin is definitely deteriorated by LPTV control. For sturctured perturbations, the paper clarifies the mechanism of LPTV control in stability margin improvement and the side effect of this improvement - deterioration of the stability margin for unstructured perturbations. In a unified frequency domain framework, the paper exposes the relevance and conflictions of the previous results on the robustness of LPTV control, and therefore provides a deeper insight into the problem. 1. Introduction Robustness enhancement is the primary motivation for the investigation into linear periodically time varying (LPTV) control of linear time invariant (LTI) plants. It has been shown by many authors that LPTV control can improve significantly gainlphase margin and can provide strong and simultaneous stabilization. However, it has also been shown that nonlinear time varying (NLTV) control and linear time varying (LTV) control, which include LPTV control as a special case, offer no advantages over LTI control for robust stabilization of LTI plants subject to the norm bounded unstructured model perturbations, and that LPTV control systems may be sensitive to the high frequency band unstructured perturbations. For details of the above results, see e.g. [4, 10, 1, 7, 8, 9, 6, 111 and the references therein. These different results appear to be uncorrelated and conflict to certain extent, and the relevance and tradeoffs between the different results and cases are not clear. It is therefore necessary and important to gain further understanding of the intrinsic properties of LPTV control systems and the system robustness. In [12], the authors have analyzed the closed loop stability margin of discrete LPTV control system subject to NLTV unstructured model perturbations, and have shown that for this specific case, LPTV control deteriorates the stability margin. This result provides a deeper understanding for LPTV control. However, NLTV perturbation is a very large family, it contains many different practically important subsets, e.g. LPTV and LTI perturbations. It is known that for different perturbations, the robust stability conditions can be quite different. Thus [la] has not given a complete answer to the robustness of discrete LPTV control. Furthermore, [12] shows only the negative part of LPTV control. It gives no explanation on how can LPTV control improve closed loop robustness for some other classes of perturbations, e.g. gain variations, and what are the relationships among the different cases. This paper looks further into the problem. It investigates, respectively, the robustness of LPTV control system under LTI and a class of LPTV unstructured perturbations and structured real perturbations. It is shown that for unstructured perturbations, LPTV control definitely deteriorates the closed loop system stability margin. The paper also clarifies the mechanism of LPTV control in gain margin improvement and the side effect of this improvement - deterioration of the system robustness for unstructured perturbations. All the analyses are carried out in a unified frequency domain framework. The results exposes the relevance and the relationship of the previous results on this issue. Due to space limit, the proofs for all the lemmas and corollary in the sequel will be omitted. 2 Problem statement Throughout the paper, II.II denotes the Lz norm and 12 norm on continuous and discrete signals; 11. 1, denotes the co-norm of a discrete system, or the H, norm if the system is stable; *(.) and p(.) denote the maxi- mum singular value and the spectral radius of a matrix, respectively; I. 1 denotes the magnitude of a complex variable; dim(.) denotes the dimension of a square matrix; X* denotes the complex conjugate of a variable X; 72. and C are the fields of real and complex numbers, respectively. In time domain, suppose that G is a causal, N- periodically time varying system, then it admits the following minimum state space representation *Work supported by Australian Research Council and Research Development Grant of University of South Australia /96 $ IEEE 3984 where u(t) and y(t) are the input and output, re-

2 spectively, r(t) is the n-dimensional state vector, and A(t), B(t), C(t) and D(t) are the N-periodically time varying matrices with appropriate dimensions and satisfyinga(t+in) = A(t), B(t+lN) = B(t), C(t+lN) = C(t), D(t + 1N) = D(t). Note that if N = 1, G reduces to an LIT system. Throughout the paper, this case is distinguished from the cases N # 1, i.e. an LPTV sys- tem is defined as not LTI. The system G in the form of (l), is a finite order system if n < 00. The system G is a real system if A(t), B(t), C(t) and D(t) are real matrices. The system G zs a stable system if Xi, i = 1,..., n, the eigenvalues of A := A(N - 1)A(N - 2).A(O), satisfy IXil<l, i=l,..., n (2) Denote Y(t) and F(z) the t-transforms of a discrete signal y(t) and an LTI discrete system F, respectively. F(z) zs defined as finite order if its pole polynomial 2s finite order. Where the pole polynomial is defined as the polynomial containing all the modes of F which is not necessarily minimum order. Write explicitly z = e'". The frequency responses of y(t) is defined as Y(ej"). The frequency transfer functzon of F zs defined as F(ej"'). Then Y(ej") and F(ej") are continuous functions in w E EO,%). The problems to be considered in the paper are the stability margin of 3 under different perturbations given in Al-A3, namely, the maximum tolerable r for which the system F controlled by LPTV Ii remains stable, and the comparison of the stability margin attainable by LPTV Ii with that attainable by LTI I<. For simplicity, only multiplicative perturbation case is considered. However, all the analyses in the sequel carry over to additive perturbation case. To make the analysis meaningful, the LPTV control and the resulting closed loop system are distinguished from the LTI control and the resulting closed loop system. It is defined that an LPTV system is not LTI. 3 Frequency domain lifting for systems For a discrete signal y(t), the norm of y(t) is llyll = d m. Let Y(ej") be the frequency reof Y(ej") is llyll = WN = Q. Then... Y(ej("+(N-l)"N) 11 is defined as the lifted frequency response of the signal w E [O,WN) Apparently, the norm is preserved under the lifting in frequency domain, i.e. IbII = IlYll = 1 1 ~ 1 1. Consider a discrete LPTV system G in the form of (1). Let ri(ej") and Y(ej") be the lifted frequency responses of the input U and output y, respectively. It has been shown in [13] that as i.(ejw) Fig. 1 LPTV feedback control system F Fig. 1 gives the feedback control system, denoted F, to be consider in the paper. It is assumed that all the blocks of F are SISO discrete systems. In the figure, P denotes a real, causal, finite order and stabilizable LTI nominal plant, K is a real, causal and finite order LPTV controller with period N, the dashed-line enclosed subsystem S is the nominal closed loop system resulting from the interconnection of P, I< and weighting function W, and A is a multiplicative perturbation to P. The following different cases of A will be considered. Al. A is an LPTV, causal, possibly unstable operator with period N, llal)m 5 r. A2. A is an LTI, causal, possibly unstable operator, llalloo 5 r, and P + AWP possesses the same number of unstable poles as P. A3. A = 6, ER, 0 5 b 5 r. In Al-A3, r E R, 0 5 r < 03. W in AI and A2 is a stable LTI weighting function with stable inverse, and in A3 W = 1. The As in A1 and A2 represent two different classes of unstructured perturbations. While A in A3 represents a class of structured uncertainties - gain variations. where G(ej") is defined on w E [ 0,w~) and is in the following form G(ejw) = [Gk(e3(w+'"N))]k,~=~,l,..,,~-l = G(z) = [ G~(z~~'"~)]~,I=o,I,_.., N-1 (3) G(ej") or G(z) as given above is defined as the lifted frequency transfer function of the LPTV system G, which transfers the lifted input U(ej") to the lifted output?(elw). Lemma 3.1: Suppose that G is a real, causal, n-th order LPTV system in the form of (1) and G(z) in the form of (3) is the lifted transfer function of G. Then a) G(t) is a proper, finite order transfer function matrix an z with an N x (n x N)-th order pole polynomial D(rN). b) The zeros of D(zN) are given by XiejlWN, i=1,2,..., n,1=0,1,...) N-1. cj G is stable zf and only if all the zeros of D(zN) belong to the open unit disk. d) If G is stable, then llgllm = llgllm. Remark 3.1: Lemma 3.3 is in fact the theoretical basis of the paper. It reveals an important fact that G(t) 3985

3 carries the same stability information of G as its time domain counterpart (l), and G(z) is a proper, finite order transfer function matrix of z with finite number of poles. Thus the frequency domain techniques for LTI MIMO system analysis can be readily applied to G(z). Actually, this is the basic thought of the paper. Lemma 3.2: Suppose that G is a real, causal, and finite order LPTV system with the lifted transfer function G(z) in the form of (3). Then Go(.) on the diagonal of (3) is a real-rational function of z and it gives rise to a real, causal and finite order LTI system Go with Go(%) as its transfer function. Moreover, Go is a stable system if G is a stable system. Lemma 3.3: A system F is LTI if and only if the lifted frequency transfer function F(ejw) has a diagonal structure written as P(ejw) = c ~iag[~o(ej(~+~~~))], i = 0,1,..., N-1. 4 Robust stability conditions of closed loop LPTV systems Consider the nominal closed loop subsystem S in Fig. 1. It is assumed that S is internally stabilized by IC. Apparently, S is LPTV if I< is LPTV. Denote S(&'), i)(ejw), r/z.(ejw), k(ej"), and A(ej") the lifted transfer function matrices of S, P, W, I< and A, respectively. Then F can be represented equivalently by an LTI MIMO system with a nominal closed loop,$(ejw> = r/ir(ej")p(ej")li.(ejw)[i - p(ejw)li.(ejw)]-' and a perturbation block A(.&"). According to Lemmas and the assumptions on P, W, K and A, S(ejw), P(ej"), r/z.(ej"),.k(ej"), and A(ejw) are all N x N dimensional, proper, finite order transfer function matrices, and S(ej") is in the form of (3) with So(ej(w) = diag[so(ej(w+'"n))],=o,~,...,~-l on the diagonal and some nonzero Sk(ej("+lWN)), k = l,..., N - 1, 1 = 0,1,..., N - 1 on the off-diagonals. Hence, the frequency domain techniques for LTI MIMO system analysis can be readily applied to the equivalent system. Lemma 4.1: Let I< be LPTV. Suppose that A satisfies A1 and that p(ej") + A(ej")r/ir(ej")P(ej") possesses the same number of unstable poles as P(ej"). Then the closed loop system 3 is stable if and only if llsll, < 1/r. Lemma 4.2: Let Ir' be LPTV. Suppose that A satisfies A2. Then the closed loop system F is stable if and only if supwe[o,wn) p[s(ejw)] < 1/r, where p[s(ej")] is the structured singular value of S(ej") [3]. Lemma 4.3: Let K be LPTV. Denote yi(w), i = 1,2,..., N, the N eigenvalues of S(ejw) and &(U) the phase of 7i(w). Suppose that A satisfies A3. Then the closed loop system 3 is stable if and only if for w E [0,w~) and i = 1,2,..., N, IYi(0)l # 1/r, h(w) = (4) 5 Stability margin for different perturbations Theorem 5.1: Given a real, causal, finite order, LPTV controller I< which internally stabilizes the closed loop 3986 system S, a real, causal, finite order LTI controller KO can always be constructed such that when applied to the plant P, KO yields a stable LTI closed loop system So and the lifted transfer function of So is just So(ej"), the diagonal of S(ejw). For the proof of the theorem and the details of construc- tion of KO, readers are referred to [13]. From Lemmas 4.1 to 4.3 it is obvious that the stability margin maximization problem for case A1 amounts to the H,-optimization problem of finding a IC which minimizes llsll, = 11S11,; for case A2 it amounts to the p-optimization problem of finding a K which minimizes p(s); while for case A3 it amounts to the characteristic locus shaping problem of finding a IC which shapes the characteristic loci of S so as to maximize r for which the condition (4) holds. The rest of this section will analyze 11S11, p(s) and the characteristic loci of S attainable by the LPTV controller K in comparison with those attainable by the LTI controller KO and the optimal LTI controller I<:. In the following, it is assumed that I<,+ is an optimal LTI controller that yields the nominal LTI closed loop system Sg and the maximumstability margin attainable by LTI controllers. Following the same convention, the lifted frequency transfer function of S,* is denoted as S,+(ej"). Note that for different cases of perturbations, IC: may be different, and that IC: does not necessarily belong to the set KO which, as shown in Theorem 5.1, is constructed from a given LPTV IC set. Accordingly, Sg is not necessarily given by the diagonal of S, the lifted transfer function of an LPTV S. Theorem 5.2: The H, norm of the LPTV system S satisfies IISII, > IISgllm. Before embarking on the proof of the theorem, two lemmas required in the proof are introduced first. Lemma 5.1: The H, norm o the LPTV s stem s satisfies IlSllm L d----k-+ s~p,e[o,2?r)ck=o S,(ej") 2 I IS0 (ei 1 I loo Lemma 5.2: Subject to the assumptions on the nominal plant P, there exists an optimal LTI controller IC: such that the nominal closed loop S$(ej") resulting from IC,+ is all-pass, i.e. IS,+(ejw)l = a G cont, Vw. Proof of Theorem 5.2: Suppose So # S:. It follows from Lemma 5.1 and the optimality of 5': that llslloo 2 IlS0lloo > IISGllm. Conversely, suppose So = Sg. Since S is LPTV, there must be k # 0 and w E [0,2s] such that Sk(eJw) # 0. It then follows from Lemma 5.1 and N--l 2 jw 5.2 that IISIIL 2 SuP,E[0,27r) Ck=O = N-1 2 jw CY2 + SUPwE[0,zrr)Ck=1 &(e > CY2 = 11%112 This proves the theorem. 0 Theorem 5.3: For the LPTV system S with period N 5 3, and for the LPTV system S having period N > 3 and possessing a scaling matrix F(w) which gives ~[F(w)S(ej~)F-'(w)l = p[s(ejw)l, w E [o,wn) (5) the following holds: "P[O,WN) p[s('jw)1 > supio,wn) p[sg

4 Proof: In [3] it is shown that for a square complex matrix M associated with a block diagonal matrix A from which p(m) is defined, p(m) 5 inffa(fmf-'), and the equality always holds if the number of the blocks of A is less than or equal to 3. Where F is a block diagonal scaling matrix with the same number of blocks as that of A. In the special case considered in the theorem, A and hence F are diagonal. Thus the equality holds for dim(a) = N 5 3 and some S with N > 3 and satisfying (5). Suppose F(w) is a scaling matrix which gives the equality (5). According to [3] F(w) = diag[fk(w)], fk(w) E 72, fk(w) >0,.k = 0,1,..., N - 1, w E [0, ON). Then SUP[^,^,) p[s(ejw)] can be written as where S(ejw) := F(w)S(ej")F-'(w) = (ej(w+'wn))}k 1=o,1,..., N- 1, 3 k (e.f(w+lwn) = %sk(ej(w+iwn)!i 1 From the last equations and the structure of S(ej"> it can be observed that S[ej") has the same structure as S(ejw) and contains So(ej") as its diagonal. Since So(eJw) is diagonal, sup p[so(eiw)] = sup S[SO(S")] [OWN) [OWN) = IISo(.iW)IIm = 11soIIw (7) Thus following the same line as that in the proof of Theorem 5.2, it can be readily shown that llsllm > llsg[lm. The theorem then follows from (6) and (7). 0 Corollary 5.1: Suppose that the LPTV system S satisfies the condiiions of Theorem 5.2 and Theorem 5.3. Then llsllm > llsollm and su~~o,~~)~[s(ej")l > s'p[o,wn) p[ S 0 (ej")] if 3k, k # 0, such that Sk(z) does not possess a zero at ejw-. Where wm is the w at which So(ej") takes its Ha norm. Remark 5.1: Theorem 5.2 and Theorem 5.3 reveal an important intrinsic property of LPTV control - for unstructured perturbations, LPTV control can neither improve stability margin nor attain the same level of stability margin as LTI control, instead, it deteriorates stability margin. The cause of this deterioration is the presence of the nonzero off-diagonals of S arising from the LPTV dynamics of IC. Corollary 5.1 further shows that if the channels arising from LPTV dynamics do not all possess a zero at e'"-, the stability margin of LPTV closed loop system S is simply poor than that of the LTI closed loop system So given by the diagonal of 3. A demonstrative example is given in section 6. Note that the condition N 5 3 in Theorem 5.3 is not restrictive. It has been shown in [7] that N = 2 is sufficient for the stabilization of LTI plants subject to structured perturbations. The theorem is in fact valid for the N suggested (implicitly) in the previous literature Now consider cases A.3. Let &i, i = 1,2,3, be the stability margin for cases A1 - A3, respectively, i.e. R,i = the maximum r in case Ai, i = 1,2,3, for which 3 remains stable. Further, let &i(kz) and Rmi(K) be the stability margins attained by K; and the maximum stability margins attainable by the LPTV K set, respectively. Define r,i := the maximum r for which yj(w) satisfies condition (4). Theorem 5.4: a) R,,,3(K) > &3(KO+) provided P is biproper. b) Rm3(I() = minlsig rmi. c) a) and b) are achieved only if S(ejw) possesses nonzero off-diagonals resulting from the periodically tame varying dynamics of LPTV Ii. d) Provided that S(ejw) satisfies the conditions of Theorem 5.2 and 5.3, Rm3(K) > Rm3(K;) impltes Rm1(K) < Rml(K;) and & 2(K) < &2(K;). Proof: a) This is the well known result of [7]. b) Directly from condition (4) and the definition of Rm3(K). c) Suppose $(ejw) does not have nonzero off-diagonals, S(ejw) reduces to a diagonal matrix which, as shown in Theorem 5.1, corresponds to an LTI closed loop system resulting from an LTI controller Iih. Denote &a(ka) the stability margin given by this K;. From the optimality of Kz, &3(KA) 5 Rm3(Kz). This proves c). d) From c), if a) holds, S(eJw) must have nonzero offdiagonals. d) then follows from Theorem 5.2 and Theorem Remark 5.2: Theorem 5.4 reveals how can LPTV control improve gain margin - shaping n(w) loci with nonzero off-diagonals. In case S is LTI, yi(w) loci are determined solely by the diagonals of S, which are the frequency responses of an LTI nominal closed loop system at different frequency bands. It is known that for LTI controllers, if P is nonminimum phase, gain margin is always limited [7]. Notice that the gain margin defined in [7] equals &3 - l. This means that with only diagonals, 7i(ejw) is confined to certain region which gives the limited Rm3. Whereas, if S is LPTV, S has nonzero off-diagonals. These off-diagonals provide extra freedom for further tuning of yi(ej") so that a better shape of 7i(ej") which gives larger &3 can be obtained. This is the mechanism of LPTV K in gain margin improvement. The example in next section will demonstrate this graphically. Apparently, any benefit that LPTV IC can bring is from tuning the magnitudes and/or phases of yi(ej") with nonzero off-diagonals. The nonzore off-diagonals are essentially indispensable for this tuning. However, as shown in the theorem, these nonzero off-diagonals definitely deteriorate the stability margin for unstructured perturbations. Hence the LPTV Ii' designed for gain margin maximization can be very sensitive to other classes of perturbations. The example in next section will show how sensitive it could be.

5 6 Example It can be readily shown using bilinear transform and the Consider the LTI plant P(z) = k ~ This is ~ an ex- ~ well known ~ procedure ~ ~ given in.[5] that the optimal conample studied by many authors, e.g. [7, 21. It is shown troller I<$ for the plant is I{$ = $& and the resulting in [7] that with LTI controller R-3 = 1.25 (R-3 = gain all-pass LTI closed loop system is S: = -2.5,-, Bz-f margin -1, where the gain margin is as defined in [7]). with ls811m = lls;,.llw = p[s,*] = 14db. Thus Whereas in [2] it is shown that with the LPTV con- troller K(q-') = l+(-l)'+(6+6(-l)t)q-1, the closed loop system is stable for IC < -5 and k > 4. Note that for the given I<, N = 2, WN = 7r, ej'"n = (-1)'. Take W = 1 (i@(z) = I> and assume k = ko, a known nominal value. The lifted transfer function of the nominal closed loop system S can be calculated as S( z) = P(,)I? (2)[I-P( z )I? (z)]- 1 = [ $?) )I : :?: Sl(2) = ko(1-2~-')(1+ 3.~-~)(1-6z-l) 1 + 2k0-9r-2 Following the line of [13], the LTI controller I?o(r) as described in Theorem 5.1 can be calculated as It can be easily checked that when applied to the nominal plant P(z), I<o(z) gives the closed loop system So(z). This verifies the result of Theorem 5.1. Since S1(z) does not have zero on unit disk, from Corollary 5.1 it is known that llsll > lls0ll and ' suplde[o,wn) p[s(ejw 11 > supcde[o,wn) piso Because N = 2, according to [3], (5) always holds and p[$ can be calculated precisely (e.g. using MATLAB p-toolbox). Hence IIS(ej")llm = 6[S(ejw)] and p[s(ej")] can be evaluated from the peak values of e[s(ej")] and p[s(ejw)] plots, and can be compared with ISo(ej")l = 5[S?(ej,")] = p[so(ej")] which is given by the diagonals of S(eJW). All the plots given are plotted for ko = -6 and w E [0,7r) since WN = r. Fig. 2 gives the 5[S(ej")], p[s(ejw)] and 5[S0(ejw)] plots. From the peak values of the three plots, it can be seen clearly that lls(ejw)llm = s~p,~[~-,,~),p[s(ej")] = 48db > IISo(ej")llw = sup,e[o,wn) p[so(ej")] M 43db. This coincides with the analysis of Corollary 5.1. Fig. 3 gives the plots for n (w), the minimumeigenvalue of S(ej"). It can be observed that Iyl(w)l < -250db and ld1(w)l 5 7r. Because I-yl(w)I is virtually zero, r-1 = 00. Fig. 4 gives the plots for yz(w), the maximum eigenvalue of S(ej"). As shown in the figure, -5db < yz(w) 5 16db and 1~#2(w)l 5 ~/2. Since &?(U) is always smaller than T, r-2 = 03. Thus, for -cm < ko 5-6 the closed loop system is always stable, i.e. Rm3 = m(azl<i<2~~i = gain margin -1 = 00. The results coincide with the analysis of Theorem 5.4 and explain how the gain margin is improved llsll00 > IlS,'llm, SUPW [0,2?r) > SUPWE[0,27r) P[S;l. This coincides with the analyses of Theorem 5.2 and Theorem 5.3. It is obvious that although the LPTV control K provides a very significant gain margin improvement, the resultant IIS(eJ")llm and p[s(ej")] are very large. Hence it is very sensitive to the unstructured perturbations. When ko = -6, a perturbation A of form AI or A2 with r > will destabilize the system, while a destabilizing A for the optimal LTI I(: must have r > 5, which is 1250 times of that for the LPTV K. Similar results have also been observed in the computation for ko = 5, which show that though the shapes of the plots are different, the conclusions of Theorem 5.2, Theorem 5.3 and Corollary 5.1 are still true. Conclusions The necessary and sufficient conditions on the robust stability of LPTV control systems have been presented in frequency domain for the different classes of perturbations. These conditions are the extension of the LTI system robust stability conditions to LPTV systems and can be further extended to the analysis and design of general LPTV systems with LPTV plants and controllers. The three classes of model perturbations considered in the paper are all the theoretically and practically important ones, and were most often analyzed separately by different techniques in the previous literature - resulting in somewhat uncorrelated and conflict results. The quantitative analysis and computational results have shown that for unstructured perturbations, LPTV control definitely deteriorates the system stability margin. The condition (4) have provided a frequency domain insight into the mechanism of LPTV control in gain margin improvement and have enable us to revealed the consequence of this improvement - deterioration of the stability margin for unstructured perturbations. References &I Chapellat, H. and M. Dahleh, (1992), Analysis of time varying control strategies for optimal disturbance rejection and robustness, IEEE Trans. on Automatzc Control, Vol. AC-37, pp Das, S. K. and Rajagopalan, P. K., (1992), Periodic discrete-time systems: stability analysis and robust control using zero placement, IEEE Trans. on Automatic Control, Vol. AC- 37, No. 3, pp

6 [3] Doyle, J., (1982), Analysis of feedback systems with structured uncertainties, IEE Proc Pt D, Control Theory and Applications, Vol. 129, No. [ll] Zhang, J. and C. Zhang, (1994), Robustness analysis of control systems using generalized sample hold functions, Proc. 33th IEEE CDC, Florida, 6, pp , USA., Vol. 1, pp [4] Er, M. J. and B. D. 0. Anderson and W. Yan, (1994), Gain margin improvement using generalized sample-data hold function based multirate output compensator, Automatica, Vol. 30, No. 4, pp [SI Francis, B. A. (1987), A course in H, control theory, Vol. 88 in Lecture Notes in Control and Information Sciences, Springer-Verlag, New York. [6] Goodwin, G.C. and A. Feuer, (1992), Linear periodic control: A frequency domain viewpoint, Systems and Control Letters, Vol. 19, pp [7] Khargonekar, P.P., K. Poolla, and A. Tannenbaum, (1985), Robust control of linear time invariant plants using periodic compensation, IEEE Trans. on Automatic Control, Vol. AC-30, pp [8] Poolla, K. and T. Ting, (1987), Nonlinear time varying controllers for robust stabilization, IEEE Trans. on Automatic Control, Vol. AC-32, pp [12] Zhang, J. and C. Zhang, (1995), Stability margin analysis of discrete periodically time varying controllers, Proc. 34th IEEE CDC, New Orleans, USA, pp [13] Zhang, C. and J. Zhang, (1996), Performance analysis of periodically time varying controllers, Preprints of 13th IFAC Congress, San Francisco, USA, Vol. D, pp % 47 l Or E &al.- E Frequency (rad'sec) Multi pertub, plant gain k=-6 [9] Shamma, J.S. and M.A. Dahleh, (1991), Time varying versus time invariant compensation for rejection of persistent bounded disturbances and robust stabilization, IEEE Trans. on Automatic Control, Vol. AC-36, pp [lo] Yang, C. and P. T. Karbamba, (1994), Multichannel output gain margin improvement using generalized sampled-data hold functions, IEEE Trans. on Awtomatic Control, Vol. AC-39, pp z (D z cn II 8 ;" :..... A.. _.( ; ;.. Fig ' I io-2 lo-' loo 10' Frequency (radkec) Magnitude and phase plots of n(w) -10' 1 o-2 lo-' loo 10' Frequency (radlsec) Multi Derlub. olant oain k=-6 Fig. 2 8[S(ejw)], p[s(ej'")], and 5[&(ejw)] plots -1 00' I 1 o loo 10' Frequency (radsec) -: ~[S(ejw)], 000: p[s(eju)],..,: ii[so(eju)~ Fig. 4 Magnitude and phase plots of -yz(w) 3989

Robustness of Discrete Periodically Time-Varying Control under LTI Unstructured Perturbations

Robustness of Discrete Periodically Time-Varying Control under LTI Unstructured Perturbations 1370 IEEE TRANSACTIONS ON AUTOMATIC CONTROL, VOL. 45, NO. 7, JULY 000 Robustness of Discrete Periodically Time-Varying Control under LTI Unstructured Perturbations Jingxin Zhang and Cishen Zhang Abstract

More information

Zeros and zero dynamics

Zeros and zero dynamics CHAPTER 4 Zeros and zero dynamics 41 Zero dynamics for SISO systems Consider a linear system defined by a strictly proper scalar transfer function that does not have any common zero and pole: g(s) =α p(s)

More information

MIMO analysis: loop-at-a-time

MIMO analysis: loop-at-a-time MIMO robustness MIMO analysis: loop-at-a-time y 1 y 2 P (s) + + K 2 (s) r 1 r 2 K 1 (s) Plant: P (s) = 1 s 2 + α 2 s α 2 α(s + 1) α(s + 1) s α 2. (take α = 10 in the following numerical analysis) Controller:

More information

ThM06-2. Coprime Factor Based Closed-Loop Model Validation Applied to a Flexible Structure

ThM06-2. Coprime Factor Based Closed-Loop Model Validation Applied to a Flexible Structure Proceedings of the 42nd IEEE Conference on Decision and Control Maui, Hawaii USA, December 2003 ThM06-2 Coprime Factor Based Closed-Loop Model Validation Applied to a Flexible Structure Marianne Crowder

More information

Introduction. Performance and Robustness (Chapter 1) Advanced Control Systems Spring / 31

Introduction. Performance and Robustness (Chapter 1) Advanced Control Systems Spring / 31 Introduction Classical Control Robust Control u(t) y(t) G u(t) G + y(t) G : nominal model G = G + : plant uncertainty Uncertainty sources : Structured : parametric uncertainty, multimodel uncertainty Unstructured

More information

Design Methods for Control Systems

Design Methods for Control Systems Design Methods for Control Systems Maarten Steinbuch TU/e Gjerrit Meinsma UT Dutch Institute of Systems and Control Winter term 2002-2003 Schedule November 25 MSt December 2 MSt Homework # 1 December 9

More information

and Mixed / Control of Dual-Actuator Hard Disk Drive via LMIs

and Mixed / Control of Dual-Actuator Hard Disk Drive via LMIs and Mixed / Control of Dual-Actuator Hard Disk Drive via LMIs Nasser Mohamad Zadeh Electrical Engineering Department Tarbiat Modares University Tehran, Iran mohamadzadeh@ieee.org Ramin Amirifar Electrical

More information

Stability Margin Based Design of Multivariable Controllers

Stability Margin Based Design of Multivariable Controllers Stability Margin Based Design of Multivariable Controllers Iván D. Díaz-Rodríguez Sangjin Han Shankar P. Bhattacharyya Dept. of Electrical and Computer Engineering Texas A&M University College Station,

More information

MTNS 06, Kyoto (July, 2006) Shinji Hara The University of Tokyo, Japan

MTNS 06, Kyoto (July, 2006) Shinji Hara The University of Tokyo, Japan MTNS 06, Kyoto (July, 2006) Shinji Hara The University of Tokyo, Japan Outline Motivation & Background: H2 Tracking Performance Limits: new paradigm Explicit analytical solutions with examples H2 Regulation

More information

Optimal triangular approximation for linear stable multivariable systems

Optimal triangular approximation for linear stable multivariable systems Proceedings of the 007 American Control Conference Marriott Marquis Hotel at Times Square New York City, USA, July -3, 007 Optimal triangular approximation for linear stable multivariable systems Diego

More information

Robust fixed-order H Controller Design for Spectral Models by Convex Optimization

Robust fixed-order H Controller Design for Spectral Models by Convex Optimization Robust fixed-order H Controller Design for Spectral Models by Convex Optimization Alireza Karimi, Gorka Galdos and Roland Longchamp Abstract A new approach for robust fixed-order H controller design by

More information

Network Reconstruction from Intrinsic Noise: Non-Minimum-Phase Systems

Network Reconstruction from Intrinsic Noise: Non-Minimum-Phase Systems Preprints of the 19th World Congress he International Federation of Automatic Control Network Reconstruction from Intrinsic Noise: Non-Minimum-Phase Systems David Hayden, Ye Yuan Jorge Goncalves Department

More information

Lecture 6. Chapter 8: Robust Stability and Performance Analysis for MIMO Systems. Eugenio Schuster.

Lecture 6. Chapter 8: Robust Stability and Performance Analysis for MIMO Systems. Eugenio Schuster. Lecture 6 Chapter 8: Robust Stability and Performance Analysis for MIMO Systems Eugenio Schuster schuster@lehigh.edu Mechanical Engineering and Mechanics Lehigh University Lecture 6 p. 1/73 6.1 General

More information

Chapter Stability Robustness Introduction Last chapter showed how the Nyquist stability criterion provides conditions for the stability robustness of

Chapter Stability Robustness Introduction Last chapter showed how the Nyquist stability criterion provides conditions for the stability robustness of Lectures on Dynamic Systems and Control Mohammed Dahleh Munther A Dahleh George Verghese Department of Electrical Engineering and Computer Science Massachuasetts Institute of Technology c Chapter Stability

More information

Chapter Robust Performance and Introduction to the Structured Singular Value Function Introduction As discussed in Lecture 0, a process is better desc

Chapter Robust Performance and Introduction to the Structured Singular Value Function Introduction As discussed in Lecture 0, a process is better desc Lectures on Dynamic Systems and Control Mohammed Dahleh Munther A Dahleh George Verghese Department of Electrical Engineering and Computer Science Massachuasetts Institute of Technology c Chapter Robust

More information

Title unstable additive/multiplicative pe. works must be obtained from the IEE

Title unstable additive/multiplicative pe.   works must be obtained from the IEE Title Robust stability of sampled-data sy unstable additive/multiplicative pe Author(s) Hagiwara, T; Araki, M Citation IEEE Transactions on Automatic Cont 346 Issue Date 998-09 URL http://hdl.handle.net/2433/39968

More information

Iterative Feedback Tuning for robust controller design and optimization

Iterative Feedback Tuning for robust controller design and optimization Iterative Feedback Tuning for robust controller design and optimization Hynek Procházka, Michel Gevers, Brian D.O. Anderson, Christel Ferrera Abstract This paper introduces a new approach for robust controller

More information

Chapter 9 Robust Stability in SISO Systems 9. Introduction There are many reasons to use feedback control. As we have seen earlier, with the help of a

Chapter 9 Robust Stability in SISO Systems 9. Introduction There are many reasons to use feedback control. As we have seen earlier, with the help of a Lectures on Dynamic Systems and Control Mohammed Dahleh Munther A. Dahleh George Verghese Department of Electrical Engineering and Computer Science Massachuasetts Institute of Technology c Chapter 9 Robust

More information

Lecture 7 (Weeks 13-14)

Lecture 7 (Weeks 13-14) Lecture 7 (Weeks 13-14) Introduction to Multivariable Control (SP - Chapters 3 & 4) Eugenio Schuster schuster@lehigh.edu Mechanical Engineering and Mechanics Lehigh University Lecture 7 (Weeks 13-14) p.

More information

Fall 線性系統 Linear Systems. Chapter 08 State Feedback & State Estimators (SISO) Feng-Li Lian. NTU-EE Sep07 Jan08

Fall 線性系統 Linear Systems. Chapter 08 State Feedback & State Estimators (SISO) Feng-Li Lian. NTU-EE Sep07 Jan08 Fall 2007 線性系統 Linear Systems Chapter 08 State Feedback & State Estimators (SISO) Feng-Li Lian NTU-EE Sep07 Jan08 Materials used in these lecture notes are adopted from Linear System Theory & Design, 3rd.

More information

LMI Based Model Order Reduction Considering the Minimum Phase Characteristic of the System

LMI Based Model Order Reduction Considering the Minimum Phase Characteristic of the System LMI Based Model Order Reduction Considering the Minimum Phase Characteristic of the System Gholamreza Khademi, Haniyeh Mohammadi, and Maryam Dehghani School of Electrical and Computer Engineering Shiraz

More information

CHAPTER 5 ROBUSTNESS ANALYSIS OF THE CONTROLLER

CHAPTER 5 ROBUSTNESS ANALYSIS OF THE CONTROLLER 114 CHAPTER 5 ROBUSTNESS ANALYSIS OF THE CONTROLLER 5.1 INTRODUCTION Robust control is a branch of control theory that explicitly deals with uncertainty in its approach to controller design. It also refers

More information

Chapter 7 Interconnected Systems and Feedback: Well-Posedness, Stability, and Performance 7. Introduction Feedback control is a powerful approach to o

Chapter 7 Interconnected Systems and Feedback: Well-Posedness, Stability, and Performance 7. Introduction Feedback control is a powerful approach to o Lectures on Dynamic Systems and Control Mohammed Dahleh Munther A. Dahleh George Verghese Department of Electrical Engineering and Computer Science Massachuasetts Institute of Technology c Chapter 7 Interconnected

More information

BUMPLESS SWITCHING CONTROLLERS. William A. Wolovich and Alan B. Arehart 1. December 27, Abstract

BUMPLESS SWITCHING CONTROLLERS. William A. Wolovich and Alan B. Arehart 1. December 27, Abstract BUMPLESS SWITCHING CONTROLLERS William A. Wolovich and Alan B. Arehart 1 December 7, 1995 Abstract This paper outlines the design of bumpless switching controllers that can be used to stabilize MIMO plants

More information

Iterative Learning Control Analysis and Design I

Iterative Learning Control Analysis and Design I Iterative Learning Control Analysis and Design I Electronics and Computer Science University of Southampton Southampton, SO17 1BJ, UK etar@ecs.soton.ac.uk http://www.ecs.soton.ac.uk/ Contents Basics Representations

More information

Near Optimal LQR Performance for Uncertain First Order Systems

Near Optimal LQR Performance for Uncertain First Order Systems Near Optimal LQR Performance for Uncertain First Order Systems Li Luo Daniel Miller e-commerce Development Dept. of Elect. and Comp. Eng. IBM Canada Toronto Laboratory University of Waterloo Markham, Ontario

More information

Uncertainty and Robustness for SISO Systems

Uncertainty and Robustness for SISO Systems Uncertainty and Robustness for SISO Systems ELEC 571L Robust Multivariable Control prepared by: Greg Stewart Outline Nature of uncertainty (models and signals). Physical sources of model uncertainty. Mathematical

More information

Closed-loop system 2/1/2016. Generally MIMO case. Two-degrees-of-freedom (2 DOF) control structure. (2 DOF structure) The closed loop equations become

Closed-loop system 2/1/2016. Generally MIMO case. Two-degrees-of-freedom (2 DOF) control structure. (2 DOF structure) The closed loop equations become Closed-loop system enerally MIMO case Two-degrees-of-freedom (2 DOF) control structure (2 DOF structure) 2 The closed loop equations become solving for z gives where is the closed loop transfer function

More information

6.245: MULTIVARIABLE CONTROL SYSTEMS by A. Megretski. Solutions to Problem Set 1 1. Massachusetts Institute of Technology

6.245: MULTIVARIABLE CONTROL SYSTEMS by A. Megretski. Solutions to Problem Set 1 1. Massachusetts Institute of Technology Massachusetts Institute of Technology Department of Electrical Engineering and Computer Science 6.245: MULTIVARIABLE CONTROL SYSTEMS by A. Megretski Solutions to Problem Set 1 1 Problem 1.1T Consider the

More information

Lyapunov Stability of Linear Predictor Feedback for Distributed Input Delays

Lyapunov Stability of Linear Predictor Feedback for Distributed Input Delays IEEE TRANSACTIONS ON AUTOMATIC CONTROL VOL. 56 NO. 3 MARCH 2011 655 Lyapunov Stability of Linear Predictor Feedback for Distributed Input Delays Nikolaos Bekiaris-Liberis Miroslav Krstic In this case system

More information

Disturbance Attenuation for a Class of Nonlinear Systems by Output Feedback

Disturbance Attenuation for a Class of Nonlinear Systems by Output Feedback Disturbance Attenuation for a Class of Nonlinear Systems by Output Feedback Wei in Chunjiang Qian and Xianqing Huang Submitted to Systems & Control etters /5/ Abstract This paper studies the problem of

More information

Frequency methods for the analysis of feedback systems. Lecture 6. Loop analysis of feedback systems. Nyquist approach to study stability

Frequency methods for the analysis of feedback systems. Lecture 6. Loop analysis of feedback systems. Nyquist approach to study stability Lecture 6. Loop analysis of feedback systems 1. Motivation 2. Graphical representation of frequency response: Bode and Nyquist curves 3. Nyquist stability theorem 4. Stability margins Frequency methods

More information

10 Transfer Matrix Models

10 Transfer Matrix Models MIT EECS 6.241 (FALL 26) LECTURE NOTES BY A. MEGRETSKI 1 Transfer Matrix Models So far, transfer matrices were introduced for finite order state space LTI models, in which case they serve as an important

More information

THIS paper deals with robust control in the setup associated

THIS paper deals with robust control in the setup associated IEEE TRANSACTIONS ON AUTOMATIC CONTROL, VOL 50, NO 10, OCTOBER 2005 1501 Control-Oriented Model Validation and Errors Quantification in the `1 Setup V F Sokolov Abstract A priori information required for

More information

Synthesis via State Space Methods

Synthesis via State Space Methods Chapter 18 Synthesis via State Space Methods Here, we will give a state space interpretation to many of the results described earlier. In a sense, this will duplicate the earlier work. Our reason for doing

More information

Chapter 2. Classical Control System Design. Dutch Institute of Systems and Control

Chapter 2. Classical Control System Design. Dutch Institute of Systems and Control Chapter 2 Classical Control System Design Overview Ch. 2. 2. Classical control system design Introduction Introduction Steady-state Steady-state errors errors Type Type k k systems systems Integral Integral

More information

A brief introduction to robust H control

A brief introduction to robust H control A brief introduction to robust H control Jean-Marc Biannic System Control and Flight Dynamics Department ONERA, Toulouse. http://www.onera.fr/staff/jean-marc-biannic/ http://jm.biannic.free.fr/ European

More information

Simultaneous State and Fault Estimation for Descriptor Systems using an Augmented PD Observer

Simultaneous State and Fault Estimation for Descriptor Systems using an Augmented PD Observer Preprints of the 19th World Congress The International Federation of Automatic Control Simultaneous State and Fault Estimation for Descriptor Systems using an Augmented PD Observer Fengming Shi*, Ron J.

More information

Structured Stochastic Uncertainty

Structured Stochastic Uncertainty Structured Stochastic Uncertainty Bassam Bamieh Department of Mechanical Engineering University of California at Santa Barbara Santa Barbara, CA, 9306 bamieh@engineeringucsbedu Abstract We consider linear

More information

H-INFINITY CONTROLLER DESIGN FOR A DC MOTOR MODEL WITH UNCERTAIN PARAMETERS

H-INFINITY CONTROLLER DESIGN FOR A DC MOTOR MODEL WITH UNCERTAIN PARAMETERS Engineering MECHANICS, Vol. 18, 211, No. 5/6, p. 271 279 271 H-INFINITY CONTROLLER DESIGN FOR A DC MOTOR MODEL WITH UNCERTAIN PARAMETERS Lukáš Březina*, Tomáš Březina** The proposed article deals with

More information

Fundamental Design Limitations of the General Control Configuration

Fundamental Design Limitations of the General Control Configuration IEEE TRANSACTIONS ON AUTOMATIC CONTROL, VOL 48, NO 8, AUGUST 2003 1355 Fundamental Design Limitations of the General Control Configuration Jim S Freudenberg, Fellow, IEEE, C V Hollot, Senior Member, IEEE,

More information

Optimal Signal to Noise Ratio in Feedback over Communication Channels with Memory

Optimal Signal to Noise Ratio in Feedback over Communication Channels with Memory Proceedings of the 45th IEEE Conference on Decision & Control Manchester rand Hyatt Hotel San Diego, CA, USA, December 13-15, 26 Optimal Signal to Noise Ratio in Feedback over Communication Channels with

More information

ECE317 : Feedback and Control

ECE317 : Feedback and Control ECE317 : Feedback and Control Lecture : Routh-Hurwitz stability criterion Examples Dr. Richard Tymerski Dept. of Electrical and Computer Engineering Portland State University 1 Course roadmap Modeling

More information

arxiv: v1 [cs.sy] 2 Apr 2019

arxiv: v1 [cs.sy] 2 Apr 2019 On the Existence of a Fixed Spectrum for a Multi-channel Linear System: A Matroid Theory Approach F Liu 1 and A S Morse 1 arxiv:190401499v1 [cssy] 2 Apr 2019 Abstract Conditions for the existence of a

More information

Stability radii and spectral value sets for real matrix perturbations Introduction D. Hinrichsen and B. Kelb Institut fur Dynamische Systeme Universitat Bremen D-859 Bremen, F. R. G. dh@mathematik.uni-bremen.de

More information

Analysis of SISO Control Loops

Analysis of SISO Control Loops Chapter 5 Analysis of SISO Control Loops Topics to be covered For a given controller and plant connected in feedback we ask and answer the following questions: Is the loop stable? What are the sensitivities

More information

MRAGPC Control of MIMO Processes with Input Constraints and Disturbance

MRAGPC Control of MIMO Processes with Input Constraints and Disturbance Proceedings of the World Congress on Engineering and Computer Science 9 Vol II WCECS 9, October -, 9, San Francisco, USA MRAGPC Control of MIMO Processes with Input Constraints and Disturbance A. S. Osunleke,

More information

Fundamental Limitations in Self-Sensing Magnetic Bearings when Modeled as Linear Periodic Systems

Fundamental Limitations in Self-Sensing Magnetic Bearings when Modeled as Linear Periodic Systems Fundamental Limitations in Self-Sensing Magnetic Bearings when Modeled as Linear Periodic Systems K.S. Peterson and R.H. Middleton and J.S. Freudenberg Abstract In Magnetic Bearing Measurement Configurations

More information

ECE317 : Feedback and Control

ECE317 : Feedback and Control ECE317 : Feedback and Control Lecture : Stability Routh-Hurwitz stability criterion Dr. Richard Tymerski Dept. of Electrical and Computer Engineering Portland State University 1 Course roadmap Modeling

More information

Topic # Feedback Control Systems

Topic # Feedback Control Systems Topic #19 16.31 Feedback Control Systems Stengel Chapter 6 Question: how well do the large gain and phase margins discussed for LQR map over to DOFB using LQR and LQE (called LQG)? Fall 2010 16.30/31 19

More information

(Continued on next page)

(Continued on next page) (Continued on next page) 18.2 Roots of Stability Nyquist Criterion 87 e(s) 1 S(s) = =, r(s) 1 + P (s)c(s) where P (s) represents the plant transfer function, and C(s) the compensator. The closedloop characteristic

More information

Research Article State-PID Feedback for Pole Placement of LTI Systems

Research Article State-PID Feedback for Pole Placement of LTI Systems Mathematical Problems in Engineering Volume 211, Article ID 92943, 2 pages doi:1.1155/211/92943 Research Article State-PID Feedback for Pole Placement of LTI Systems Sarawut Sujitjorn and Witchupong Wiboonjaroen

More information

Fixed-Order Robust H Controller Design with Regional Pole Assignment

Fixed-Order Robust H Controller Design with Regional Pole Assignment SUBMITTED 1 Fixed-Order Robust H Controller Design with Regional Pole Assignment Fuwen Yang, Mahbub Gani, and Didier Henrion Abstract In this paper, the problem of designing fixed-order robust H controllers

More information

A Case Study for the Delay-type Nehari Problem

A Case Study for the Delay-type Nehari Problem Proceedings of the 44th EEE Conference on Decision and Control, and the European Control Conference 5 Seville, Spain, December -5, 5 MoA A Case Study for the Delay-type Nehari Problem Qing-Chang Zhong

More information

ROBUST STABILITY AND PERFORMANCE ANALYSIS OF UNSTABLE PROCESS WITH DEAD TIME USING Mu SYNTHESIS

ROBUST STABILITY AND PERFORMANCE ANALYSIS OF UNSTABLE PROCESS WITH DEAD TIME USING Mu SYNTHESIS ROBUST STABILITY AND PERFORMANCE ANALYSIS OF UNSTABLE PROCESS WITH DEAD TIME USING Mu SYNTHESIS I. Thirunavukkarasu 1, V. I. George 1, G. Saravana Kumar 1 and A. Ramakalyan 2 1 Department o Instrumentation

More information

State Regulator. Advanced Control. design of controllers using pole placement and LQ design rules

State Regulator. Advanced Control. design of controllers using pole placement and LQ design rules Advanced Control State Regulator Scope design of controllers using pole placement and LQ design rules Keywords pole placement, optimal control, LQ regulator, weighting matrixes Prerequisites Contact state

More information

POSITIVE REALNESS OF A TRANSFER FUNCTION NEITHER IMPLIES NOR IS IMPLIED BY THE EXTERNAL POSITIVITY OF THEIR ASSOCIATE REALIZATIONS

POSITIVE REALNESS OF A TRANSFER FUNCTION NEITHER IMPLIES NOR IS IMPLIED BY THE EXTERNAL POSITIVITY OF THEIR ASSOCIATE REALIZATIONS POSITIVE REALNESS OF A TRANSFER FUNCTION NEITHER IMPLIES NOR IS IMPLIED BY THE EXTERNAL POSITIVITY OF THEIR ASSOCIATE REALIZATIONS Abstract This letter discusses the differences in-between positive realness

More information

L2 gains and system approximation quality 1

L2 gains and system approximation quality 1 Massachusetts Institute of Technology Department of Electrical Engineering and Computer Science 6.242, Fall 24: MODEL REDUCTION L2 gains and system approximation quality 1 This lecture discusses the utility

More information

Parametrization of All Strictly Causal Stabilizing Controllers of Multidimensional Systems single-input single-output case

Parametrization of All Strictly Causal Stabilizing Controllers of Multidimensional Systems single-input single-output case Parametrization of All Strictly Causal Stabilizing Controllers of Multidimensional Systems single-input single-output case K. Mori Abstract We give a parametrization of all strictly causal stabilizing

More information

EL2520 Control Theory and Practice

EL2520 Control Theory and Practice So far EL2520 Control Theory and Practice r Fr wu u G w z n Lecture 5: Multivariable systems -Fy Mikael Johansson School of Electrical Engineering KTH, Stockholm, Sweden SISO control revisited: Signal

More information

Control Systems I. Lecture 7: Feedback and the Root Locus method. Readings: Jacopo Tani. Institute for Dynamic Systems and Control D-MAVT ETH Zürich

Control Systems I. Lecture 7: Feedback and the Root Locus method. Readings: Jacopo Tani. Institute for Dynamic Systems and Control D-MAVT ETH Zürich Control Systems I Lecture 7: Feedback and the Root Locus method Readings: Jacopo Tani Institute for Dynamic Systems and Control D-MAVT ETH Zürich November 2, 2018 J. Tani, E. Frazzoli (ETH) Lecture 7:

More information

Control Systems I. Lecture 6: Poles and Zeros. Readings: Emilio Frazzoli. Institute for Dynamic Systems and Control D-MAVT ETH Zürich

Control Systems I. Lecture 6: Poles and Zeros. Readings: Emilio Frazzoli. Institute for Dynamic Systems and Control D-MAVT ETH Zürich Control Systems I Lecture 6: Poles and Zeros Readings: Emilio Frazzoli Institute for Dynamic Systems and Control D-MAVT ETH Zürich October 27, 2017 E. Frazzoli (ETH) Lecture 6: Control Systems I 27/10/2017

More information

An efficient algorithm to compute the real perturbation values of a matrix

An efficient algorithm to compute the real perturbation values of a matrix An efficient algorithm to compute the real perturbation values of a matrix Simon Lam and Edward J. Davison 1 Abstract In this paper, an efficient algorithm is presented for solving the nonlinear 1-D optimization

More information

Fundamental Limitations in Self-Sensing Magnetic Bearings when Modeled as Linear Periodic Systems

Fundamental Limitations in Self-Sensing Magnetic Bearings when Modeled as Linear Periodic Systems Proceedings of the 6 American Control Conference Minneapolis, Minnesota, USA, June 14-16, 6 FrA11.1 Fundamental Limitations in Self-Sensing Magnetic Bearings when Modeled as Linear Periodic Systems K.S.

More information

Mapping MIMO control system specifications into parameter space

Mapping MIMO control system specifications into parameter space Mapping MIMO control system specifications into parameter space Michael Muhler 1 Abstract This paper considers the mapping of design objectives for parametric multi-input multi-output systems into parameter

More information

NOWADAYS, many control applications have some control

NOWADAYS, many control applications have some control 1650 IEEE TRANSACTIONS ON AUTOMATIC CONTROL, VOL 49, NO 10, OCTOBER 2004 Input Output Stability Properties of Networked Control Systems D Nešić, Senior Member, IEEE, A R Teel, Fellow, IEEE Abstract Results

More information

Closed-Loop Structure of Discrete Time H Controller

Closed-Loop Structure of Discrete Time H Controller Closed-Loop Structure of Discrete Time H Controller Waree Kongprawechnon 1,Shun Ushida 2, Hidenori Kimura 2 Abstract This paper is concerned with the investigation of the closed-loop structure of a discrete

More information

Structured State Space Realizations for SLS Distributed Controllers

Structured State Space Realizations for SLS Distributed Controllers Structured State Space Realizations for SLS Distributed Controllers James Anderson and Nikolai Matni Abstract In recent work the system level synthesis (SLS) paradigm has been shown to provide a truly

More information

Chap 4. State-Space Solutions and

Chap 4. State-Space Solutions and Chap 4. State-Space Solutions and Realizations Outlines 1. Introduction 2. Solution of LTI State Equation 3. Equivalent State Equations 4. Realizations 5. Solution of Linear Time-Varying (LTV) Equations

More information

On Optimal Performance for Linear Time-Varying Systems

On Optimal Performance for Linear Time-Varying Systems On Optimal Performance for Linear Time-Varying Systems Seddik M. Djouadi and Charalambos D. Charalambous Abstract In this paper we consider the optimal disturbance attenuation problem and robustness for

More information

Exam. 135 minutes + 15 minutes reading time

Exam. 135 minutes + 15 minutes reading time Exam January 23, 27 Control Systems I (5-59-L) Prof. Emilio Frazzoli Exam Exam Duration: 35 minutes + 5 minutes reading time Number of Problems: 45 Number of Points: 53 Permitted aids: Important: 4 pages

More information

CDS 101/110a: Lecture 10-1 Robust Performance

CDS 101/110a: Lecture 10-1 Robust Performance CDS 11/11a: Lecture 1-1 Robust Performance Richard M. Murray 1 December 28 Goals: Describe how to represent uncertainty in process dynamics Describe how to analyze a system in the presence of uncertainty

More information

CDS 101/110a: Lecture 8-1 Frequency Domain Design

CDS 101/110a: Lecture 8-1 Frequency Domain Design CDS 11/11a: Lecture 8-1 Frequency Domain Design Richard M. Murray 17 November 28 Goals: Describe canonical control design problem and standard performance measures Show how to use loop shaping to achieve

More information

Chapter 5. Standard LTI Feedback Optimization Setup. 5.1 The Canonical Setup

Chapter 5. Standard LTI Feedback Optimization Setup. 5.1 The Canonical Setup Chapter 5 Standard LTI Feedback Optimization Setup Efficient LTI feedback optimization algorithms comprise a major component of modern feedback design approach: application problems involving complex models

More information

QUANTITATIVE L P STABILITY ANALYSIS OF A CLASS OF LINEAR TIME-VARYING FEEDBACK SYSTEMS

QUANTITATIVE L P STABILITY ANALYSIS OF A CLASS OF LINEAR TIME-VARYING FEEDBACK SYSTEMS Int. J. Appl. Math. Comput. Sci., 2003, Vol. 13, No. 2, 179 184 QUANTITATIVE L P STABILITY ANALYSIS OF A CLASS OF LINEAR TIME-VARYING FEEDBACK SYSTEMS PINI GURFIL Department of Mechanical and Aerospace

More information

Stabilization, Pole Placement, and Regular Implementability

Stabilization, Pole Placement, and Regular Implementability IEEE TRANSACTIONS ON AUTOMATIC CONTROL, VOL. 47, NO. 5, MAY 2002 735 Stabilization, Pole Placement, and Regular Implementability Madhu N. Belur and H. L. Trentelman, Senior Member, IEEE Abstract In this

More information

A Comparative Study on Automatic Flight Control for small UAV

A Comparative Study on Automatic Flight Control for small UAV Proceedings of the 5 th International Conference of Control, Dynamic Systems, and Robotics (CDSR'18) Niagara Falls, Canada June 7 9, 18 Paper No. 13 DOI: 1.11159/cdsr18.13 A Comparative Study on Automatic

More information

State feedback gain scheduling for linear systems with time-varying parameters

State feedback gain scheduling for linear systems with time-varying parameters State feedback gain scheduling for linear systems with time-varying parameters Vinícius F. Montagner and Pedro L. D. Peres Abstract This paper addresses the problem of parameter dependent state feedback

More information

Design and Implementation of Sliding Mode Controller using Coefficient Diagram Method for a nonlinear process

Design and Implementation of Sliding Mode Controller using Coefficient Diagram Method for a nonlinear process IOSR Journal of Electrical and Electronics Engineering (IOSR-JEEE) e-issn: 2278-1676,p-ISSN: 2320-3331, Volume 7, Issue 5 (Sep. - Oct. 2013), PP 19-24 Design and Implementation of Sliding Mode Controller

More information

Norm invariant discretization for sampled-data fault detection

Norm invariant discretization for sampled-data fault detection Automatica 41 (25 1633 1637 www.elsevier.com/locate/automatica Technical communique Norm invariant discretization for sampled-data fault detection Iman Izadi, Tongwen Chen, Qing Zhao Department of Electrical

More information

A design method for two-degree-of-freedom multi-period repetitive controllers for multiple-input/multiple-output systems

A design method for two-degree-of-freedom multi-period repetitive controllers for multiple-input/multiple-output systems A design method for two-degree-of-freedom multi-period repetitive controllers for multiple-input/multiple-output systems Zhongxiang Chen Kou Yamada Tatsuya Sakanushi Iwanori Murakami Yoshinori Ando Nhan

More information

A DESIGN METHOD FOR SIMPLE REPETITIVE CONTROLLERS WITH SPECIFIED INPUT-OUTPUT CHARACTERISTIC

A DESIGN METHOD FOR SIMPLE REPETITIVE CONTROLLERS WITH SPECIFIED INPUT-OUTPUT CHARACTERISTIC International Journal of Innovative Computing, Information Control ICIC International c 202 ISSN 349-498 Volume 8, Number 7(A), July 202 pp. 4883 4899 A DESIGN METHOD FOR SIMPLE REPETITIVE CONTROLLERS

More information

Bisection Algorithm for Computing the Frequency Response Gain of Sampled-Data Systems Infinite-Dimensional Congruent Transformation Approach

Bisection Algorithm for Computing the Frequency Response Gain of Sampled-Data Systems Infinite-Dimensional Congruent Transformation Approach IEEE TRANSACTIONS ON AUTOMATIC CONTROL, VOL. 46, NO. 3, MARCH 2001 369 Bisection Algorithm for Computing the Frequency Response Gain of Sampled-Data Systems Infinite-Dimensional Congruent Transformation

More information

Linear Quadratic Gausssian Control Design with Loop Transfer Recovery

Linear Quadratic Gausssian Control Design with Loop Transfer Recovery Linear Quadratic Gausssian Control Design with Loop Transfer Recovery Leonid Freidovich Department of Mathematics Michigan State University MI 48824, USA e-mail:leonid@math.msu.edu http://www.math.msu.edu/

More information

Robust Tuning of Power System Stabilizers Using Coefficient Diagram Method

Robust Tuning of Power System Stabilizers Using Coefficient Diagram Method International Journal of Electrical Engineering. ISSN 0974-2158 Volume 7, Number 2 (2014), pp. 257-270 International Research Publication House http://www.irphouse.com Robust Tuning of Power System Stabilizers

More information

ẋ n = f n (x 1,...,x n,u 1,...,u m ) (5) y 1 = g 1 (x 1,...,x n,u 1,...,u m ) (6) y p = g p (x 1,...,x n,u 1,...,u m ) (7)

ẋ n = f n (x 1,...,x n,u 1,...,u m ) (5) y 1 = g 1 (x 1,...,x n,u 1,...,u m ) (6) y p = g p (x 1,...,x n,u 1,...,u m ) (7) EEE582 Topical Outline A.A. Rodriguez Fall 2007 GWC 352, 965-3712 The following represents a detailed topical outline of the course. It attempts to highlight most of the key concepts to be covered and

More information

ON CHATTERING-FREE DISCRETE-TIME SLIDING MODE CONTROL DESIGN. Seung-Hi Lee

ON CHATTERING-FREE DISCRETE-TIME SLIDING MODE CONTROL DESIGN. Seung-Hi Lee ON CHATTERING-FREE DISCRETE-TIME SLIDING MODE CONTROL DESIGN Seung-Hi Lee Samsung Advanced Institute of Technology, Suwon, KOREA shl@saitsamsungcokr Abstract: A sliding mode control method is presented

More information

HANKEL-NORM BASED INTERACTION MEASURE FOR INPUT-OUTPUT PAIRING

HANKEL-NORM BASED INTERACTION MEASURE FOR INPUT-OUTPUT PAIRING Copyright 2002 IFAC 15th Triennial World Congress, Barcelona, Spain HANKEL-NORM BASED INTERACTION MEASURE FOR INPUT-OUTPUT PAIRING Björn Wittenmark Department of Automatic Control Lund Institute of Technology

More information

Robust Control. 2nd class. Spring, 2018 Instructor: Prof. Masayuki Fujita (S5-303B) Tue., 17th April, 2018, 10:45~12:15, S423 Lecture Room

Robust Control. 2nd class. Spring, 2018 Instructor: Prof. Masayuki Fujita (S5-303B) Tue., 17th April, 2018, 10:45~12:15, S423 Lecture Room Robust Control Spring, 2018 Instructor: Prof. Masayuki Fujita (S5-303B) 2nd class Tue., 17th April, 2018, 10:45~12:15, S423 Lecture Room 2. Nominal Performance 2.1 Weighted Sensitivity [SP05, Sec. 2.8,

More information

Robust SPR Synthesis for Low-Order Polynomial Segments and Interval Polynomials

Robust SPR Synthesis for Low-Order Polynomial Segments and Interval Polynomials Robust SPR Synthesis for Low-Order Polynomial Segments and Interval Polynomials Long Wang ) and Wensheng Yu 2) ) Dept. of Mechanics and Engineering Science, Center for Systems and Control, Peking University,

More information

Control System Design

Control System Design ELEC ENG 4CL4: Control System Design Notes for Lecture #36 Dr. Ian C. Bruce Room: CRL-229 Phone ext.: 26984 Email: ibruce@mail.ece.mcmaster.ca Friday, April 4, 2003 3. Cascade Control Next we turn to an

More information

Introduction to Model Order Reduction

Introduction to Model Order Reduction Introduction to Model Order Reduction Lecture 1: Introduction and overview Henrik Sandberg Kin Cheong Sou Automatic Control Lab, KTH ACCESS Specialized Course Graduate level Ht 2010, period 1 1 Overview

More information

Control System Design

Control System Design ELEC ENG 4CL4: Control System Design Notes for Lecture #14 Wednesday, February 5, 2003 Dr. Ian C. Bruce Room: CRL-229 Phone ext.: 26984 Email: ibruce@mail.ece.mcmaster.ca Chapter 7 Synthesis of SISO Controllers

More information

Overlapping Control Design for Multi-Channel Systems

Overlapping Control Design for Multi-Channel Systems Overlapping Control Design for Multi-Channel Systems Javad Lavaei a, Amir G. Aghdam b a Department of Control and Dynamical Systems, California Institute of Technology, Pasadena, CA 91125, USA b Department

More information

Robust Loop Shaping Controller Design for Spectral Models by Quadratic Programming

Robust Loop Shaping Controller Design for Spectral Models by Quadratic Programming Robust Loop Shaping Controller Design for Spectral Models by Quadratic Programming Gorka Galdos, Alireza Karimi and Roland Longchamp Abstract A quadratic programming approach is proposed to tune fixed-order

More information

A robust Hansen Sargent prediction formula

A robust Hansen Sargent prediction formula Economics Letters 71 (001) 43 48 www.elsevier.com/ locate/ econbase A robust Hansen Sargent prediction formula Kenneth Kasa* Research Department, Federal Reserve Bank of San Francisco, P.O. Box 770, San

More information

Recent Advances in Positive Systems: The Servomechanism Problem

Recent Advances in Positive Systems: The Servomechanism Problem Recent Advances in Positive Systems: The Servomechanism Problem 47 th IEEE Conference on Decision and Control December 28. Bartek Roszak and Edward J. Davison Systems Control Group, University of Toronto

More information

An LQ R weight selection approach to the discrete generalized H 2 control problem

An LQ R weight selection approach to the discrete generalized H 2 control problem INT. J. CONTROL, 1998, VOL. 71, NO. 1, 93± 11 An LQ R weight selection approach to the discrete generalized H 2 control problem D. A. WILSON², M. A. NEKOUI² and G. D. HALIKIAS² It is known that a generalized

More information

Linear State Feedback Controller Design

Linear State Feedback Controller Design Assignment For EE5101 - Linear Systems Sem I AY2010/2011 Linear State Feedback Controller Design Phang Swee King A0033585A Email: king@nus.edu.sg NGS/ECE Dept. Faculty of Engineering National University

More information

Chapter 9 Observers, Model-based Controllers 9. Introduction In here we deal with the general case where only a subset of the states, or linear combin

Chapter 9 Observers, Model-based Controllers 9. Introduction In here we deal with the general case where only a subset of the states, or linear combin Lectures on Dynamic Systems and Control Mohammed Dahleh Munther A. Dahleh George Verghese Department of Electrical Engineering and Computer Science Massachuasetts Institute of Technology c Chapter 9 Observers,

More information